JPH0942413A - Blade member and forming method therefor - Google Patents

Blade member and forming method therefor

Info

Publication number
JPH0942413A
JPH0942413A JP7194787A JP19478795A JPH0942413A JP H0942413 A JPH0942413 A JP H0942413A JP 7194787 A JP7194787 A JP 7194787A JP 19478795 A JP19478795 A JP 19478795A JP H0942413 A JPH0942413 A JP H0942413A
Authority
JP
Japan
Prior art keywords
blade
plate
blade member
pump
portions
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP7194787A
Other languages
Japanese (ja)
Inventor
Junji Miyagawa
川 順 次 宮
Ryuichi Uchino
野 龍 一 内
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aisin Corp
Original Assignee
Aisin Seiki Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aisin Seiki Co Ltd filed Critical Aisin Seiki Co Ltd
Priority to JP7194787A priority Critical patent/JPH0942413A/en
Publication of JPH0942413A publication Critical patent/JPH0942413A/en
Pending legal-status Critical Current

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PROBLEM TO BE SOLVED: To shorten a time which is necessary for assembling a plurality of impeller parts, and also reduce the position of the plurality of impellers and a pitch. SOLUTION: One steel plate is worked so as to form a blade plate which consists of a plurality of circle impeller parts 11, and a connecting part 12 for connecting both ends of the arcs of the impeller to each other so as to position the impeller part 11 on the same right line. The folding rate of the connecting part 12 of the one end is enlarged more than the folding rate of the connecting part 12 of the other end of the each impeller part 11, and the blade plate is curved in a circular shape, and the impeller part 11 is folded nearly vertically to the blade plate. It is thus possible to form a blade member 10.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、複数の羽根部が回
転することによりトルクの伝達を行う装置、例えば自動
変速機のトルクコンバータのポンプ或いはタービン内周
面に取付けられるような、複数の羽根部からなるブレー
ド部材、およびその成形方法に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a device for transmitting torque by rotating a plurality of blades, for example, a plurality of blades attached to a pump or a turbine inner peripheral surface of a torque converter of an automatic transmission. And a method for forming the same.

【0002】[0002]

【従来の技術】複数の羽根部を備える装置の従来技術と
して、図7に特開平6−129530号公報に開示され
るトルクコンバータ20の断面図を示す。上記公報に開
示されるトルクコンバータ20は、エンジンからの駆動
力を伝達する入力軸21に連結するポンプ22と、ポン
プ22の内周面に取り付けられたポンプ羽根部23と、
変速装置に駆動力を伝達する出力軸24に連結するター
ビン25と、タービン25の内周面に取り付けられたタ
ービン羽根部26と、流体の流通路断面積を変化させる
べくポンプ22の内周面にボルトにて取付けられた遮蔽
板27と、を備えるものである。
2. Description of the Related Art FIG. 7 shows a sectional view of a torque converter 20 disclosed in Japanese Patent Laid-Open No. 6-129530, as a prior art of a device having a plurality of blades. The torque converter 20 disclosed in the above publication includes a pump 22 connected to an input shaft 21 that transmits a driving force from an engine, a pump blade portion 23 attached to an inner peripheral surface of the pump 22,
A turbine 25 connected to an output shaft 24 that transmits a driving force to a transmission device, a turbine blade portion 26 attached to an inner peripheral surface of the turbine 25, and an inner peripheral surface of a pump 22 for changing a fluid passage cross-sectional area. And a shield plate 27 attached to the base plate with bolts.

【0003】図8は図7のトルクコンバータ20のポン
プ側正面図である。トルクコンバータ20においては、
ポンプ22からタービン25へトルクを伝達するための
複数のポンプ羽根部23が、ポンプ22の内周面の取付
け部22aに1枚ずつ取り付けられており、ポンプ羽根
部23の取付け片23aが環状のインナコア28の取付
け孔28aに挿通した後に折り曲げられている。
FIG. 8 is a pump side front view of the torque converter 20 of FIG. In the torque converter 20,
A plurality of pump blade portions 23 for transmitting torque from the pump 22 to the turbine 25 are attached one by one to the attachment portion 22a of the inner peripheral surface of the pump 22, and the attachment piece 23a of the pump blade portion 23 is annular. It is bent after being inserted into the mounting hole 28a of the inner core 28.

