JPH06336998A - Motor-driven runner vane servo-motor - Google Patents

Motor-driven runner vane servo-motor

Info

Publication number
JPH06336998A
JPH06336998A JP5129037A JP12903793A JPH06336998A JP H06336998 A JPH06336998 A JP H06336998A JP 5129037 A JP5129037 A JP 5129037A JP 12903793 A JP12903793 A JP 12903793A JP H06336998 A JPH06336998 A JP H06336998A
Authority
JP
Japan
Prior art keywords
motor
shaft
thrust
main shaft
screw shaft
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.)
Granted
Application number
JP5129037A
Other languages
Japanese (ja)
Other versions
JP2735109B2 (en
Inventor
Katsumi Sato
克己 佐藤
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.)
Ebara Corp
Original Assignee
Ebara Corp
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 Ebara Corp filed Critical Ebara Corp
Priority to JP5129037A priority Critical patent/JP2735109B2/en
Publication of JPH06336998A publication Critical patent/JPH06336998A/en
Application granted granted Critical
Publication of JP2735109B2 publication Critical patent/JP2735109B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To reduce the capacity and rotational friction loss of thrust bearings by connecting plural planetary reduction gears to a driving motor, connecting a case to the main shaft of a hydraulic turbine or the like, and connecting the operating rod of a movable vane to the output shaft of one planetary reduction gear by a lift nut. CONSTITUTION:In order to change the vane angle of a movable vane 1, a screw shaft 9 is rotated normally or reversely. At this time, thrust does not act upon thrust bearings 6a, 6b because of being offset by the tension or compression of a main shaft 5. The capacity and rotational friction loss of a main bearing 6 can be thereby reduced. In order to rotate the screw shaft 9 normally or reversely, the rotation of a variable speed motor 11 is increased or reduced to produce relative rotational difference between the output shaft 12b of a secondary planetary reduction gear 12, that is, the screw shaft 9, and the main shaft 5, that is, an extended part 12B. When the relative rotational difference is plus, for instance, a lift nut 7 moves axially by the specified stroke S so as to move an operating rod 4 in a direction (b), thus changing the vane angle of the movable vane 1 in a direction (d).

Description

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

【0001】[0001]

【産業上の利用分野】本発明は、水車又はポンプの流量
変化に対応して可動翼の角度を電動で変化させる電動ラ
ンナベーンサーボモータに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an electric runner vane servomotor for electrically changing the angle of a movable blade in response to a change in flow rate of a water turbine or a pump.

【0002】[0002]

【従来の技術】可動翼の角度を変える手段としては、従
来からの油圧シリンダ式、又は電動アクチュエータを別
置きしてレバーを介して行う電動レバー式とが一般的で
ある。
2. Description of the Related Art As a means for changing the angle of a movable blade, a conventional hydraulic cylinder type or an electric lever type in which an electric actuator is separately installed and a lever is used is generally used.

【0003】[0003]

【発明が解決しようとする課題】従来の油圧シリンダ式
の場合は、大掛かりな圧油装置を必要とする他に、操作
のための油を含めたメンテナンスとイニシャルコスト、
ランニングコストがかかる欠点がある。
In the case of the conventional hydraulic cylinder type, in addition to requiring a large-scale pressure oil device, maintenance and initial cost including oil for operation,
There is a drawback that running costs are high.

【0004】また、図3に示す電動レバー式においては
油圧シリンダ式と異なり、可動翼1の翼角度を正逆に変
化させるに必要な大きい駆動力は、電動アクチュエータ
2から、レバー3、操作ロッド4及び水車又はポンプ1
00とモータ又は発電機200を連結する主軸5を介
し、主軸受6の推力軸受6a、6bに加わる。したがっ
て、この推力を受ける分だけ主軸受6の容量が大きくな
る他に、推力に伴う回転摩擦損失が推力軸受6a、6b
に生じ、水車又はポンプ100の効率が大幅に低下す
る。
Unlike the hydraulic cylinder type in the electric lever type shown in FIG. 3, the large driving force required to change the blade angle of the movable blade 1 in the forward and reverse directions is generated from the electric actuator 2 to the lever 3 and the operating rod. 4 and turbine or pump 1
00 and the motor or generator 200 are connected to the thrust bearings 6a and 6b of the main bearing 6 through the main shaft 5. Therefore, in addition to the capacity of the main bearing 6 increasing by the amount of this thrust, the rotational friction loss due to the thrust also causes thrust bearings 6a and 6b.
And the efficiency of the turbine or pump 100 is significantly reduced.

