Claims (574)
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)と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 as a counter-rotating water-cooled blade compression counter-rotating engine (12G) having bearings (12C) at both ends and enabling temporary assembly processing.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の2段圧縮機(12N)と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 as a two-stage compressor (12N) of counter-rotating water-cooled blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転噴射機関(12E)と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 as a counter-rotating water-cooled blade-compressed counter-rotating injection engine (12E) having bearings (12C) at both ends and enabling temporary assembly processing.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転空気噴射機関(12F)と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 as a counter-rotating water-cooled blade compression counter-rotating air injection engine (12F) equipped with bearings (12C) at both ends to enable temporary assembly processing.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends to enable temporary assembly processing Various energy conservation cycle coalescing engines with a counter-rotating engine (12G) having a compression part as a two-stage compressor (12N) for counter-rotating water cooling blade compression And coalescing method.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転噴射機関(12E)と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 with various energy storage cycles with a counter-rotating injection engine (12E) having bearings (12C) at both ends to enable temporary assembly processing, and the compression part is a two-stage compressor (12N) of counter-rotating water cooling blade compression Organization and coalescence method.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転空気噴射機関(12F)と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 counter-rotating air injection engine (12F) with bearings (12C) at both ends and a compression section that is a two-stage compressor (12N) for counter-rotating water cooling blade compression that enables temporary assembly. Merger engine and merger method.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)と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 as a counter-rotating automobile (11B) equipped with a counter-rotating water cooling blade compression counter-rotating engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly processing .
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)と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 counter rotating water cooled blade compression counter rotating engine (12G) and counter rotating ship (11C) equipped with bearings (12C) at both ends and enabling temporary assembly processing .
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)と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 as a counter-rotating aircraft (11E) equipped with a counter rotating water cooling blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly processing .
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)と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 comprising a counter rotating engine (12G) with a counter rotating water cooled blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing, and a rotor blade airplane (11I).
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)と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 such as a counter rotating water-cooled blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and an Osprey extra large (11M).
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)と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 including a counter-rotating water-cooled blade compression counter-rotating injection engine (12E) and counter-rotating injection ship (11F) equipped with bearings (12C) at both ends and enabling temporary assembly processing; Merge method.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)と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 including a counter rotating water cooled blade compression counter rotating injection engine (12E) and counter rotating injection airplane (11G) equipped with bearings (12C) at both ends and enabling temporary assembly processing; Merge method.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 with a counter rotating water injection vane compression engine (12E) equipped with bearings (12C) at both ends and enabling temporary assembly processing, and a rotary blade injection airplane (11J) Method.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)と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 counter rotating water-cooled blade compression contra-rotating injection engine (12E) equipped with bearings (12C) at both ends and an Osprey large size (11N).
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)と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 equipped with counter-rotating water-cooled blade compression counter-rotating air injection engine (12F) and counter-rotating injection ship (11F) equipped with bearings (12C) at both ends to enable temporary assembly processing And coalescing method.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)と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 counter rotating engine (12G) of a counter rotating water cooling blade compressed with a bearing (12C) at both ends and enabling temporary assembly processing (12G), an outer compressing blade (8r) of cooling water (52a), an inner compressing blade (8q), and Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)に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 counter rotating engine (12G) of a counter rotating water cooling blade (12a) that is provided with bearings (12C) at both ends to enable provisional assembly processing, and a water (52a) cooling outer compression blade (8r) and an inner compressing blade (8q). Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engines and coalescence methods as wings (8r) inner compression wings (8q).
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engine and coalescence method for the blade (8r) inner compression blade (8q).