【0004】[0004]

【本発明が解決する課題】上記従来の技術においては、
トルクコンバータのポンプおよびタービンの内周面に各
羽根部を1枚ずつ取り付けているために、羽根部の組付
けに時間がかかってしまう。また、ポンプおよびタービ
ンの内周の取付け孔と羽根部の組付け部分との間のクリ
アランスにより、羽根部の取付け時において羽根部の位
置やピッチが各羽根部毎でずれる恐れがある。
SUMMARY OF THE INVENTION In the above conventional technique,
Since one blade is attached to each of the inner peripheral surfaces of the pump and the turbine of the torque converter, it takes time to assemble the blade. Further, due to the clearance between the mounting holes on the inner circumference of the pump and the turbine and the assembly portion of the blade portion, the position and pitch of the blade portion may be deviated for each blade portion when the blade portion is mounted.

【0005】そこで本発明は、複数の羽根部を取付ける
際に要する時間を可及的に短縮するとともに、羽根部の
位置やピッチのずれを少なくすることを技術的課題とす
る。
Therefore, it is a technical object of the present invention to shorten the time required for mounting a plurality of blades as much as possible and to reduce the deviation of the position and pitch of the blades.

【0006】[0006]

【課題を解決するための手段】上記課題を解決するため
の請求項1は、1枚の鋼板を加工することにより、扇形
状の複数の羽根部と、羽根部が同一直線上にあるように
羽根部の弧の両端をそれぞれ連結する連結部と、からな
るブレード板を形成する形成工程と、ブレード板の各々
の羽根部の一端の連結部の折り曲げ量に対して他端の連
結部の折り曲げ量を大きくしてブレード板を円弧状に湾
曲させるとともに、ブレード板に対して羽根部を略垂直
に折り曲げる折り曲げ工程と、によりブレード部材を成
形する成形方法である。
According to a first aspect of the present invention, a plurality of fan-shaped blade portions and a plurality of blade portions are formed on the same straight line by processing one steel plate. A step of forming a blade plate consisting of a connecting part for connecting both ends of the arc of the blade part, and a bending of the connecting part at the other end with respect to the bending amount of the connecting part at one end of each blade part of the blade plate This is a forming method of forming a blade member by a bending step of bending the blade plate into an arc shape by increasing the amount and bending the blade portion substantially perpendicular to the blade plate.

【0007】請求項1の発明によると、ブレード部材は
1枚の鋼板から複数の羽根部を形成しているので、ブレ
ード部材の取付けに要する時間が少なくなるとともに、
各羽根部の位置やピッチのずれは殆どない。更に、形成
工程にて羽根部が同一直線上にあるように鋼板をプレス
加工しているので、材料歩留りが悪くなるのを防ぐこと
が可能になる。
According to the first aspect of the invention, the blade member has a plurality of blades formed from a single steel plate, so that the time required for mounting the blade member is reduced and
There is almost no deviation in the position or pitch of each blade. Furthermore, since the steel plate is pressed so that the blade portions are on the same straight line in the forming step, it is possible to prevent the material yield from being deteriorated.

【0008】請求項2の発明は、1枚の鋼板を加工する
ことにより、扇形状の複数の羽根部と、羽根部が同一直
線上にあるように羽根部の弧の両端をそれぞれ連結する
連結部と、からなるブレード板を形成する形成工程と、
ブレード板の各々の羽根部の一端の連結部の折り曲げ量
に対して他端の連結部の折り曲げ量を大きくしてブレー
ド板を円弧状に湾曲させるとともに、ブレード板に対し
て羽根部を略垂直に折り曲げる折り曲げ工程と、により
成形されるブレード部材である。
According to the second aspect of the present invention, by processing one steel plate, a plurality of fan-shaped blade portions are connected to each other so as to connect both ends of the arc of the blade portions so that the blade portions are on the same straight line. And a forming step of forming a blade plate composed of
The blade plate is curved in an arc shape by increasing the bending amount of the connecting portion at the other end relative to the bending amount of the connecting portion at one end of each blade portion of the blade plate, and the blade portion is substantially perpendicular to the blade plate. The blade member is formed by a bending step of bending into a.

