Claims (693)
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which a cylindrical inner rotor blade group (60C) is one stage and a cylindrical outer rotor blade group (60D) is two stages, and a vertical all-blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which a cylindrical inner rotor blade group (60C) has two stages and a cylindrical outer rotor blade group (60D) has three stages, and a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which a cylindrical inner rotor blade group (60C) has three stages and a cylindrical outer rotor blade group (60D) has four stages, and a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, with a cylindrical inner blade group (60C) as four stages and a cylindrical outer blade group (60D) as five stages, and a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which a cylindrical inner rotor blade group (60C) is five stages and a cylindrical outer rotor blade group (60D) is six stages, and a vertical all blade steam water gravity turbine (11Z) is used.
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which a cylindrical inner rotor blade group (60C) has six stages and a cylindrical outer rotor blade group (60D) has seven stages, and a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, with a cylindrical inner blade group (60C) as seven stages and a cylindrical outer blade group (60D) as eight stages, and a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a cylindrical inner rotor blade group (60C) as eight stages and a cylindrical outer rotor blade group (60D) as nine stages as a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a cylindrical inner blade group (60C) as nine stages and a cylindrical outer blade group (60D) as ten stages, and a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a cylindrical inner rotor blade group (60C) as 10 stages and a cylindrical outer rotor blade group (60D) as 11 stages and a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a cylindrical inner rotor blade group (60C) as 11 stages and a cylindrical outer rotor blade group (60D) as 12 stages, and a vertical all-blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles using a cylindrical inner blade group (60C) as one stage, a cylindrical outer blade group (60D) as two stages, and each stage as a cast part, a vertical all blade steam water gravity turbine (11Z). Merger engine and merger method.
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy conservation cycles with a cylindrical inner blade group (60C) as two stages, a cylindrical outer blade group (60D) as three stages, and each stage as one cast part as a vertical all blade steam water gravity turbine (11Z) Merger engine and merger method.
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles with a cylindrical inner rotor blade group (60C) as three stages, a cylindrical outer rotor blade group (60D) as four stages, and each stage as a cast part, a vertical all blade steam water gravity turbine (11Z). Merger engine and merger method.
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy conservation cycles with a cylindrical inner blade group (60C) as four stages, a cylindrical outer blade group (60D) as five stages, and each stage as a cast part, a vertical all blade steam water gravity turbine (11Z). Merger engine and merger method.
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy conservation cycles with a cylindrical inner blade group (60C) as five stages, a cylindrical outer blade group (60D) as six stages, and each stage as a cast part, a vertical all blade steam water gravity turbine (11Z). Merger engine and merger method.
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles with a cylindrical inner blade group (60C) as six stages, a cylindrical outer blade group (60D) as seven stages, and each stage as a cast part, a vertical all blade steam water gravity turbine (11Z) Merger engine and merger method.
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles with a cylindrical inner blade group (60C) as seven stages, a cylindrical outer blade group (60D) as eight stages, and each stage as a cast part, a vertical all blade steam water gravity turbine (11Z) Merger engine and merger method.
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles using a cylindrical all-blade group (60C) as eight stages, a cylindrical outer blade group (60D) as nine stages, and each stage as one cast part, a vertical all-blade steam-water gravity turbine (11Z) Merger engine and merger method.
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles using a cylindrical inner blade group (60C) as nine stages, a cylindrical outer blade group (60D) as ten stages, and each stage as one cast part as a vertical all blade steam water gravity turbine (11Z). Merger engine and merger method.
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles using a cylindrical inner rotor blade group (60C) as 10 stages, a cylindrical outer rotor blade group (60D) as 11 stages, and each stage as one casting part as a vertical all blade steam water gravity turbine (11Z). Merger engine and merger method.
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycles using a cylindrical inner blade group (60C) as 11 stages, a cylindrical outer blade group (60D) as 12 stages, and each stage as a cast part, a vertical all blade steam water gravity turbine (11Z). Merger engine and merger method.
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is processed as one cast part by a vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage is processed as a cast part with a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage is processed as a cast part with a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage is processed as one cast part by a vertical lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has five stages, the cylindrical outer rotor blade group (60D) has six stages, and each stage is processed as a cast part by a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage is processed as a cast part on a counter-rotating engine vertical lathe (10B). Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has seven stages, the cylindrical outer blade group (60D) has eight stages, and each stage is processed as a cast part with a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage is processed as a cast part on a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is nine stages, the cylindrical outer rotor blade group (60D) is ten stages, and each stage is processed as one cast part by a vertical lathe (10B) for a counter rotating engine, and the vertical type Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage is processed as a cast part on a counter-rotating engine vertical lathe (10B). Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 11 stages, the cylindrical outer rotor blade group (60D) has 12 stages, and each stage is processed as a cast part by a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one cast part. 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is composed of nine stages, the cylindrical outer blade group (60D) is composed of ten stages, and each stage is formed as one cast component, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescence engines and coalescence methods that are processed into a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one casting part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is composed of nine stages, the cylindrical outer blade group (60D) is composed of ten stages, and each stage is formed as one cast component, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine, and the super-high-speed balance adjustment processing is performed to make the vertical rotor blade steam water gravity turbine (11Z) ) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one cast part. 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is four stages, the cylindrical outer blade group (60D) is five stages, and each stage is one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is composed of nine stages, the cylindrical outer blade group (60D) is composed of ten stages, and each stage is formed as one cast component, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part. 