CN106640215A - 一种空心叶片冷却介质节流孔板的配置结构及其装配方法 - Google Patents

一种空心叶片冷却介质节流孔板的配置结构及其装配方法 Download PDF

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CN106640215A
CN106640215A CN201611212456.XA CN201611212456A CN106640215A CN 106640215 A CN106640215 A CN 106640215A CN 201611212456 A CN201611212456 A CN 201611212456A CN 106640215 A CN106640215 A CN 106640215A
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China
Prior art keywords
orifice plate
locking key
cooling medium
fitting recess
blade
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Pending
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CN201611212456.XA
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English (en)
Inventor
赵仕志
刘维兵
艾松
范小平
周洪宇
方宇
赵世全
张晓东
孙奇
成露
陈贝贝
陈晓平
饶真炎
祁乃斌
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DEC Dongfang Turbine Co Ltd
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DEC Dongfang Turbine Co Ltd
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Priority to CN201611212456.XA priority Critical patent/CN106640215A/zh
Publication of CN106640215A publication Critical patent/CN106640215A/zh
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

本发明公开一种空心叶片冷却介质节流孔板的配置结构,所述空心叶片通过其叶根装在叶轮的轮槽中,所述轮槽具有冷却介质输入通道,所述空心叶片的冷却介质入口设在叶根底面,与轮槽的冷却介质输入通道相对应,在空心叶片的冷却介质入口设有节流孔板,用于限定冷却介质流量;所述孔板采用装配方式配置在叶根与轮槽的结合部,并采用锁键将孔板限位锁定。

Description

一种空心叶片冷却介质节流孔板的配置结构及其装配方法
技术领域
本发明涉及高温透平(涡轮)空心叶片,具体涉及该空心叶片冷却介质节流孔板的配置结构及其装配方法。
背景技术
空心叶片是地面燃气轮机和航空发动机的核心部件,由于工作温度很高,要通入冷却介质进行冷却,在转子主轴和叶轮上设有冷却介质通道,经叶根通往叶片腹腔,叶片的冷却介质进口设在叶根底面上,该进口配有节流孔板,由孔板的通流面积来限定冷却介质流量,使叶片的工作温度稳定在设计值。
以往,该孔板的配置结构是将孔板直接焊接在叶根底面上,该结构存在的问题是,在确定空心叶片冷却介质流量时,理论计算只能得到粗略值,还需模拟叶片工况,通过试验手段才能获得冷却介质流量的精确值。也就是说,孔板的通流面积无法预先确定,需要在实验过程中不断修改,通常需要多次修改才能找到符合叶片工作温度的冷却介质流量值,这就需要反复地焊接、切割孔板,费工费时,工作效率很低,且容易损伤孔板和叶片,导致实验数据精度下降,冷却介质流量不精确。
发明内容
针对以上问题,本发明提供一种空心叶片冷却介质节流孔板的配置结构及其装配方法,其技术解决方案是:
一种空心叶片冷却介质节流孔板的配置结构,所述空心叶片通过其叶根装在叶轮的轮槽中,所述叶轮具有冷却介质输入通道,所述空心叶片的冷却介质入口设在叶根底面,与叶轮的冷却介质输入通道相对应,在空心叶片的冷却介质入口设有节流孔板,用于限定冷却介质流量;其特征在于,所述孔板采用装配方式配置在叶根与轮槽的结合部,并采用锁键将孔板限位锁定;所述叶根底面设有孔板装配槽和锁键装配槽,所述孔板装配槽是轴向水平开口槽,开口位于叶根的一侧,孔板从该开口装入其装配槽内,与叶根装入叶轮轮槽的方向一致;所述孔板的底面上有一个凸台,位于节流孔板的轴向中分线上,凸台的左端面与孔板的左端面齐平;所述锁键的左端面底部有一左伸凸台,该左伸凸台的竖直高度等于节流孔板上的凸台高度,所述孔板的右部底面坐落在锁键的凸台上;所述孔板、锁键组合后,通过孔板、锁键的凸台坐落在叶轮轮槽内;所述锁键装配槽位于叶根的右部,锁键的左壁面与孔板的右端面齐平,该槽是径向竖直开口槽,槽口在下,锁键由下向上装进其装配槽内;当锁键装配到位后,其左端面与孔板的右端面对齐接触,将孔板限位锁定,使孔板不会从轮槽中窜出,并将孔板装配槽的开口封堵,起密封作用,避免冷却介质从孔板装配槽的开口泄出。
上述空心叶片冷却介质节流孔板的装配方法,包括步骤:
A、先把孔板装入其装配槽内;
B、再把叶片的叶根连同孔板一起从右向左推进叶轮的轮槽,不推到位,留出锁键的安装操作空间;
C、将锁键装进其装配槽内;
D、继续把叶片的叶根连同节流孔板、锁键一并推进叶轮的轮槽,直至到位。
本发明的有益效果:
由于孔板采用装配结构,拆装方便,节省试验时间,提高试验工效,并避免了因反复焊接损伤孔板和叶根,导致其变形,确保实验数据精确、真实可靠。
附图说明
图1是本发明的孔板结构图
图2是本发明的锁键结构图
图3是本发明的叶根结构图
图4至图7是本发明的孔板、锁键装配过程示意图。
具体实施方式
参见图1、图2、图3、图4至图7:本空心叶片冷却介质节流孔板的配置结构,所述空心叶片通过其叶根3装在叶轮4的轮槽中,所述叶轮4具有冷却介质输入通道,所述空心叶片的冷却介质入口设在叶根底面,与叶轮4的冷却介质输入通道相对应,在空心叶片的冷却介质入口设有节流孔板1,用于限定冷却介质流量。所述孔板1采用装配方式配置在叶根3与叶轮4轮槽的结合部,并采用锁键2将孔板1限位锁定。所述叶根3底面设有孔板装配槽3-2和锁键装配槽3-1,所述孔板装配槽3-2是轴向水平开口槽,开口位于叶根3的右侧,孔板1从右向左装入其装配槽3-2内,与叶根3装入叶轮4轮槽的方向一致;所述孔板1的中央有节流孔1-1,底面上有一个凸台1-2,位于孔板1的轴向中分线上,凸台1-2的左端面与孔板1的左端面齐平;所述锁键2的左端面底部有一左伸凸台2-1,该左伸凸台2-1的竖直高度等于孔板1上的凸台1-2高度,所述孔板1的右部底面坐落在锁键2的凸台2-1上;所述孔板1、锁键2组合后,通过它们的凸台1-2、2-1坐落在叶轮4的轮槽内;所述锁键装配槽3-1位于叶根3的右部,它的左壁面与孔板1的右端面齐平,该锁键装配槽3-1是径向竖直开口槽,槽口在下,锁键2由下向上装进其装配槽3-1内;当锁键2装配到位后,其左端面与孔板1的由端面接触,将孔板1限位锁定,使孔板1不会从叶轮4的轮槽中窜出,并将孔板装配槽3-2的开口封堵,起密封作用,避免冷却介质从孔板装配槽3-2的开口泄出。
上述空心叶片冷却介质节流孔板的装配方法,参见图4至图7,包括如下步骤:
A、先把孔板1装入其装配槽3-2内,如图4所示;
B、再把叶片的叶根3连同孔板1一起推进叶轮4的轮槽,不推到位,留出锁键2的安装操作空间,如图5所示;
C、将锁键2装进其装配槽3-1内,如图6所示;
D、继续把叶片的叶根3连同节流孔板1、锁键2一并推进叶轮4的轮槽,直至到位,如图7所示。