【0005】本発明は、翼角度を変える際に生じる推力
に係る不具合を解消する電動ランナベーンサーボモータ
を提供することを目的としている。
It is an object of the present invention to provide an electric runner vane servomotor which eliminates the problems associated with the thrust generated when changing the blade angle.

【0006】[0006]

【課題を解決するための手段】本発明によれば、駆動用
モータに一次及び二次遊星減速機を連結して該二次遊星
減速機のケースを水車又はポンプの主軸に連結し、該水
車又はポンプの可動翼の操作ロッドを前記二次遊星減速
機の出力軸にリフトナットを介して連繋している。
According to the present invention, primary and secondary planetary speed reducers are connected to a drive motor, and a case of the secondary planetary speed reducer is connected to a main shaft of a water turbine or a pump. Alternatively, the operating rod of the movable blade of the pump is connected to the output shaft of the secondary planetary speed reducer via a lift nut.

【0007】上記リフトナットは、二次遊星減速機の出
力軸に設けたねじ軸の台形ねじ部に螺合させるのが好ま
しい。
It is preferable that the lift nut is screwed into a trapezoidal screw portion of a screw shaft provided on the output shaft of the secondary planetary speed reducer.

【0008】[0008]

【作用】上記のように構成された電動ランナベーンサー
ボモータにおいては、駆動用モータの回転を増速又は減
速し、ねじ軸と主軸との間に相対回転差を生じさせ、リ
フトナットを軸方向に移動し、操作ロッドを介して可動
翼の翼角度を変化させる。この際に生じる推力は、ねじ
軸を支持する推力軸受に加わり、その反力は主軸を引張
り、又は、圧縮し、主軸内で打ち消される。したがっ
て、前記推力に係る従来の不具合が解消される。
In the electric runner vane servomotor configured as described above, the rotation of the drive motor is accelerated or decelerated to cause a relative rotation difference between the screw shaft and the spindle, and the lift nut is axially moved. It moves and changes the wing angle of the movable wing via the operation rod. The thrust generated at this time is applied to the thrust bearing that supports the screw shaft, and the reaction force pulls or compresses the main shaft, and is canceled within the main shaft. Therefore, the conventional problem related to the thrust is eliminated.

【0009】[0009]

【実施例】以下図面を参照して本発明の実施例を説明す
る。
Embodiments of the present invention will be described below with reference to the drawings.

【0010】図1において、可変速モータ11の出力軸
11aには、一次遊星減速機13の太陽歯車軸13aが
連結されている。その減速機13の出力軸13bには、
二次遊星減速機12のラジアル軸受14で支持された太
陽歯車軸12aが連結されている。この減速機12の出
力軸12bには、台形ねじ部aを備えたねじ軸9が連結
されている。また、減速機12のケース12Aには、延
長部12Bが一体に結合され、その延長部12Bには、
主軸5の一端がフランジ結合されている。この主軸5
は、モータ又は発電機200の動力軸であり、ラジアル
軸受15及び主軸受6の推力軸受6a、6bで支持さ
れ、他端には、水車又はポンプランジ結合されている。
In FIG. 1, a sun gear shaft 13a of a primary planetary speed reducer 13 is connected to an output shaft 11a of a variable speed motor 11. On the output shaft 13b of the speed reducer 13,
The sun gear shaft 12a supported by the radial bearing 14 of the secondary planetary speed reducer 12 is connected. The output shaft 12b of the speed reducer 12 is connected to a screw shaft 9 having a trapezoidal screw portion a. Further, an extension 12B is integrally connected to the case 12A of the speed reducer 12, and the extension 12B is
One end of the main shaft 5 is flanged. This spindle 5
Is a power shaft of the motor or generator 200, is supported by the radial bearing 15 and the thrust bearings 6a and 6b of the main bearing 6, and is connected to the other end by a water turbine or a pump lunge.