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)単数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) A single set of various energy storage cycle coalescence engines and coalescence methods that form a vertical all blade steam water gravity turbine (11Z).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one casting part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is nine stages, the cylindrical outer blade group (60D) is ten stages, and each stage is one cast part. 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)複数組にして竪型全動翼蒸気水重力タービン(11Z)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Apparatus (60B) Inner shaft apparatus (60A) Various energy storage cycle coalescing engine and coalescence method using a plurality of sets of vertical rotor blade steam water gravity turbines (11Z).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as a first stage and a cylindrical outer rotor blade group (60D) as a second stage and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a cylindrical inner rotor blade group (60C) in two stages and a cylindrical outer rotor blade group (60D) in three stages as a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a cylindrical inner rotor blade group (60C) as three stages and a cylindrical outer rotor blade group (60D) as four stages and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as four stages and a cylindrical outer rotor blade group (60D) as five stages and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as five stages and a cylindrical outer rotor blade group (60D) as six stages and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as six stages and a cylindrical outer rotor blade group (60D) as seven stages, and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as seven stages and a cylindrical outer rotor blade group (60D) as eight stages and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as eight stages and a cylindrical outer rotor blade group (60D) as nine stages and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as nine stages and a cylindrical outer rotor blade group (60D) as ten stages and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as 10 stages and a cylindrical outer rotor blade group (60D) as 11 stages, and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a cylindrical inner rotor blade group (60C) as 11 stages and a cylindrical outer rotor blade group (60D) as 12 stages and a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energies for the vertical inner blade group (60C) and the outer cylindrical blade group (60D) as two stages, and each stage as one casting component, and a vertical all-blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy for a cylindrical full-scale blade steam ratio critical material gravity turbine (11Y) with the cylindrical inner blade group (60C) in two stages, the cylindrical outer blade group (60D) in three stages, and each stage as one cast part Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energies for the vertical inner blade group (60C) and the outer cylindrical blade group (60D) as four stages, and each stage as one cast part for the vertical type moving blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy for the vertical inner blade group (60Y) and the outer cylindrical blade group (60D) as five stages, and each stage as one cast part, and a vertical all-blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy for a cylindrical full-scale blade steam ratio critical material gravity turbine (11Y) with a cylindrical inner blade group (60C) as five stages, a cylindrical outer blade group (60D) as six stages, and each stage as one cast part. Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy for the vertical inner blade group (60Y) and the outer cylindrical blade group (60D) as seven stages and each stage as one casting part as a vertical all-blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energies for the vertical inner blade group (60C) and the outer cylindrical blade group (60D) as eight stages, and each stage as one cast component for a vertical all-blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy for the vertical inner rotor blade group (60Y) and the outer cylindrical rotor blade group (60D) as nine stages, and each stage as one cast part for a vertical all-blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energies for the vertical inner blade group (60Y) and the outer cylindrical blade group (60D) as 10 stages, and each stage as one cast part, and a vertical all-blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energies of a vertical all-blade steam ratio critical material gravity turbine (11Y) with 10 cylinder inner rotor blade groups (60C), 11 outer cylinder blade groups (60D) and 11 stages each casting part Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energies for the cylindrical inner blade group (60C) and the outer cylindrical blade group (60D) as 12 stages and each stage as one cast part for the vertical type moving blade steam ratio critical material gravity turbine (11Y) Storage cycle coalescence engine and coalescence method.
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is processed as one cast part by a vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage is processed as a cast part with a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage is processed as a cast part with a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage is processed as one cast part by a vertical lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is five stages, the cylindrical outer rotor blade group (60D) is six stages, and each stage is processed as one cast part by a vertical lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage is processed as a cast part on a counter-rotating engine vertical lathe (10B). Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has seven stages, the cylindrical outer blade group (60D) has eight stages, and each stage is processed as a cast part with a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage is processed as a cast part on a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is nine stages, the cylindrical outer rotor blade group (60D) is ten stages, and each stage is processed as one cast part by a vertical lathe (10B) for a counter rotating engine, and the vertical type Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage is processed as a cast part on a counter-rotating engine vertical lathe (10B). Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 11 stages, the cylindrical outer rotor blade group (60D) has 12 stages, and each stage is processed as a cast part by a vertical turning lathe (10B) for a counter rotating engine. Various energy storage cycle coalescence engine and coalescence method as a moving blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one casting part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is composed of nine stages, the cylindrical outer blade group (60D) is composed of ten stages, and each stage is formed as one cast component, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), various energy storage cycle coalescing engines and coalescence methods that are processed into a vertical all-blade steam ratio critical material gravity turbine (11Y).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one casting part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is composed of nine stages, the cylindrical outer blade group (60D) is composed of ten stages, and each stage is formed as one cast component, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B) and the like are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. (11Y) Various energy storage cycle coalescence engines and coalescence methods.
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one casting part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is composed of nine stages, the cylindrical outer blade group (60D) is composed of ten stages, and each stage is formed as one cast component, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engines and coalescence methods, wherein the inner shaft device (60A) of the device (60B) is a vertical type moving blade steam ratio critical material gravity turbine (11Y) driven vertically by a counter rotating magnetic device (85).