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends to enable provisional assembly processing. A counter rotating engine (12G) having a compression section made of a two-stage compressor (12N) for counter rotating water cooling blade compression. Counter rotating vehicle (11B) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends to enable temporary assembly processing. Provided with a counter-rotating engine (12G) having a compression section of a two-stage compressor (12N) for counter-rotating water cooling blade compression. Counter-rotating ship (11C) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends to enable provisional assembly processing. Compressed part is a two-stage compressor (12N) with a counter-rotating water cooling blade compression. A counter-rotating airplane (11E) is equipped with a counter-rotating engine (12G). Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)と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 rotary wing airplane (11I) equipped with a counter rotating engine (12G) having bearings (12C) at both ends and capable of temporary assembly processing and having a compression section as a two stage compressor (12N) of a counter rotating water cooled blade compression; Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends to enable provisional assembly processing The compression section is a double-reversed engine (12G) with a double-stage water-cooled blade compression two-stage compressor (12N) and an Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends to enable temporary assembly processing. A counter-rotating jet ship (12E) having a counter-rotating water-cooled blade compression two-stage compressor (12N). 11F) various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends to enable temporary assembly processing. A counter-rotating jet airplane (12E) having a counter-rotating water-cooled blade compression two-stage compressor (12N) having a counter-rotating jet engine (12E) 11G) various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends to enable temporary assembly processing. Rotating blade injection airplane (11J) equipped with counter rotating injection engine (12E) having a compression section made of a two-stage compressor (12N) of counter rotating water cooling blade compression. ) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey large size (11N) equipped with a counter-rotating injection engine (12E) having a bearing (12C) at both ends to enable temporary assembly processing and having a compression part as a two-stage compressor (12N) for counter-rotating water cooling blade compression; Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)と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 counter-rotating jet ship equipped with a counter-rotating air injection engine (12F) having bearings (12C) at both ends and capable of provisional assembly processing, and the compression part being a two-stage compressor (12N) of counter-rotating water cooling blade compression (11F) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼と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 counter-rotating water cooling blade compression counter rotating engine (12G) water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling provided with bearings (12C) at both ends to enable temporary assembly processing. Various energy storage cycle coalescence engines and coalescence methods as wings.
両端に軸受(12C)具備して仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼と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 counter-rotating water cooling blade compression counter rotating engine (12G) water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling provided with bearings (12C) at both ends to enable temporary assembly processing. Various energy storage cycle coalescence engines and coalescence methods as compression blades.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engine and coalescence method using a blade (8r) inner compression blade (8q) cooling blade.
両端に軸受(12C)具備して仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮の2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engine and coalescence method as a blade (8r) inner compression blade (8q) cooled compression blade.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転機関(12G)と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 with various energy storage cycles as a counter rotating engine (12G) for counter rotating water cooling blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing by annular inner compression blade (8q) screw assembly fixing etc. Organization and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水冷却翼圧縮の2段圧縮機(12N)と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 with various energy storage cycles as a two-stage compressor (12N) of counter-rotating water-cooled blades equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blades (8q) screw assembly fixing etc. Organization and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転噴射機関(12E)と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 as a counter-rotating water-cooled-blade-compressed counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Merger engine and merger method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水冷却翼圧縮の二重反転空気噴射機関(12F)と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 types of energy storage as a counter-rotating water-cooled-blade-compressed counter-rotating air injection engine (12F) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly and fixing. Cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an engine (12G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)と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 rotor (12G) with counter rotating water (52a) for cooling and compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and an annular inner compression blade (8q) screw assembly assembly fixed, etc. allows counter assembly water (52a) Cooling compression blade compression counter rotation engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by annular inner compression blade (8q) screw assembly and fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by annular inner compression blade (8q) screw assembly and fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter rotating water (52a) with a counter rotating injection engine (12E) equipped with bearings (12C) at both ends and enabling temporary assembly by an annular inner compressor blade (8q) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey equipped with a counter rotating water (52a) cooling compressor blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and a counter-rotating water (52a) with a counter-rotating air injection engine (12F) for cooling / compressing compressor blades, which can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)と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 counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)と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 counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)と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 counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal air having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversal water cooling blades of the compression section so that temporary assembly can be performed by assembling and fixing the annular inner compression blade (8q) screw. Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 types of counter-rotating engine (12G) for counter rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly by annular outer compression blade (8r) screw assembly and fixing. Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の2段圧縮機(12N)と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 types of counter-rotating water (52a) cooling compression blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and capable of temporary assembly by annular outer compression blade (8r) screw assembly and fixing Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 counter-rotating water (52a) is a counter-rotating injection engine (12E) for cooling compression blade compression that has bearings (12C) at both ends and can be temporarily assembled by an annular outer compression blade (8r) screw assembly and fixing. Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)と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 counter-rotating water (52a) counter-rotating air jet engine (12F) for compressing a cooling compressor blade, which has bearings (12C) at both ends and can be temporarily assembled by an annular outer compressor blade (8r) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an engine (12G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing compression blade reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing compression blade reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing compression blade reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)と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 rotor (12G) having a counter rotating engine (12G) for compressing and compressing compressed air that has bearings (12C) at both ends and is capable of temporary assembly by an annular outer compressor blade (8r) screw assembly and fixing. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and an annular outer compression blade (8r) screw assembly and fixing, enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)と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 counter rotating water (52a) with a bearing (12C) at both ends and an annular outer compression blade (8r) screw assembly fixing and the like enabling temporary assembly processing. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)と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 counter rotating water (52a) with a bearing (12C) at both ends and an annular outer compression blade (8r) screw assembly fixing and the like enabling temporary assembly processing. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter rotating water (52a) with a rotating reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular outer compression vane (8r) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey equipped with counter rotating water (52a) cooling compressor blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and a counter-rotating water (52a) cooling-compressing-blade compression counter-rotating air injection engine (12F) which can be temporarily assembled by an annular outer compressor blade (8r) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) equipped with a rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method with injection engine (12E) and large osprey (11N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy conservation cycle coalescing engines and coalescence methods, which are air injection engines (12F) and counter-rotating jets (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 types of counter-rotating engine (12G) with counter-rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly by annular outer output blade (8t) screw assembly fixing etc. Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の2段圧縮機(12N)と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 types of counter-rotating water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and capable of temporary assembly processing by annular outer output blade (8t) screw assembly and fixing Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 counter-rotating water (52a) is a counter-rotating injection engine (12E) for compressing compressed air compressors that has bearings (12C) at both ends and can be temporarily assembled by fixing the annular outer output blade (8t) with screws. Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)と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 counter-rotating water (52a) cooling-compressed-blade-compressed counter-rotating air injection engine (12F) having bearings (12C) at both ends and enabling temporary assembly by annular outer output blade (8t) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12G).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer output blade (8t) screw assembly fixing etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer output blade (8t) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer output blade (8t) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).
両端に軸受(12C)ぐびして環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Rotor blades equipped with counter rotating water (52a) cooling compression blade compression counter rotating engine (12G) with bearings (12C) squeezed at both ends to allow temporary assembly by annular outer output blade (8t) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), counter-rotating water (52a) with cooling / compressing blade compression counter-rotating engine (12G), enabling temporary assembly by screw assembly fixing Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular outer output blade (8t) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular outer output blade (8t) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter rotating water (52a) with a counter rotating injection engine (12E) for cooling and compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by an annular outer output blade (8t) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey with counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and enabling temporary assembly by annular outer output blade (8t) screw assembly and fixing Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and a counter-rotating water (52a) cooling-compressing-blade compression counter-rotating air injection engine (12F) that can be temporarily assembled by an annular outer output blade (8t) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Various energy storage cycle coalescing engines and coalescence methods that are cooling outer compressor blades (8r) and inner compressor blades (8q).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Various energy storage cycle coalescing engine and coalescence method with cooling outer compression blade (8r) inner compression blade (8q).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) as various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) equipped with a rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method with injection engine (12E) and large osprey (11N).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy conservation cycle coalescing engines and coalescence methods, which are air injection engines (12F) and counter-rotating jets (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method as cooling compression blade.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compression blades (8r) Inner compression blades (8q) Cooling blades Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 types of counter-rotating engine (12G) with counter-rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and capable of temporary assembly by annular inner output vane (8s) screw assembly fixing etc. Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の2段圧縮機(12N)と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 types of counter-rotating water (52a) cooling compression blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and capable of temporary assembly by annular inner output blade (8s) screw assembly fixing etc. Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 counter-rotating water (52a) is a counter-rotating injection engine (12E) for compression of compressed compression blades, which has bearings (12C) at both ends and can be temporarily assembled by an annular inner output blade (8s) screw assembly and fixing. Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)と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 counter-rotating water (52a) with a bearing (12C) at both ends and an annular inner output vane (8s) screw assembly fixing and the like, and a counter-rotating air injection engine (12F) for cooling compression blade compression; Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an engine (12G).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)と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 rotating blade with a counter rotating engine (12G) with a counter rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly by an annular inner output blade (8s) screw assembly and fixing. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and an annular inner output blade (8s) screw assembly and fixing, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)と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 counter rotating water (52a) having a bearing (12C) at both ends and enabling temporary assembly by an annular inner output blade (8s) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)と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 counter rotating water (52a) having a bearing (12C) at both ends and enabling temporary assembly by an annular inner output blade (8s) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter rotating water (52a) with a counter rotating injection engine (12E) equipped with a bearing (12C) at both ends and temporarily assembled by an annular inner output blade (8s) screw assembly and fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner output blades (8s) with counter-rotating water (52a) cooled and compressed blade compression counter-rotating injection engine (12E) capable of temporary assembly by screw assembly fixing etc. Osprey Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) that can be temporarily assembled by an annular inner output blade (8s) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Various energy storage cycle coalescing engines and coalescence methods that are cooling outer compressor blades (8r) and inner compressor blades (8q).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Various energy storage cycle coalescing engine and coalescence method with cooling outer compression blade (8r) inner compression blade (8q).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) as various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) equipped with a rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method with injection engine (12E) and large osprey (11N).