【0009】請求項2によると、ブレード部材は複数の
羽根部を連結部にて一体に備えているので、ブレード部
材を組付ける際には複数の羽根部を一度に組付けること
が可能になり、ブレード部材の組付けに要する時間が少
なくなる。また、組付け時に各羽根部の位置及びピッチ
のずれが生じることがない。
According to the second aspect, the blade member is integrally provided with a plurality of blade portions at the connecting portion. Therefore, when assembling the blade member, a plurality of blade portions can be assembled at once. The time required for assembling the blade member is reduced. Further, the position and pitch of the blades do not deviate during assembly.

【0010】[0010]

【発明の実施の形態】以下、本発明の実施の形態を図面
を参照して説明する。本実施の形態では、複数の羽根部
をポンプ及びタービンの内周面に備えるトルクコンバー
タに、本発明のブレード部材を用いた場合について説明
する。
Embodiments of the present invention will be described below with reference to the drawings. In the present embodiment, a case will be described in which the blade member of the present invention is used in a torque converter including a plurality of blades on the inner peripheral surfaces of a pump and a turbine.

【0011】図1は本実施の形態におけるブレード部材
10をトルクコンバータのポンプ側に取付けた時のポン
プ側正面図であり、図2は図1のA−A断面図である。
FIG. 1 is a pump-side front view when the blade member 10 according to the present embodiment is attached to the pump side of the torque converter, and FIG. 2 is a sectional view taken along line AA of FIG.

【0012】始めに構成について説明する。エンジンか
らの駆動力を伝達する入力軸に連結するポンプ13と、
変速装置に駆動力を伝達する出力軸に連結するタービン
(図示せず)と、ポンプ13の内周面に取り付けられた
ブレード部材10と、を有し、ブレード部材10は複数
の扇形状の羽根部11と、複数の羽根部11の弧の両端
部近傍をそれぞれ連結するとともに、羽根部11に対し
て略垂直な連結部12と、ボルト15にてポンプ13の
内周面に取付けられた遮蔽板14と、を備えるものであ
る。ここで、本実施の形態におけるブレード部材10以
外の構成は図4に示す従来のトルクコンバータと同じ構
成である。
First, the configuration will be described. A pump 13 connected to an input shaft for transmitting the driving force from the engine,
The transmission includes a turbine (not shown) connected to an output shaft that transmits a driving force to the transmission, and a blade member 10 attached to an inner peripheral surface of the pump 13. The blade member 10 has a plurality of fan-shaped blades. The shield is attached to the inner peripheral surface of the pump 13 by a bolt 12 and a connecting portion 12 that is substantially perpendicular to the blade portion 11 while connecting the portion 11 and the vicinity of both ends of the arc of the plurality of blade portions 11 respectively. And a plate 14. Here, the configuration other than the blade member 10 in the present embodiment is the same as that of the conventional torque converter shown in FIG.

【0013】次に、本実施の形態におけるブレード部材
10の成形方法について、図3から図6を用いて説明す
る。
Next, a method of molding the blade member 10 in this embodiment will be described with reference to FIGS. 3 to 6.