円筒内側動翼群(60C)を1段として円筒外側動翼群(60D)を2段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) is one stage, the cylindrical outer rotor blade group (60D) is two stages, and each stage is one casting part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を2段として円筒外側動翼群(60D)を3段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has two stages, the cylindrical outer rotor blade group (60D) has three stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を3段として円筒外側動翼群(60D)を4段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has three stages, the cylindrical outer rotor blade group (60D) has four stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を4段として円筒外側動翼群(60D)を5段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has four stages, the cylindrical outer rotor blade group (60D) has five stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を5段として円筒外側動翼群(60D)を6段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has five stages, the cylindrical outer blade group (60D) has six stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を6段として円筒外側動翼群(60D)を7段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has six stages, the cylindrical outer blade group (60D) has seven stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を7段として円筒外側動翼群(60D)を8段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has seven stages, the cylindrical outer rotor blade group (60D) has eight stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を8段として円筒外側動翼群(60D)を9段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has eight stages, the cylindrical outer blade group (60D) has nine stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を9段として円筒外側動翼群(60D)を10段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) is composed of nine stages, the cylindrical outer blade group (60D) is composed of ten stages, and each stage is formed as one cast component, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を10段として円筒外側動翼群(60D)を11段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner rotor blade group (60C) has 10 stages, the cylindrical outer rotor blade group (60D) has 11 stages, and each stage has one cast part, and the counter rotating engine vertical lathe (10B) and turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
円筒内側動翼群(60C)を11段として円筒外側動翼群(60D)を12段として夫々の段を1鋳造部品として二重反転機関用立型旋盤(10B)とタービン翼用研削盤(10F)で加工して外側軸装置(60B)等夫々を仮組立して二重反転機関用立型旋盤(10B)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で垂直連結駆動する竪型全動翼蒸気比重大物質重力タービン(11Y)とした各種エネルギ保存サイクル合体機関及び合体方法。
The cylindrical inner blade group (60C) has 11 stages, the cylindrical outer blade group (60D) has 12 stages, and each stage has one cast part, and a counter rotating engine vertical lathe (10B) and a turbine blade grinding machine ( 10F), the outer shaft device (60B), etc. are temporarily assembled and held by the vertical turning lathe (10B) for counter rotating engine. Various energy storage cycle coalescence engine and coalescence method using a vertical type moving blade steam ratio critical material gravity turbine (11Y) in which the device (60B) inner shaft device (60A) is vertically connected and driven by a counter rotating gear device (85Y).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods with a horizontal all-blade steam-water gravity turbine (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as one cast part and a total length of 1.5 m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescing methods in which the integrated turbine blade group (8G) horizontal shaft (16A) is a cast part and the total length is 2 m or less, and a horizontal all-blade steam-water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) horizontal shaft (16A) is a cast part and the total length is 2.5 m or less, and is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which the integrated turbine blade group (8G) and the horizontal shaft (16A) are one cast part and the total length is 3 m or less, and a horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods with a horizontal all-blade steam-water gravity turbine (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as one cast part and a total length of 3,5 m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescing methods in which the integrated turbine blade group (8G) horizontal shaft (16A) is a cast part and the total length is 4 m or less, and a horizontal all-blade steam-water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) horizontal shaft (16A) is a cast part and the overall length is 4,5 m or less, and is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which the integrated turbine blade group (8G) and the horizontal axis (16A) are one cast part and the total length is 5 m or less, and a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) horizontal shaft (16A) is a cast part and the overall length is 5,5 m or less and is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescing methods in which the integrated turbine blade group (8G) horizontal shaft (16A) is a cast part and the total length is 6 m or less, and a horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as one cast part and has a total length of 6 m or more, and is a horizontal full blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the horizontal turbine (11G) has a total length of 1.5 m or less with two integrated cast turbine blade groups (8G) and a horizontal axis (16A).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as two cast parts and has a total length of 2 m or less, and is a horizontal full blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as two cast parts and has a total length of 2.5 m or less, and is a horizontal full blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, including a horizontal all-blade steam water gravity turbine (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 3 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as two cast parts and has a total length of 3,5 m or less, and is a horizontal full-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal turbine blade (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 4 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as two cast parts and has a total length of 4,5 m or less, and is a horizontal full-blade steam water gravity turbine (11X)
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal turbine blade (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 5 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as two cast parts and has a total length of 5,5 m or less, and is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods with a horizontal all-blade steam-water gravity turbine (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 6 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal axis (16A) as two cast parts and has a total length of 6 m or more, and is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) and the horizontal shaft (16A) are three cast parts and the total length is 1.5 m or less, and is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 2 m or less, and is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal all-blade steam water gravity turbine (11X) with a total length of 2.5 m or less using three integral parts of an integrated turbine blade group (8G) horizontal axis (16A).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 3 m or less, and is a horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 3,5 m or less, and is a horizontal full blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which an integrated turbine blade group (8G) and a horizontal shaft (16A) are three cast parts and the total length is 4 m or less, and a horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal turbine blade (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and a total length of 4,5 m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal all-blade steam water gravity turbine (11X) with a total length of 5 m or less using three integral parts of the integrated turbine blade group (8G) horizontal axis (16A).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal all-blade steam-water gravity turbine (11X) with an integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and a total length of 5,5 m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which an integrated turbine blade group (8G) and a horizontal shaft (16A) are three cast parts and the total length is 6 m or less, and a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, including an integral turbine blade group (8G) and a horizontal shaft (16A) as three cast parts and a total length of 6 m or more, and a horizontal full-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part and the total length is 1.5 m or less and machined with a counter-rotating engine lathe (10C) to obtain a horizontal all-blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 2m or less, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 2,5 m or less, machined with a counter-rotating engine lathe (10C) to obtain a horizontal all-blade steam water gravity turbine (11X) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 3 m or less, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part and the total length is 3.5 m or less and machined with a counter-rotating engine lathe (10C) to make a horizontal all-blade steam water gravity turbine (11X) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 4m or less, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less and machined with counter-rotating engine lathe (10C) to make a horizontal all blade steam water gravity turbine (11X) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 5 m or less, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) horizontal