【0011】この水車又はポンプ100には、複数の可
動翼1が設けられ、操作ロッド4の前後進により翼角度
が正逆に変化されるようになっている。
The water turbine or pump 100 is provided with a plurality of movable vanes 1 so that the vane angle can be changed forward and backward by the forward and backward movement of the operating rod 4.

【0012】その操作ロッド4の先端は延長部12B内
において、リフトナット7ト固設され、スプラインガイ
ド8により延長部12Bに対し回転方向に係止されると
共に軸方向に摺動自在に支持されている。そして、この
リフトナット7には、ねじ軸9のねじ部aが螺合されて
いる。なお、図中の符号10a、10bはねじ軸9のデ
ィスク部9aを挟持する推力軸受である。
The distal end of the operating rod 4 is fixedly mounted in the extension portion 12B with a lift nut 7 and locked by the spline guide 8 in the rotational direction with respect to the extension portion 12B and supported slidably in the axial direction. ing. Then, the screw portion a of the screw shaft 9 is screwed into the lift nut 7. Reference numerals 10a and 10b in the drawing denote thrust bearings that sandwich the disk portion 9a of the screw shaft 9.

【0013】次に作用について説明する。Next, the operation will be described.

【0014】可動翼1の翼角度を変化させるには、ねじ
軸9を正方向または逆方向に回転させる。その際に生じ
る推力は、推力軸受10a又は10bに加わり、その反
力は主軸5を引張り、または、圧縮する。すなわち可動
翼1の翼角度を変更させるのに必要な推力は、主軸5の
内部で打ち消され、推力軸受6a、6bには作用しな
い。したがって、この分だけ主軸受6の容量を小さくす
ることができ、また、回転摩擦損失を少なくすることが
できる。
To change the blade angle of the movable blade 1, the screw shaft 9 is rotated in the forward or reverse direction. The thrust generated at that time is applied to the thrust bearing 10a or 10b, and the reaction force pulls or compresses the main shaft 5. That is, the thrust required to change the blade angle of the movable blade 1 is canceled inside the main shaft 5 and does not act on the thrust bearings 6a and 6b. Therefore, the capacity of the main bearing 6 can be reduced by this amount, and the rotational friction loss can be reduced.

【0015】上記のねじ軸9を正方向または逆方向に回
転させるには、可変速モータ11の回転を増速または減
速させ、二次遊星減速機12の出力軸12bすなわちね
じ軸9と主軸5すなわち延長部12Bとの間に、相対回
転差を生じさせる。このことにより、例えば相対回転差
がプラスの場合は、リフトナット7が軸方向にストロー
クSだけ移動し、操作ロッド4を矢印b方向に移動して
可動翼1の翼角度を矢印d方向に変化させる。また、相
対回転差がマイナスの場合は、操作ロッド4が矢印c方
向に移動し、矢印e方向に変化させる。また、相対回転
差がゼロの場合は、翼角度は変化しない。すなわち、可
変速モータ11は無負荷状態であり、水車又はポンプ1
00の動力により空転されている。このような相対回転
差がゼロのときにおいて、翼に作用する水面によって操
作ロッド4に推力がかかっても、ねじ部aが台形ねじで
あることと、ねじ勾配が小さいこととから、ボールねじ
のようにはねじ軸9は回転しないので、リフトナット7
は移動しなく、したがって、翼角度はその位置を保持す
る。
In order to rotate the screw shaft 9 in the forward or reverse direction, the rotation of the variable speed motor 11 is accelerated or decelerated, and the output shaft 12b of the secondary planetary speed reducer 12, that is, the screw shaft 9 and the main shaft 5. That is, a relative rotation difference is generated between the extension 12B. Accordingly, for example, when the relative rotation difference is positive, the lift nut 7 moves in the axial direction by the stroke S, the operation rod 4 moves in the arrow b direction, and the blade angle of the movable blade 1 changes in the arrow d direction. Let When the relative rotation difference is negative, the operating rod 4 moves in the direction of arrow c and changes in the direction of arrow e. When the relative rotation difference is zero, the blade angle does not change. That is, the variable speed motor 11 is in an unloaded state, and the turbine or pump 1
It is idling by the power of 00. When such a relative rotation difference is zero, even if thrust is applied to the operating rod 4 by the water surface acting on the blade, the screw portion a is a trapezoidal screw and the screw gradient is small, so Since the screw shaft 9 does not rotate, the lift nut 7
Does not move, so the wing angle retains its position.