【0014】先ず、形成工程により、1枚の鋼板をプレ
ス加工して、扇形状の複数の羽根部11と複数の羽根部
11が同一直線上にあるように羽根部11の弧の両端部
11a近傍をそれぞれ連結する連結部12と、からなる
ブレード板10aを形成する(図3)。次に、折り曲げ
工程にて、各々の羽根部11の一端の連結部12の折り
曲げ量に対して他端の連結部12の折り曲げ量を大きく
することにより、ブレード板10aを円弧状に湾曲させ
るとともに(図4)、ブレード板10aに対して羽根部
11を略垂直に折り曲げる(図5,図6)。上記の工程
によりブレード部材10が成形される。ここで図4は、
ブレード部材10の羽根部11の形状がわかるように斜
視図となっており、図5および図6は図4のA視および
B視の一部拡大図である。図5および図6から、連結部
12の折り曲げ量の違いがわかる。
First, in the forming step, one steel plate is pressed to form a plurality of fan-shaped blade portions 11 and both end portions 11a of the arc of the blade portion 11 so that the blade portions 11 are on the same straight line. A blade plate 10a composed of connecting portions 12 for connecting the respective neighborhoods is formed (FIG. 3). Next, in the bending step, the blade plate 10a is curved in an arc shape by increasing the bending amount of the connecting portion 12 at the other end with respect to the bending amount of the connecting portion 12 at the one end of each blade 11. (FIG. 4), the blade portion 11 is bent substantially perpendicular to the blade plate 10a (FIGS. 5 and 6). The blade member 10 is molded by the above steps. Here, in FIG.
It is a perspective view so that the shape of the blade portion 11 of the blade member 10 can be seen, and FIGS. 5 and 6 are partially enlarged views of FIG. 5 and 6, the difference in the bending amount of the connecting portion 12 can be seen.

【0015】上記の折り曲げ工程における鋼板の曲げ加
工は、予め決められた所定量だけ鋼板の連結部12を曲
げるようにコンピュータ制御されるロボット(図示せ
ず)により行われている。
The bending of the steel sheet in the above bending step is performed by a computer-controlled robot (not shown) so as to bend the connecting portion 12 of the steel sheet by a predetermined amount.

【0016】このようにして成形されたブレード部材1
0は、溶接や接着、あるいはカシメ等によってトルクコ
ンバータのポンプ13の内周面に取付けられる。
The blade member 1 thus formed
0 is attached to the inner peripheral surface of the pump 13 of the torque converter by welding, adhesion, caulking or the like.

【0017】尚、本実施の形態においては、ポンプ13
の内周面全体に羽根部11を設けるには、本実施の形態
のブレード部材10が3つ必要になるように羽根部11
の枚数を設定してあるが、特にこの枚数に限定する意図
はなく、1つのブレード部材でポンプの内周面全体に羽
根部が設けられるように設定してもよい。また、本実施
の形態では、図8の従来技術に示すような可変容量型ト
ルクコンバータに本発明のブレード部材を用いた場合を
示したが、トルクコンバータに用いることに限定する意
図はなく、複数の羽根部を備える装置であれば、どのよ
うな装置に用いてもよい。
In the present embodiment, the pump 13
In order to provide the blade portion 11 on the entire inner peripheral surface of the blade portion, the blade portion 11 of the present embodiment requires three blade members 10.
The number of the blades is set, but there is no particular limitation to this number, and one blade member may be set so that the blade portion is provided on the entire inner peripheral surface of the pump. Further, in the present embodiment, the case where the blade member of the present invention is used in the variable displacement torque converter as shown in the prior art of FIG. 8 is shown, but there is no intention to limit the use to the torque converter, and a plurality of blade members may be used. Any device may be used as long as it is a device provided with the vane part.

【0018】[0018]

【発明の効果】請求項1の成形方法によると、複数の羽
根部を一体に形成しているので、複数の羽根部を一度に
取り付けることが可能になり、組付ける際に要する時間
を可及的に短縮することができるとともに、各々の羽根
部の位置およびピッチがずれることがないブレード部材
を成形することが可能になる。更に、ブレード部材の材
料歩留りが悪くなるのを防ぐことができる。
According to the molding method of the first aspect, since the plurality of blade portions are integrally formed, the plurality of blade portions can be attached at one time, and the time required for the assembling can be reduced. It is possible to form a blade member that can be shortened as a whole and in which the positions and pitches of the respective blade portions do not shift. Further, it is possible to prevent the material yield of the blade member from being deteriorated.

【0019】請求項2の発明によると、複数の羽根部を
一度に取り付けることが可能になるので、ブレード部材
を取付ける際に要する時間を短縮することができる。ま
た、複数の羽根部が一体となっているため、各々の羽根
部の位置およびピッチがずれることがない。
According to the second aspect of the present invention, since it is possible to attach a plurality of blade portions at once, it is possible to shorten the time required for attaching the blade member. Further, since the plurality of blade portions are integrated, the position and pitch of each blade portion do not shift.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の実施の形態を示すポンプ側正面図であ
る。
FIG. 1 is a pump-side front view showing an embodiment of the present invention.