shaft (16A) as a single cast part and processed with a counter rotating machine lathe (10C) with a total length of 5,5 m or less to form a horizontal full blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 6m or less, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 6m or more, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 1.5 m or less, machined with a counter-rotating engine lathe (10C) to make a horizontal all blade steam water gravity turbine (11X) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machined with counter-rotating engine lathe (10C) and various energies to make a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 2,5 m or less, machined with a counter-rotating engine lathe (10C) to make a horizontal all blade steam water gravity turbine (11X) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various turbine energies (8G) Horizontal shaft (16A) with two cast parts and a total length of 3m or less, machined with a counter-rotating engine lathe (10C) to produce a horizontal all-blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) with a horizontal axis (16A) as two cast parts and a total length of 3,5 m or less, machined with a counter rotating engine lathe (10C), to obtain a horizontal all blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various turbine energies (8G) Horizontal shaft (16A) with two cast parts and a total length of 4m or less, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) horizontal shaft (16A) with two cast parts and a total length of 4,5 m or less, machined with a counter-rotating engine lathe (10C), to obtain a horizontal all-blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various turbine energies (8G) Horizontal shaft (16A) with two cast parts and a total length of 5m or less, machined with a counter-rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 5,5 m or less, machined with a counter-rotating engine lathe (10C) to make a horizontal all-blade steam water gravity turbine (11X) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 6m or less, machined with a counter-rotating engine lathe (10C) to produce a horizontal all-blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 6m or more and machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) with a horizontal axis (16A) as three cast parts and a total length of 1.5 m or less and machined with a counter-rotating engine lathe (10C) to produce a horizontal all-blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and total length of 2m or less, machined with counter rotating engine lathe (10C) to make horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) with a horizontal axis (16A) as three cast parts and a total length of 2.5 m or less and machined with a counter-rotating engine lathe (10C) to obtain a horizontal all-blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machined with counter-rotating engine lathe (10C), and various energies to make horizontal all-blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) with a horizontal axis (16A) as three cast parts and a total length of 3,5 m or less and processed with a counter rotating lathe (10C) to form a horizontal all blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machined with counter-rotating engine lathe (10C) to make horizontal all-blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) with a horizontal axis (16A) as three cast parts and a total length of 4,5 m or less and machined with a counter rotating engine lathe (10C) to obtain a horizontal all blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machined with counter-rotating engine lathe (10C), and various energies made into a horizontal all-blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
An integrated turbine blade group (8G) horizontal shaft (16A) with three cast parts and a total length of 5,5 m or less was machined with a counter rotating engine lathe (10C) to obtain a horizontal all blade steam water gravity turbine (11X). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machined with counter-rotating engine lathe (10C) and various energies to make a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 6m or more, machined with a counter rotating engine lathe (10C) to produce a horizontal all blade steam water gravity turbine (11X) Storage cycle coalescence engine and coalescence method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 1.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 2 m or less, processed by a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G), and a horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 3 m or less, machined with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G), and a horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 3,5 m or less, machined with a counter-rotating engine lathe (10C) and a turbine blade grinding machine (10G), and a horizontal full blade Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 4 m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 4,5 m or less, machined with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G), and a horizontal all blade Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal axis (16A) as one cast part, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 5,5m or less, machined with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G) to create a horizontal all blade Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 6m or more, processed by a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G), and a horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 1.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2.5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 3 m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 3.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4m or less, machined with counter rotating engine lathe (10C) and turbine blade grinder (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of less than 4,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 6m or more, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 1.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2.5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 3,5 m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and total length of 4,5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 6m or more, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade steam water Various energy storage cycle coalescence engine and coalescence method as a gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy conservation cycle coalescing engines and coalescence methods, which are obtained by using a horizontal all-blade steam-water gravity turbine (11X) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method for a horizontal full blade steam water gravity turbine (11X) that is held and adjusted with a lathe (10C) for ultra-high speed balance.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding Ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, and making a horizontal full blade steam water gravity turbine (11X) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various types of energy conservation cycle coalescence engine and coalescence using various magnetics to make a bearing (12C) with a bearing load close to 0 to form a horizontal all blade steam water gravity turbine (11X) Method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing blade steam water gravity that is held by a rotating engine lathe (10C) and is made of ultra-high-speed balance and processed by various magnetisms to make a bearing (12C) close to zero bearing load and vertically connected by a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal full-swing steam-water gravity turbine (4D) driven in series by the same rotating gear (4D), using a magnetic lathe (10C) and adjusting the ultra-high-speed balance and using various magnets to make a bearing (12C) close to zero bearing load. 11X) various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to the horizontal all-blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気水重力タービン(11X)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescing engine and coalescence method, which is a horizontal all blade steam water gravity turbine (11X).
内側出力翼群(53B)を1段として外側出力翼群(53A)を2段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) is one stage and the outer output blade group (53A) is two stages and a liquid oxygen producing machine (89A).
内側出力翼群(53B)を2段として外側出力翼群(53A)を3段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which the inner output blade group (53B) is in two stages and the outer output blade group (53A) is in three stages to form a liquid oxygen production machine (89A).
内側出力翼群(53B)を3段として外側出力翼群(53A)を4段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which the inner output blade group (53B) has three stages and the outer output blade group (53A) has four stages, and a liquid oxygen producing machine (89A).
内側出力翼群(53B)を4段として外側出力翼群(53A)を5段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has four stages and the outer output blade group (53A) has five stages and a liquid oxygen producing machine (89A).
内側出力翼群(53B)を5段として外側出力翼群(53A)を6段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which five stages of inner output blade groups (53B) and six stages of outer output blade groups (53A) are used as a liquid oxygen producing machine (89A).
内側出力翼群(53B)を6段として外側出力翼群(53A)を7段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods using six stages of inner output blade groups (53B) and seven stages of outer output blade groups (53A) as a liquid oxygen producing machine (89A).