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy conservation cycle coalescing engines and coalescence methods, which are air injection engines (12F) and counter-rotating jets (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method as cooling compression blade.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compression blades (8r) Inner compression blades (8q) Cooling blades Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 as a counter-rotating engine (12G) for counter-rotating water (52a) cooling compressor blade compression with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q) Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の2段圧縮機(12N)と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 as a double-reversed water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner compressor blade (8q) Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 types of counter-rotating water (52a) cooled counter-rotating jet compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing an annular inner compressor blade (8q) Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)と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 counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for compressing compressed compressor blades, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing the annular inner compressor blade (8q). Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)と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 counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating air having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q). Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method for automobile (11B).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Rotating wing airplane equipped with bearings (12C) at both ends and counter-reversing water (52a) cooling-compressing wing compression counter-rotating engine (12G), which can be temporarily assembled by inserting and fixing an annular inner compression wing (8q) (11I) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) Cooling compression blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner compression blade (8q) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing annular inner compression blades (8q) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing annular inner compression blades (8q) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Rotating blades equipped with counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey large size equipped with bearing (12C) at both ends and counter-inverted water (52a) cooling-compressed-blade-compressed counter-rotating injection engine (12E) capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q) (11N) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q). Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)と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 counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)と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 counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)と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 counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)と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 counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)と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 counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)と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 counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods for a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)と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 counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods, including a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor bladed airplanes (11J).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)と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 counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods, each having a large osprey large size (11N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)と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 counter-rotating air jet having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression part that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). Various energy storage cycle coalescing engine and coalescence method as an engine (12F) equipped counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 as a counter rotating water (52a) counter rotating engine (12G) for cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer compression blade (8r). Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の2段圧縮機(12N)と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 as a double-reversed water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compressor blade (8r) Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing an annular outer compression blade (8r). Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)と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 counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer compression blade (8r). Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)と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 counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating air having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular outer compression blade (8r) fitted and fixed, etc., enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Various energy storage cycle coalescence engine and coalescence method for automobile (11B).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular outer compression blade (8r) fitted and fixed, etc., enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular outer compression blade (8r) fitted and fixed, etc., enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Rotating wing airplane equipped with bearing (12C) at both ends and counter-reversing water (52a) cooling compression-blade compression counter-rotating engine (12G) that can be temporarily assembled by inserting and fixing the annular outer compression wing (8r) (11I) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) Cooling compression blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compression blade (8r) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compression blade (8r) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Rotating blades equipped with counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing annular outer compression blades (8r) Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey large size equipped with bearings (12C) at both ends and counter-reversing water (52a) cooling-compressed-blade compression counter-rotating injection engine (12E) that enables temporary assembly by inserting and fixing the annular outer compression blade (8r) (11N) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing an annular outer compressor blade (8r) Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)と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 counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)と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 counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)と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 counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)と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 counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)と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 counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating air having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 as a counter-rotating engine (12G) of counter-rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing by inserting and fixing the annular outer output vane (8t). Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の2段圧縮機(12N)と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 as a double-reversed water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 types of counter rotating water (52a) cooling compression blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing an annular outer output blade (8t). Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)と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 counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for cooling / compressing blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer output blade (8t). Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating air with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that enables temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular outer output blade (8t) fitted and fixed, etc., with counter-rotating water (52a), cooling-compressed blade compression counter-rotating engine (12G), counter-rotating Various energy storage cycle coalescence engine and coalescence method for automobile (11B).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular outer output blade (8t) fitted and fixed, etc., with counter-rotating water (52a), cooling-compressed blade compression counter-rotating engine (12G), counter-rotating Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular outer output blade (8t) fitted and fixed, etc., with counter-rotating water (52a), cooling-compressed blade compression counter-rotating engine (12G), counter-rotating Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).