【図2】図1のA−A断面図である。FIG. 2 is a sectional view taken along line AA of FIG.

【図3】本実施の形態におけるブレード部材の形成工程
後を示す図である。
FIG. 3 is a diagram showing a state after a blade member forming step in the present embodiment.

【図4】本実施の形態におけるブレード部材の折り曲げ
工程後を示す図である。
FIG. 4 is a diagram showing a blade member after a bending step in the present embodiment.

【図5】図4のA視の一部拡大図である。5 is a partially enlarged view of FIG. 4 viewed from A. FIG.

【図6】図4のB視の一部拡大図である。FIG. 6 is a partially enlarged view of FIG. 4 viewed from B.

【図7】従来技術を示すトルクコンバータの断面図であ
る。
FIG. 7 is a sectional view of a torque converter showing a conventional technique.

【図8】従来のブレード部材の取付け状態を示す図であ
る。
FIG. 8 is a view showing a state in which a conventional blade member is attached.

【符号の説明】[Explanation of symbols]

10・・・ブレード部材 11・・・羽根
部 12・・・連結部 13、22・・
・ポンプ 14、27・・・遮蔽板 15・・・ボル
ト 20・・・トルクコンバータ 21・・・入力
軸 23・・・ポンプ羽根部 24・・・出力
軸 25・・・タービン 26・・・ター
ビン羽根部 28・・・インナコア
10 ... Blade member 11 ... Blade part 12 ... Connection part 13, 22 ...
-Pumps 14, 27 ... Shielding plate 15 ... Bolts 20 ... Torque converter 21 ... Input shaft 23 ... Pump blade portion 24 ... Output shaft 25 ... Turbine 26 ... Turbine Feather part 28: Inner core

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 1枚の鋼板を加工することにより、扇形
状の複数の羽根部と、該羽根部が同一直線上にあるよう
に前記羽根部の弧の両端をそれぞれ連結する連結部と、
からなるブレード板を形成する形成工程と、 各々の羽根部の一端の連結部の折り曲げ量に対して他端
の連結部の折り曲げ量を大きくすることにより、前記ブ
レード板を円弧状に湾曲させるとともに、前記ブレード
板に対して前記羽根部を略垂直に折り曲げる折り曲げ工
程と、 によりブレード部材を成形するブレード部材の成形方
法。
1. A plurality of fan-shaped blade portions by processing one steel plate, and a connecting portion that connects both ends of an arc of the blade portions so that the blade portions are on the same straight line,
A step of forming a blade plate consisting of, and increasing the bending amount of the connecting portion at the other end with respect to the bending amount of the connecting portion at one end of each blade portion, while curving the blade plate in an arc shape A bending step of bending the blade portion substantially perpendicularly to the blade plate, and a blade member forming method for forming a blade member.
【請求項2】 1枚の鋼板を加工することにより、扇形
状の複数の羽根部と、該羽根部が同一直線上にあるよう
に前記羽根部の弧の両端をそれぞれ連結する連結部と、
からなるブレード板を形成する形成工程と、 各々の羽根部の一端の連結部の折り曲げ量に対して他端
の連結部の折り曲げ量を大きくすることにより、前記ブ
レード板を円弧状に湾曲させるとともに、前記ブレード
板に対して前記羽根部を略垂直にする折り曲げ工程と、 により成形されるブレード部材。
2. A plurality of fan-shaped blade portions and a connecting portion that connects both ends of an arc of the blade portions so that the blade portions are on the same straight line by processing one steel plate.
A step of forming a blade plate consisting of, and increasing the bending amount of the connecting portion at the other end with respect to the bending amount of the connecting portion at one end of each blade portion, while curving the blade plate in an arc shape A bending step in which the blade portion is substantially perpendicular to the blade plate;
JP7194787A 1995-07-31 1995-07-31 Blade member and forming method therefor Pending JPH0942413A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7194787A JPH0942413A (en) 1995-07-31 1995-07-31 Blade member and forming method therefor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7194787A JPH0942413A (en) 1995-07-31 1995-07-31 Blade member and forming method therefor