内側出力翼群(53B)を7段として外側出力翼群(53A)を8段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has seven stages and the outer output blade group (53A) has eight stages, and a liquid oxygen producing machine (89A).
内側出力翼群(53B)を8段として外側出力翼群(53A)を9段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has eight stages and the outer output blade group (53A) has nine stages, and a liquid oxygen producing machine (89A).
内側出力翼群(53B)を9段として外側出力翼群(53A)を10段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which nine stages of inner output blade groups (53B) and ten stages of outer output blade groups (53A) are used as a liquid oxygen producing machine (89A).
内側出力翼群(53B)を10段として外側出力翼群(53A)を11段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which the inner output blade group (53B) has 10 stages and the outer output blade group (53A) has 11 stages, and is a liquid oxygen producing machine (89A).
内側出力翼群(53B)を11段として外側出力翼群(53A)を12段として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods using 11 stages of inner output blade groups (53B) and 12 stages of outer output blade groups (53A) as a liquid oxygen producing machine (89A).
内側出力翼群(53B)を1段として外側出力翼群(53A)を2段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a liquid oxygen production machine (89A) with the inner output blade group (53B) as one stage, the outer output blade group (53A) as two stages, and each stage as one casting part.
内側出力翼群(53B)を2段として外側出力翼群(53A)を3段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has two stages, the outer output blade group (53A) has three stages, and each stage has one casting part as a liquid oxygen production machine (89A).
内側出力翼群(53B)を3段として外側出力翼群(53A)を4段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which the inner output blade group (53B) has three stages, the outer output blade group (53A) has four stages, and each stage has one casting part as a liquid oxygen production machine (89A).
内側出力翼群(53B)を4段として外側出力翼群(53A)を5段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has four stages, the outer output blade group (53A) has five stages, and each stage has one casting part as a liquid oxygen production machine (89A).
内側出力翼群(53B)を5段として外側出力翼群(53A)を6段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has five stages, the outer output blade group (53A) has six stages, and each stage has one casting part as a liquid oxygen production machine (89A).
内側出力翼群(53B)を6段として外側出力翼群(53A)を7段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has six stages, the outer output blade group (53A) has seven stages, and each stage has one casting part as a liquid oxygen production machine (89A).
内側出力翼群(53B)を7段として外側出力翼群(53A)を8段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods using seven stages of inner output blade group (53B), eight stages of outer output blade group (53A), and each stage as one casting part as a liquid oxygen production machine (89A).
内側出力翼群(53B)を8段として外側出力翼群(53A)を9段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle merging engines and merging methods in which the inner output blade group (53B) has eight stages, the outer output blade group (53A) has nine stages, and each stage has one casting part as a liquid oxygen production machine (89A).
内側出力翼群(53B)を9段として外側出力翼群(53A)を10段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the inner output blade group (53B) is nine stages, the outer output blade group (53A) is ten stages, and each stage is one cast part, and a liquid oxygen production machine (89A).
内側出力翼群(53B)を10段として外側出力翼群(53A)を11段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods using a liquid oxygen production machine (89A) with 10 stages of the inner output blade group (53B), 11 stages of the outer output blade group (53A), and each stage as one casting part.
内側出力翼群(53B)を11段として外側出力翼群(53A)を12段として夫々の段を1鋳造部品として液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods in which the inner output blade group (53B) is 11 stages, the outer output blade group (53A) is 12 stages, and each stage is one cast part, and a liquid oxygen production machine (89A).
内側出力翼群(53B)を1段として外側出力翼群(53A)を2段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is one stage, the outer output blade group (53A) is two stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A) Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を2段として外側出力翼群(53A)を3段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
A liquid oxygen production machine (89A) by processing the inner output blade group (53B) in two stages, the outer output blade group (53A) in three stages, and processing each stage as a cast part with a counter rotating engine lathe (10C). Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を3段として外側出力翼群(53A)を4段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
A liquid oxygen producing machine (89A) is processed by a counter rotating engine lathe (10C) with three stages of the inner output blade group (53B) and four stages of the outer output blade group (53A) and one stage as a cast part. Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を4段として外側出力翼群(53A)を5段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has four stages, the outer output blade group (53A) has five stages, and each stage is processed as a cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A). Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を5段として外側出力翼群(53A)を6段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has five stages, the outer output blade group (53A) has six stages, and each stage is processed as a cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen producing machine (89A). Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を6段として外側出力翼群(53A)を7段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is six stages, the outer output blade group (53A) is seven stages, and each stage is processed as one casting part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A) Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を7段として外側出力翼群(53A)を8段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is seven stages, the outer output blade group (53A) is eight stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A) Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を8段として外側出力翼群(53A)を9段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is eight stages, the outer output blade group (53A) is nine stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A) Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を9段として外側出力翼群(53A)を10段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is nine stages, the outer output blade group (53A) is ten stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A) Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を10段として外側出力翼群(53A)を11段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 10 stages, the outer output blade group (53A) is 11 stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A) Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を11段として外側出力翼群(53A)を12段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 11 stages, the outer output blade group (53A) is 12 stages, and each stage is processed as a cast part on a counter rotating engine lathe (10C) to produce a liquid oxygen production machine (89A) Various energy storage cycle coalescence engines and coalescence methods.