両端に軸受(12C)ぐびして環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Rotor plane equipped with counter rotating water (52a) cooling compression blade compression counter rotating engine (12G) that can be temporarily assembled by, for example, bearings (12C) squeezed at both ends and annular outer output blades (8t) fitted and fixed. (11I) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) Cooling compression blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Rotating blades equipped with a counter rotating water engine (12E) with a counter rotating water (52a) cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey large size equipped with bearing (12C) at both ends and counter-reversing water (52a) cooled and compressed blade compression counter-rotating injection engine (12E) that can be temporarily assembled by inserting and fixing annular outer output blade (8t) (11N) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing an annular outer output blade (8t), etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods including water (52a) cooled outer compressor blades (8r) and inner compressor blades (8q).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)に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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescing methods in which water (52a) is cooled as an outer compressor blade (8r) and an inner compressor blade (8q).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)と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 counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating air with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that enables temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling blades.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling compression blades.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Water (52a) Cooling outer compressor blades (8r) Inner compressor blades (8q) Cooling blades and various energy storage cycle coalescing engines and coalescence methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Water (52a) Cooled outer compressor blade (8r) Inner compressor blade (8q) Cooled compressor blade and various energy storage cycle coalescing engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 as a counter-rotating engine (12G) for counter-rotating water (52a) cooling compression blade compression with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner output vane (8s) Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の2段圧縮機(12N)と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 as a double-reversed water (52a) cooling compression blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and enabling temporary assembly processing by inserting and fixing the annular inner output blade (8s) Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 types of counter-rotating injection engine (12E) for counter-rotating water (52a) cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing the annular inner output vane (8s). Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)と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 counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for cooling / compressing blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular inner output blade (8s). Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating air with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blades for compression by enabling the temporary assembly by fitting the annular inner output blade (8s) into place. Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular inner output blade (8s) fitted and fixed, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) and counter rotating Various energy storage cycle coalescence engine and coalescence method for automobile (11B).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular inner output blade (8s) fitted and fixed, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) and counter rotating Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends and an annular inner output blade (8s) fitted and fixed, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) and counter rotating Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)と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 rotating wing airplane equipped with bearings (12C) at both ends and a counter rotating water (52a) cooling compression blade compression counter rotating engine (12G) capable of temporary assembly by inserting and fixing an annular inner output blade (8s). (11I) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) Cooling compression blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner output blade (8s) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner output blade (8s) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)と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 rotating blade with a counter rotating water engine (12E) with a counter rotating water (52a) cooling compression blade compression, which has a bearing (12C) at both ends and can be temporarily assembled by inserting and fixing an annular inner output blade (8s). Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Osprey large size equipped with bearing (12C) at both ends and counter-inverted water (52a) cooled compression compression blade compression counter-rotating injection engine (12E) that can be temporarily assembled by inserting and fixing the annular inner output blade (8s) (11N) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing an annular inner output blade (8s), etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods including water (52a) cooled outer compressor blades (8r) and inner compressor blades (8q).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)に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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescing methods in which water (52a) is cooled as an outer compressor blade (8r) and an inner compressor blade (8q).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)と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 counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating air with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blades for compression by enabling the temporary assembly by fitting the annular inner output blade (8s) into place. Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling blades.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工を可能にした二重反転水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling compression blades.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼と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 counter-rotating engine (12N) having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that can be temporarily assembled by fitting and fixing the annular inner output blade (8s). 12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling blade, various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼と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 counter-rotating engine (12N) having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that can be temporarily assembled by fitting and fixing the annular inner output blade (8s). 12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade and various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)と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 bearings (12C) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool (52a). Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling blade compression two-stage compressor (12N) with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine. Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)と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 bearing (12C) is provided at both ends, and the water (52a) cooled and compressed blade-compressed counter-rotating injection engine (12E) is disassembled after confirming that both ends are held by a temporary assembly machine tool and the ultra-high speed rotation balance processing is good. Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled and compressed blade compression counter-rotating air injection engine (12F) equipped with bearings (12C) at both ends and disassembled after confirming the goodness of both ends holding ultra-high speed rotation balance processing with a temporary assembly machine tool; Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating injection engine (12E).