Publications (1)

Publication Number Publication Date
JPH0942413A true JPH0942413A (en) 1997-02-14

Family

ID=16330261

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7194787A Pending JPH0942413A (en) 1995-07-31 1995-07-31 Blade member and forming method therefor

Country Status (1)

Country Link
JP (1) JPH0942413A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001141028A (en) * 1999-08-27 2001-05-25 Yutaka Giken Co Ltd Blade linking body of hydraulic power transmission and its manufacturing method
JP2008249049A (en) * 2007-03-30 2008-10-16 Jatco Ltd Blade structure for torque converter, and its manufacturing method
EP2022575A2 (en) 2007-08-07 2009-02-11 JATCO Ltd Blade structure for torque converter and process of producing the same
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JP2009531605A (en) * 2006-03-24 2009-09-03 ルーク ラメレン ウント クツプルングスバウ ベタイリグングス コマンディートゲゼルシャフト Two-piece fixed wing
US20130160438A1 (en) * 2011-12-23 2013-06-27 Schaeffler Technologies AG & Co. KG Extended turbine blade
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US6382916B1 (en) 1999-08-27 2002-05-07 Kabushiki Kaisha Yutaka Giken Blade assembly for hydraulic power transmitting apparatus and method of manufacturing same
JP2001141028A (en) * 1999-08-27 2001-05-25 Yutaka Giken Co Ltd Blade linking body of hydraulic power transmission and its manufacturing method
JP2009531605A (en) * 2006-03-24 2009-09-03 ルーク ラメレン ウント クツプルングスバウ ベタイリグングス コマンディートゲゼルシャフト Two-piece fixed wing
JP2008249049A (en) * 2007-03-30 2008-10-16 Jatco Ltd Blade structure for torque converter, and its manufacturing method
EP2022575A2 (en) 2007-08-07 2009-02-11 JATCO Ltd Blade structure for torque converter and process of producing the same
JP2009041611A (en) * 2007-08-07 2009-02-26 Jatco Ltd Blade structure for torque converter and method of producing blade structure for torque converter
KR101480558B1 (en) * 2007-08-07 2015-01-08 쟈트코 가부시키가이샤 Blade structure of torque converter and method for manufacturing blade structure of torque converter
EP2468431A1 (en) 2007-08-07 2012-06-27 Jatco Ltd Blade structure for torque converter and process of producing the same
US8128370B2 (en) 2007-08-07 2012-03-06 Jatco Ltd Blade structure for torque converter and process of producing the same
JP4540693B2 (en) * 2007-08-07 2010-09-08 ジヤトコ株式会社 Torque converter blade structure and method of manufacturing torque converter blade structure
US8069563B2 (en) 2007-08-31 2011-12-06 Jatco Ltd Blade structure for torque converter and process for producing the same
EP2030702A2 (en) 2007-08-31 2009-03-04 JATCO Ltd Blade structure for torque converter and process for producing the same
KR101522428B1 (en) * 2007-08-31 2015-05-21 쟈트코 가부시키가이샤 Blade structure of torque converter and method for manufacturing blade structure of torque converter
JP4540696B2 (en) * 2007-08-31 2010-09-08 ジヤトコ株式会社 Torque converter blade structure and method of manufacturing torque converter blade structure
JP2009058046A (en) * 2007-08-31 2009-03-19 Jatco Ltd Blade structure of torque converter, and method for manufacturing torque converter blade structure
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US8157529B2 (en) 2007-09-28 2012-04-17 Jatco Ltd Blade structure of torque converter and method for producing blade structure of torque converter
EP2042773A2 (en) 2007-09-28 2009-04-01 JATCO Ltd Blade structure of torque converter and method for producing blade structure of torque converter
US20130160438A1 (en) * 2011-12-23 2013-06-27 Schaeffler Technologies AG & Co. KG Extended turbine blade
US9476490B2 (en) * 2011-12-23 2016-10-25 Schaeffler Technologies AG & Co. KG Extended turbine blade
CN106969127A (en) * 2016-01-13 2017-07-21 熵零技术逻辑工程院集团股份有限公司 A kind of energy adjustment system
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