内側出力翼群(53B)を1段として外側出力翼群(53A)を2段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is one stage, the outer output blade group (53A) is two stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を2段として外側出力翼群(53A)を3段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is two stages, the outer output blade group (53A) is three stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を3段として外側出力翼群(53A)を4段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is three stages, the outer output blade group (53A) is four stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を4段として外側出力翼群(53A)を5段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has four stages, the outer output blade group (53A) has five stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を5段として外側出力翼群(53A)を6段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is five stages, the outer output blade group (53A) is six stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を6段として外側出力翼群(53A)を7段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has six stages, the outer output blade group (53A) has seven stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を7段として外側出力翼群(53A)を8段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is seven stages, the outer output blade group (53A) is eight stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を8段として外側出力翼群(53A)を9段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 8 stages, the outer output blade group (53A) is 9 stages, and each stage is processed as one cast part with a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を9段として外側出力翼群(53A)を10段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 9 stages, the outer output blade group (53A) is 10 stages, and each stage is processed as one cast part on the counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を10段として外側出力翼群(53A)を11段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 10 stages, the outer output blade group (53A) is 11 stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を11段として外側出力翼群(53A)を12段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 11 stages, the outer output blade group (53A) is 12 stages, and each stage is processed as one cast part on the counter rotating engine lathe (10C) and output blade grinding machine (10E). Various energy storage cycle coalescing engines and coalescence methods for a liquid oxygen producing machine (89A).
内側出力翼群(53B)を1段として外側出力翼群(53A)を2段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is one stage, the outer output blade group (53A) is two stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を2段として外側出力翼群(53A)を3段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is two stages, the outer output blade group (53A) is three stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を3段として外側出力翼群(53A)を4段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is three stages, the outer output blade group (53A) is four stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を4段として外側出力翼群(53A)を5段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has four stages, the outer output blade group (53A) has five stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を5段として外側出力翼群(53A)を6段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is five stages, the outer output blade group (53A) is six stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を6段として外側出力翼群(53A)を7段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has six stages, the outer output blade group (53A) has seven stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を7段として外側出力翼群(53A)を8段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is seven stages, the outer output blade group (53A) is eight stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を8段として外側出力翼群(53A)を9段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 8 stages, the outer output blade group (53A) is 9 stages, and each stage is processed as one cast part with a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼 群(53B)を9段として外側出力翼群(53A)を10段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 9 stages, the outer output blade group (53A) is 10 stages, and each stage is processed as one cast part with a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を10段として外側出力翼群(53A)を11段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 10 stages, the outer output blade group (53A) is 11 stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を11段として外側出力翼群(53A)を12段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 11 stages, the outer output blade group (53A) is 12 stages, and each stage is processed as one cast part on the counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, each of the outer shaft device (60B) and the inner shaft device (60A) is temporarily assembled and held by a counter rotating engine lathe (10C) to adjust the ultra-high speed balance, thereby preparing a liquid oxygen production machine (89A). Cycle coalescence engine and coalescence method.
内側出力翼群(53B)を1段として外側出力翼群(53A)を2段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is one stage, the outer output blade group (53A) is two stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を2段として外側出力翼群(53A)を3段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is two stages, the outer output blade group (53A) is three stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を3段として外側出力翼群(53A)を4段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is three stages, the outer output blade group (53A) is four stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を4段として外側出力翼群(53A)を5段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has four stages, the outer output blade group (53A) has five stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を5段として外側出力翼群(53A)を6段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is five stages, the outer output blade group (53A) is six stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を6段として外側出力翼群(53A)を7段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has six stages, the outer output blade group (53A) has seven stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を7段として外側出力翼群(53A)を8段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is seven stages, the outer output blade group (53A) is eight stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を8段として外側出力翼群(53A)を9段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 8 stages, the outer output blade group (53A) is 9 stages, and each stage is processed as one cast part with a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を9段として外側出力翼群(53A)を10段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 9 stages, the outer output blade group (53A) is 10 stages, and each stage is processed as one cast part on the counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を10段として外側出力翼群(53A)を11段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 10 stages, the outer output blade group (53A) is 11 stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を11段として外側出力翼群(53A)を12段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転歯車装置(85Y)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 11 stages, the outer output blade group (53A) is 12 stages, and each stage is processed as one cast part on the counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating gear device (85Y).