Claims (2)

1.一种空心叶片冷却介质节流孔板的配置结构,所述空心叶片通过其叶根装在叶轮的轮槽中,所述叶轮具有冷却介质输入通道,所述空心叶片的冷却介质入口设在叶根底面,与叶轮的冷却介质输入通道相对应,在空心叶片的冷却介质入口设有节流孔板,用于限定冷却介质流量;其特征在于,所述孔板采用装配方式配置在叶根与轮槽的结合部,并采用锁键将孔板限位锁定;所述叶根底面设有孔板装配槽和锁键装配槽,所述孔板装配槽是轴向水平开口槽,开口位于叶根的一侧,孔板从该开口装入其装配槽内,与叶根装入叶轮轮槽的方向一致;所述孔板的底面上有一个凸台,位于节流孔板的轴向中分线上,凸台的左端面与孔板的左端面齐平;所述锁键的左端面底部有一左伸凸台,该左伸凸台的竖直高度等于节流孔板上的凸台高度,所述孔板的右部底面坐落在锁键的凸台上;所述孔板、锁键组合后,通过孔板、锁键的凸台坐落在叶轮轮槽内;所述锁键装配槽位于叶根的右部,锁键的左壁面与孔板的右端面齐平,该槽是径向竖直开口槽,槽口在下,锁键由下向上装进其装配槽内;当锁键装配到位后,其左端面与孔板的右端面对齐接触,将孔板限位锁定,使孔板不会从轮槽中窜出,并将孔板装配槽的开口封堵,起密封作用,避免冷却介质从孔板装配槽的开口泄出。
2.权利要求1所述空心叶片冷却介质节流孔板的装配方法,包括步骤:
A、先把孔板装入其装配槽内;
B、再把叶片的叶根连同孔板一起从右向左推进叶轮的轮槽,不推到位,留出锁键的安装操作空间;
C、将锁键装进其装配槽内;
D、继续把叶片的叶根连同节流孔板、锁键一并推进叶轮的轮槽,直至到位。
CN201611212456.XA 2016-12-25 2016-12-25 一种空心叶片冷却介质节流孔板的配置结构及其装配方法 Pending CN106640215A (zh)

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB359350A (en) * 1930-03-03 1931-10-22 Ltd Co Formerly Skoda Works Connection of rotarys for combustion turbines
JP2002303101A (ja) * 2001-04-05 2002-10-18 Ishikawajima Harima Heavy Ind Co Ltd タービン翼の冷却空気調整構造
JP2006266112A (ja) * 2005-03-22 2006-10-05 Mitsubishi Heavy Ind Ltd タービン動翼
CN102197193A (zh) * 2008-10-22 2011-09-21 斯奈克玛 装有冷却流体流量调整装置的涡轮叶片
EP2990597A1 (en) * 2014-08-28 2016-03-02 Siemens Aktiengesellschaft Method for manufacturing a turbine assembly

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB359350A (en) * 1930-03-03 1931-10-22 Ltd Co Formerly Skoda Works Connection of rotarys for combustion turbines
JP2002303101A (ja) * 2001-04-05 2002-10-18 Ishikawajima Harima Heavy Ind Co Ltd タービン翼の冷却空気調整構造
JP2006266112A (ja) * 2005-03-22 2006-10-05 Mitsubishi Heavy Ind Ltd タービン動翼
CN102197193A (zh) * 2008-10-22 2011-09-21 斯奈克玛 装有冷却流体流量调整装置的涡轮叶片
EP2990597A1 (en) * 2014-08-28 2016-03-02 Siemens Aktiengesellschaft Method for manufacturing a turbine assembly

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