【0016】可変速モータ11の最大回転数は、一般的
に2400r/m程度であり、モータ容量は極力回転数
を高く決め、減速比を大きくした方が小容量で済み経済
的である。一方、水車又はポンプ100の回転数は、大
型機械の場合に低速である。例えば水車の回転数を20
0r/mと仮定した場合、一次遊星減速機13を設けな
いで可変速モータ11を図2に示すように、二次遊星減
速機12に直結した場合には、モータ11の回転は水車
100の回転数と同一の200rpmで無負荷回転す
る。この無負荷回転数を基準にしてモータ11に負荷を
かけ、加速又は減速させて翼角度を変化させる場合に、
減速幅は200r/mから0r/mまでの200r/m
しかない。しかし、加速幅は200r/mから2400
r/mまでの差が2200r/mもあり、変速幅がアン
バランスであり、翼角度の変化スピードを適切に制御で
きない場合が生じる。
The maximum rotation speed of the variable speed motor 11 is generally about 2400 r / m, and it is economical to set the rotation speed as high as possible and increase the reduction ratio so that the reduction speed is small. On the other hand, the rotation speed of the water turbine or pump 100 is low in the case of a large machine. For example, the rotation speed of the water turbine is 20
Assuming 0 r / m, when the variable speed motor 11 is directly connected to the secondary planetary speed reducer 12 without providing the primary planetary speed reducer 13 as shown in FIG. Rotate without load at the same speed of 200 rpm. When a load is applied to the motor 11 based on this no-load rotation speed to accelerate or decelerate the blade angle,
Deceleration width is 200r / m from 200r / m to 0r / m
There is nothing. However, the acceleration range is from 200r / m to 2400
There is a case where the difference up to r / m is 2200 r / m, the shift width is unbalanced, and the change speed of the blade angle cannot be properly controlled.

【0017】これに対し図1の本実施例においては、一
次遊星減速機13を設け、その減速比を例えば1/6と
した場合、モータ11の無負荷回転数は水車の回転数2
00r/mの6倍の1200r/mになる。この回転数
は、モータ11の最大回転数2400r/mの中間回転
数であるので、加速幅、減速幅が同等となり、翼角度の
変化スピード設定が幅広くできる。また、この一次遊星
減速機13の減速比を任意に変えることにより、可変速
モータ11の加速幅、減速幅の大小を決め得ることか
ら、翼の開閉スピードを任意に設定することが可能であ
る。
On the other hand, in the present embodiment shown in FIG. 1, when the primary planetary speed reducer 13 is provided and the reduction ratio thereof is set to, for example, 1/6, the no-load rotation speed of the motor 11 is the rotation speed 2 of the water turbine.
It is 1200 r / m, which is six times 00 r / m. Since this rotation speed is an intermediate rotation speed of the maximum rotation speed 2400 r / m of the motor 11, the acceleration width and the deceleration width are the same, and the blade blade change speed setting can be widened. Further, by changing the reduction ratio of the primary planetary speed reducer 13 arbitrarily, the magnitude of the acceleration width and the deceleration width of the variable speed motor 11 can be determined, so that the opening / closing speed of the blades can be set arbitrarily. .

【0018】[0018]

【発明の効果】本発明は、以上説明したように構成され
ているので、翼角度を変える際に生じる推力に係る推力
軸受の大容量化や回転摩擦損失の増加を抑え、ポンプ又
は水車の効率を大幅に向上することができる。又、翼角
の開閉スピードを任意に設定できるので、ウォータハン
マを制限できる。
EFFECTS OF THE INVENTION Since the present invention is constructed as described above, it is possible to suppress an increase in the capacity of the thrust bearing and an increase in the rotational friction loss associated with the thrust generated when the blade angle is changed, and to improve the efficiency of the pump or the turbine. Can be greatly improved. Further, since the opening / closing speed of the blade angle can be arbitrarily set, the water hammer can be limited.