内側出力翼群(53B)を1段として外側出力翼群(53A)を2段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is one stage, the outer output blade group (53A) is two stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を2段として外側出力翼群(53A)を3段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is two stages, the outer output blade group (53A) is three stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を3段として外側出力翼群(53A)を4段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is three stages, the outer output blade group (53A) is four stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を4段として外側出力翼群(53A)を5段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has four stages, the outer output blade group (53A) has five stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を5段として外側出力翼群(53A)を6段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is five stages, the outer output blade group (53A) is six stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を6段として外側出力翼群(53A)を7段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) has six stages, the outer output blade group (53A) has seven stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を7段として外側出力翼群(53A)を8段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is seven stages, the outer output blade group (53A) is eight stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を8段として外側出力翼群(53A)を9段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 8 stages, the outer output blade group (53A) is 9 stages, and each stage is processed as one cast part with a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を9段として外側出力翼群(53A)を10段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 9 stages, the outer output blade group (53A) is 10 stages, and each stage is processed as one cast part on the counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を10段として外側出力翼群(53A)を11段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 10 stages, the outer output blade group (53A) is 11 stages, and each stage is processed as one cast part on a counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
内側出力翼群(53B)を11段として外側出力翼群(53A)を12段として夫々の段を1鋳造部品として二重反転機関用旋盤(10C)と出力翼用研削盤(10E)で加工して外側軸装置(60B)内側軸装置(60A)夫々を仮組立して二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の外側軸装置(60B)内側軸装置(60A)を二重反転磁気装置(85)で水平連結駆動する液体酸素製造機(89A)とした各種エネルギ保存サイクル合体機関及び合体方法。
The inner output blade group (53B) is 11 stages, the outer output blade group (53A) is 12 stages, and each stage is processed as one cast part on the counter rotating engine lathe (10C) and output blade grinding machine (10E). Then, the outer shaft device (60B) and the inner shaft device (60A) are temporarily assembled, held by a counter rotating engine lathe (10C), and subjected to ultra-high-speed balance adjustment processing. (60B) Various energy storage cycle merging engines and merging methods in which the inner shaft device (60A) is a liquid oxygen producing machine (89A) that is horizontally coupled and driven by a counter-rotating magnetic device (85).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as one cast part and total length of 1.5m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as one cast part and total length of 2 m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11 W) with integral turbine blade group (8G) horizontal shaft (16A) as one cast part and total length of 2.5 m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as one cast part and total length of 3 m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as one cast part and total length of 3,5 m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) horizontal shaft (16A) is a cast part and the total length is 4 m or less, and the horizontal full-blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal turbine blade specific gravity gravity turbine (11 W) with an integral turbine blade group (8G) horizontal shaft (16A) as one cast part and a total length of 4,5 m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which an integral turbine blade group (8G) horizontal shaft (16A) is a cast part and a total length is 5 m or less and a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as one cast part and total length of 5,5m or less.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, including an integral turbine blade group (8G) and a horizontal axis (16A) as a single cast part and a total length of 6 m or less, and a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11 W) with integral turbine blade group (8G) horizontal shaft (16A) as one cast part and total length of 6m or more.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal full-blade steam ratio critical material gravity turbine (11 W) with an integral turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 1.5 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal axis (16A) as two cast parts and has a total length of 2 m or less and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11 W) with two integrated cast turbine blade groups (8G) horizontal shaft (16A) and a total length of 2.5 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal shaft (16A) as two cast parts and has a total length of 3 m or less, and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal full-blade steam ratio critical material gravity turbine (11 W) with an integral turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 3.5 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal axis (16A) as two cast parts and has a total length of 4 m or less, and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal full-blade steam ratio critical material gravity turbine (11W) with an integral turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 4,5 m or less.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal axis (16A) as two cast parts and has a total length of 5 m or less, and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, in which an integral turbine blade group (8G) horizontal shaft (16A) is used as two cast parts and the overall length is 5,5 m or less, and a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescing engines and coalescence methods, in which the integrated turbine blade group (8G) has a horizontal axis (16A) as two cast parts and has a total length of 6 m or less, and is a horizontal full-blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods with a turbine blade group (8G) horizontal shaft (16A) as two cast parts and a total length of 6 m or more, and a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and total length of 1.5m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and total length of 2 m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal full-blade steam ratio critical material gravity turbine (11W) with an integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and a total length of 2.5 m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 3 m or less and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal full-blade steam ratio critical material gravity turbine (11W) with an integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and a total length of 3,5 m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 4 m or less, and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using horizontal turbine blade specific gravity gravity turbine (11W) with integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and total length of 4,5m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 5 m or less and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engine and coalescence method using a horizontal turbine blade specific ratio gravity material gravity turbine (11 W) with an integral turbine blade group (8G) horizontal shaft (16A) as three cast parts and a total length of 5,5 m or less.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 6 m or less, and is a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Various energy storage cycle coalescence engines and coalescence methods, wherein the integrated turbine blade group (8G) has a horizontal shaft (16A) as three cast parts and has a total length of 6 m or more, and is a horizontal full-blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 1.5m or less and machined with a counter-rotating engine lathe (10C), horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 2 m or less and machined with a counter-rotating engine lathe (10C) to produce a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 2.5m or less and machined on a counter rotating engine lathe (10C), horizontal full blade constant ratio gravity material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 3 m or less and machined with a counter-rotating engine lathe (10C) to make a horizontal full blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 3,5 m or less and machined with a counter-rotating engine lathe (10C), horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 4 m or less and machined with a counter-rotating engine lathe (10C) to obtain a horizontal full-rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 4,5m or less and machined with a counter-rotating engine lathe (10C). Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 5 m or less and machined with a counter-rotating engine lathe (10C) to produce a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 5,5 m or less and machined on a counter rotating engine lathe (10C), and a horizontal full rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 6 m or less and machined with a counter-rotating engine lathe (10C) to make a horizontal full blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 6m or more and machined with a counter-rotating engine lathe (10C) to make a horizontal full blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 1.5m or less, machined with counter-rotating engine lathe (10C), horizontal type full blade constant ratio gravity material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 2 m or less and machined with a counter-rotating engine lathe (10C) to obtain a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2.5m or less, machined with counter-rotating engine lathe (10C), horizontal type full blade constant ratio gravity material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 3 m or less and machined with a counter-rotating engine lathe (10C) to make a horizontal full blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Combined turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 3.5m or less, machined with a counter-rotating engine lathe (10C), horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 4 m or less, machined with a counter-rotating engine lathe (10C) to make a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Combined turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, machined with counter-rotating engine lathe (10C), horizontal type full blade constant ratio gravity material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 5 m or less, machined with a counter-rotating engine lathe (10C) to make a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and total length of 5,5m or less, machined with counter-rotating