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating engine (12G) Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating engine (12G) Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating engine (12G) Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blade compression counter-rotating engine (12G) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearing (12C) at both ends and temporary assembly machine tool with both ends held Ultra high speed rotation balance processing disassembled after confirmation of good processing (52a) Cooling compression blade compression counter rotating engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, and water (52a) cooled and compressed blade-compressed counter-rotating injection engine (12E) is provided after disassembling after temporarily confirming that both ends are held by a temporary assembly machine tool. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, and water (52a) cooled and compressed blade-compressed counter-rotating injection engine (12E) is provided after disassembling after temporarily confirming that both ends are held by a temporary assembly machine tool. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) on both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating injection engine (12E) equipped and rotated Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, both ends held by a temporary assembly machine tool, and disassembled after confirmation of good balance processing at ultra high speed rotation (52a) Cooling compression blade compression counter-rotating injection engine (12E) Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool (52a) and a counter-rotating air injection engine (12F) with cooling compression blade compression Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Various energy storage cycle coalescing engines and coalescence methods that are cooling outer compressor blades (8r) and inner compressor blades (8q).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Various energy storage cycle coalescing engine and coalescence method with cooling outer compression blade (8r) inner compression blade (8q).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method comprising a counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engines and coalescence methods for a counter rotating engine (12G) and a counter rotating automobile (11B).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating engine (12G) and a contra-rotating ship (11C).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating engine (12G) and a contra-rotating airplane (11E).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating engine (12G) equipped rotor blade airplane (11I).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engines and coalescence methods, including a counter rotating engine (12G) and an Osprey extra large (11M).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet ship (11F).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engines and coalescence methods, including a contra-rotating jet engine (12E) and a contra-rotating jet airplane (11G).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy conservation cycle coalescing engines and coalescence methods, including a counter-rotating jet engine (12E) and a rotary blade jet airplane (11J).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method with counter rotating injection engine (12E) and Osprey large size (11N).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method as cooling compression blade.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade.
両端に軸受(12C)具備して仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling blade compression that is disassembled after both bearings (12C) are provided at both ends, the inner assembly blades (8q) are assembled and fixed at the temporary assembly machine tool, etc. Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high speed rotation balance processing with a temporary assembly machine tool by fixing the annular inner compression blade (8q) screw, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立て加工可能に圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is supported at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and compress the compression part so that it can be assembled Various energy storage cycle coalescence engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses water-cooled blades.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling blade compression that is disassembled after the bearings (12C) are provided at both ends, the outer outer blades (8r) are assembled and fixed at the temporary assembly machine tool, etc., and the assembly is disassembled after confirming that both ends are super-high-speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) as a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling blade compression that was disassembled after the bearings (12C) were provided at both ends, the outer assembly of the annular outer output blade (8t) was screwed and fixed, etc. Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)ぐびして環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades disassembled into a main assembly after confirming that both ends have a bearing (12C) squeeze and an annular outer output blade (8t) screw assembly assembly and the like are temporarily assembled, and both ends are held and ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G), water (52a), a cooling outer compression blade (8r), and an inner compression blade (8q).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Compressed counter rotating engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method using a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles with a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) as a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engines and coalescence methods comprising a compression counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooling blade.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including compression counter-rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade.
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for blade compression .
両端に軸受(12C)具備して環状外側出力翼(8t)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and combination of various energy storage cycles as a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade with a two-stage compressor (12N) for blade compression Method.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearing (12C) at both ends, annular inner output blade (8s) screw assembly fixed, etc. Temporary assembly machine tool supported by both ends Ultra-high speed rotation Balance processing was confirmed after being disassembled and finally assembled water (52a) Cooling blade compression Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G), water (52a), a cooling outer compression blade (8r), and an inner compression blade (8q).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Compressed counter rotating engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method using a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles with a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) as a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engines and coalescence methods comprising a compression counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooling blade.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including compression counter-rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade.
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for blade compression .
両端に軸受(12C)具備して環状内側出力翼(8s)螺子組立固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and combination of various energy storage cycles as a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade with a two-stage compressor (12N) for blade compression Method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner compression blades (8q) fitted and fixed, etc. Temporary assembly machine tool is used for both-end holding ultra-high speed rotation balance processing and after disassembling the water (52a) cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) and non-reversing motor vehicle (11B).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状内側圧縮翼(8q)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearing (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool, both ends held after ultra-high speed rotation balance processing confirmed to be disassembled and finally assembled into water (52a) cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing engine (12G) and non-reversing motor vehicle (11B).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状外側圧縮翼(8r)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) provided at both ends, annular outer output blades (8t) fitted and fixed, etc. Temporary assembly machine tool confirmed that both ends are held and the high-speed rotation balance processing is confirmed, and then disassembled into the main assembly (52a) for cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) and non-reversing motor vehicle (11B).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).