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

【図1】本発明の一実施例を示す側断面図。FIG. 1 is a side sectional view showing an embodiment of the present invention.

【図2】図1から一次遊星減速機を省いた状態を示す図
面。
FIG. 2 is a drawing showing a state in which a primary planetary speed reducer is omitted from FIG.

【図3】電動レバー式装置を示す側断面図。FIG. 3 is a side sectional view showing an electric lever type device.

【符号の説明】[Explanation of symbols]

1・・・可動翼 2・・・電動アクチュエータ 3・・・レバー 4・・・操作ロッド 5・・・主軸 6・・・主軸受 6a、6b、10a、10b・・・推力軸受 7・・・リフトナット 8・・・スプラインガイド 9・・・ねじ軸 9a・・・ディスク部 11・・・可変速モータ 11a・・・出力軸 12・・・二次遊星減速機 12a、13a・・・太陽歯車軸 12b、13b・・・出力軸 12A・・・ケース 12B・・・延長部 13・・・一次遊星減速機 14、15・・・ラジアル軸受 100・・・水車又はポンプ 200・・・モータ又は発電機 a・・・台形ねじ部 S・・・ストローク 1 ... Movable wing 2 ... Electric actuator 3 ... Lever 4 ... Operation rod 5 ... Main shaft 6 ... Main bearing 6a, 6b, 10a, 10b ... Thrust bearing 7 ... Lift nut 8 ... Spline guide 9 ... Screw shaft 9a ... Disk part 11 ... Variable speed motor 11a ... Output shaft 12 ... Secondary planetary reducer 12a, 13a ... Sun gear Shaft 12b, 13b ... Output shaft 12A ... Case 12B ... Extension 13 ... Primary planetary reducer 14, 15 ... Radial bearing 100 ... Water turbine or pump 200 ... Motor or power generation Machine a: Trapezoidal thread S: Stroke

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 駆動用モータに一次及び二次遊星減速機
を連結して該二次遊星減速機のケースを水車又はポンプ
の主軸に連結し、該水車又はポンプの可動翼の操作ロッ
ドを前記二次遊星減速機の出力軸にリフトナットを介し
て連繋したことを特徴とする電動ランナベーンサーボモ
ータ。
1. A primary and secondary planetary speed reducer is connected to a drive motor, a case of the secondary planetary speed reducer is connected to a main shaft of a water turbine or a pump, and an operating rod of a movable blade of the water turbine or the pump is connected to the drive shaft. An electric runner vane servomotor characterized by being connected to the output shaft of a secondary planetary reducer via a lift nut.
JP5129037A 1993-05-31 1993-05-31 Electric runner vane servomotor Expired - Fee Related JP2735109B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5129037A JP2735109B2 (en) 1993-05-31 1993-05-31 Electric runner vane servomotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5129037A JP2735109B2 (en) 1993-05-31 1993-05-31 Electric runner vane servomotor

Publications (2)

Publication Number Publication Date
JPH06336998A true JPH06336998A (en) 1994-12-06
JP2735109B2 JP2735109B2 (en) 1998-04-02

Family

ID=14999547

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5129037A Expired - Fee Related JP2735109B2 (en) 1993-05-31 1993-05-31 Electric runner vane servomotor

Country Status (1)

Country Link
JP (1) JP2735109B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102493964A (en) * 2011-12-29 2012-06-13 鞍山风机集团有限责任公司 Moving blade regulating device for axial flow fan

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60153479A (en) * 1984-01-23 1985-08-12 Ebara Corp Device for opening and closing runner vane

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60153479A (en) * 1984-01-23 1985-08-12 Ebara Corp Device for opening and closing runner vane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102493964A (en) * 2011-12-29 2012-06-13 鞍山风机集团有限责任公司 Moving blade regulating device for axial flow fan

Also Published As

Publication number Publication date
JP2735109B2 (en) 1998-04-02

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