engine lathe (10C), horizontal type full blade constant ratio gravity material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 6 m or less, machined with a counter-rotating engine lathe (10C), and made into a horizontal full rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 6m or more and machined with a counter-rotating engine lathe (10C) to obtain a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 1.5m or less, machined with counter-rotating engine lathe (10C), horizontal type full blade constant ratio gravity material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 2 m or less, machined with a counter-rotating engine lathe (10C) to make a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2.5m or less, machined with counter rotating engine lathe (10C), horizontal full rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 3 m or less, machined with a counter-rotating engine lathe (10C), and made into a horizontal full rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3,5m or less and machined with counter-rotating engine lathe (10C), horizontal type full blade constant ratio gravity material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 4 m or less, machined with a counter-rotating engine lathe (10C), and made into a horizontal full-rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and total length of 4,5m or less, machined with counter-rotating engine lathe (10C), horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 5m or less, machined with a counter-rotating engine lathe (10C), and made into a horizontal full rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less and machined with counter rotating machine lathe (10C), horizontal full rotor blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 6 m or less and machined with a counter-rotating engine lathe (10C) to make a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 6m or more and machined with a counter-rotating engine lathe (10C) to make a horizontal full-blade steam ratio critical material gravity turbine (11W) Various energy storage cycle coalescence engines and coalescence methods.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 1.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Combined turbine blade group (8G) with horizontal axis (16A) as one cast part and with a total length of 2 m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full rotor blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Combined turbine blade group (8G) with horizontal axis (16A) as one cast part and with a total length of 3m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full rotor blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 3,5 m or less, machined with a counter-rotating engine lathe (10C) and a turbine blade grinding machine (10G), and a horizontal full blade Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 4m or less, machined with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) to create a horizontal full blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, with a total length of 4,5 m or less, machined with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G), and a horizontal all blade Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Combined turbine blade group (8G) with horizontal axis (16A) as one cast part and with a total length of 5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full rotor blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 5,5m or less, machined with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G) to create a horizontal all blade Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) and horizontal full blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part and with a total length of 6m or more, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full rotor blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 1.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2.5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), and horizontal full blade constant gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of 3.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), and horizontal full-blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts and a total length of less than 4,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) and horizontal full blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), and horizontal full blade static gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 6m or more, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 1.5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2.5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and a total length of 3,5 m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal axis (16A) with 3 cast parts, total length of 4m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts and total length of 4,5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) and horizontal full blade steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method with steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machined with counter-rotating engine lathe (10C) and turbine blade grinding machine (10G), horizontal full blade constant steam specific gravity Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method as a large material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescing engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a turning engine lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W) by holding ultrahigh-speed balance adjustment processing on a lathe (10C).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Reversing engine lathe (10C) holding ultra high-speed balance adjustment processing, using various magnetism to make bearing (12C) close to zero bearing load, various energy storage cycle as horizontal full blade steam ratio critical material gravity turbine (11W) Merger engine and merger method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with a lathe (10C) Ultra high-speed balance adjustment processing Various magnetic storage, combined with a bearing (12C) approaching zero bearing load, a horizontal full blade steam ratio critical material gravity turbine (11W) And coalescing method.
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type rotor blade steam ratio is seriously controlled by using ultra-high-speed balance adjustment processing with a rotating engine lathe (10C) and using various magnetism to make a bearing (12C) close to a bearing load of 0 (vertical connection) with a series rotating gear (4D). Various energy storage cycle coalescence engine and coalescence method as a material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Horizontal type full-blade blade steam ratio critical material gravity that is driven by vertical connection with series rotating gear (4D) using bearings (12C) close to bearing load 0 by using various magnets and holding ultra-high-speed balance processing with lathe (10C) Various energy storage cycle coalescence engine and coalescence method as a turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 1.5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), and assembly into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 2.5 m or less, machining with double reversing engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 3m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as a single cast part, total length of 3, 5 m or less, processed with a counter rotating engine lathe (10C) and a turbine blade grinding machine (10G) and assembled into a double Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one casting part, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 4,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 5,5m or less, double-reversed engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or less, machining with a counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を1鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) as one cast part, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of less than 1,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 2,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 3,5m or less, machined by counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 2 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 4,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5m or less, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) are assembled and double-assembled Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G), assembled into a counter rotating engine Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を2鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with two cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を1,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 1,5m and machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 2m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を2,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 2,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 3m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を3,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) is 3 cast parts, total length is less than 3,5m, machined with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) and assembled into double Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を4,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 4,5m or less, machining with double turning engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を5,5m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 5,5m or less, double counter-rotating engine lathe (10C) and turbine blade grinding machine (10G) Super-high-speed balance adjustment processed by turning engine lathe (10C), using various magnetism to make bearing (12C) close to zero bearing load, driven oppositely by counter-synchronous gear (4C), and vertically driven by series co-rotating gear (4D) Various energy storage cycle coalescing engines and coalescence methods that are coupled to drive a horizontal all-blade steam ratio critical material gravity turbine (11 W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以下として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or less, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).
一体タービン翼群(8G)水平軸(16A)を3鋳造部品として全長を6m以上として二重反転機関用旋盤(10C)とタービン翼用研削盤(10G)で加工本組立てして二重反転機関用旋盤(10C)で保持超高速バランス調整加工して各種磁気利用し軸受荷重0接近の軸受(12C)にして対向同期歯車(4C)で対向駆動し直列同回転歯車(4D)で垂直連結駆動する横型全動翼蒸気比重大物質重力タービン(11W)とした各種エネルギ保存サイクル合体機関及び合体方法。
Integrated turbine blade group (8G) Horizontal shaft (16A) with 3 cast parts, total length of 6m or more, machining with counter rotating engine lathe (10C) and turbine blade grinding machine (10G) Holding with high speed lathe (10C), adjusting to ultra high speed balance, using various magnetism to make bearing (12C) close to zero bearing load, opposed driving with counter synchronous gear (4C), vertical driving with series rotating gear (4D) Various energy storage cycle coalescence engine and coalescence method using a horizontal full rotor blade steam ratio critical material gravity turbine (11W).