両端に軸受(12C)ぐびして環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression disassembled after the bearing (12C) squeezed at both ends and disassembled after confirming that both ends are held at the high-speed rotation balance with a temporary assembly machine tool by fixing the annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engines and coalescence methods comprising a counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Combined engine and method for combining various energy storage cycles into a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Cooling blade
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状外側出力翼(8t)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Rotating compressor (12G) water reversing engine (12a) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade combined with various energy storage cycle engines and coalescence method .
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却翼圧縮の2段圧縮機(12N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearing (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is used for both-end holding Ultra-high speed rotation Balance processing is disassembled after confirming good processing (52a) cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) and non-reversing motor vehicle (11B).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engines and coalescence methods comprising a counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)にした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Combined engine and method for combining various energy storage cycles into a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転自動車(11B)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転船舶(11C)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備二重反転飛行機(11E)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備回転翼飛行機(11I)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)具備オスプレイ特大(11M)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備二重反転噴射飛行機(11G)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備回転翼噴射飛行機(11J)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転噴射機関(12E)具備オスプレイ大型(11N)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転空気噴射機関(12F)具備二重反転噴射船舶(11F)とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Cooling blade
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for compression.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Rotating compressor (12G) water reversing engine (12a) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade combined with various energy storage cycle engines and coalescence method .
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)吸入空気に太陽光加熱器(21)加熱の空気(28a)使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various reversible engine (12G) using solar heater (21) heated air (28a) as intake air and water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling energy Storage cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)吸入空気に太陽光加熱器(21)加熱の空気(28a)使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various reversing engines (12G) using solar heater (21) heated air (28a) for intake air, water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling compression blade Energy conservation cycle coalescence engine and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)吸入空気に太陽光加熱器(21)加熱の空気(28a)使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A double reversing engine (12G) made into a two-stage compressor (12N) for compression uses solar air heater (21) heated air (28a) for intake air, water (52a) cooling outer compression blade (8r) inner compression Various energy storage cycle coalescence engine and coalescence method using blade (8q) cooling blade.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)吸入空気に太陽光加熱器(21)加熱の空気(28a)使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A double reversing engine (12G) made into a two-stage compressor (12N) for compression uses solar air heater (21) heated air (28a) for intake air, water (52a) cooling outer compression blade (8r) inner compression Various energy storage cycle coalescing engine and coalescence method using a blade (8q) cooled compression blade.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)吸入空気に排気で加熱した空気(28a)を使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) using air (28a) heated by exhaust gas as intake air, water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling blade combined with various energy storage cycle combined engines And coalescing method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てにした水(52a)冷却圧縮翼圧縮の二重反転機関(12G)吸入空気に排気で加熱した空気(28a)を使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Combined with various energy storage cycles using the air (28a) heated by exhaust as the intake air of the counter-rotating engine (12G) of water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade Organization and coalescence method.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)吸入空気に排気で加熱した空気(28a)を使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A counter-rotating engine (12G) made of a two-stage compressor (12N) for compression uses air (28a) heated by exhaust as intake air and water (52a) cooling outer compression blade (8r) inner compression blade (8q) Various energy storage cycle coalescence engines and coalescence methods as cooling blades.
両端に軸受(12C)具備して環状内側出力翼(8s)嵌め込み固定等で仮組立工作機械で両端保持超高速回転バランス加工良好確認後に分解して本組立てに圧縮部を二重反転水冷却翼圧縮する2段圧縮機(12N)にした二重反転機関(12G)吸入空気に排気で加熱した空気(28a)を使用し水(52a)冷却の外側圧縮翼(8r)内側圧縮翼(8q)冷却圧縮翼とした各種エネルギ保存サイクル合体機関及び合体方法。
Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A counter-rotating engine (12G) made of a two-stage compressor (12N) for compression uses air (28a) heated by exhaust as intake air and water (52a) cooling outer compression blade (8r) inner compression blade (8q) Various energy storage cycle coalescence engines and coalescence methods as cooling compression blades.