JPH0637596U - Stationary operation ring - Google Patents

Stationary operation ring

Info

Publication number
JPH0637596U
JPH0637596U JP7884092U JP7884092U JPH0637596U JP H0637596 U JPH0637596 U JP H0637596U JP 7884092 U JP7884092 U JP 7884092U JP 7884092 U JP7884092 U JP 7884092U JP H0637596 U JPH0637596 U JP H0637596U
Authority
JP
Japan
Prior art keywords
ring
operating ring
operating
operation ring
axial direction
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.)
Withdrawn
Application number
JP7884092U
Other languages
Japanese (ja)
Inventor
敏彦 宮崎
卓 一柳
渡 藤岡
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP7884092U priority Critical patent/JPH0637596U/en
Publication of JPH0637596U publication Critical patent/JPH0637596U/en
Withdrawn legal-status Critical Current

Links

Abstract

(57)【要約】 【目的】 コストの安い軸方向移動形によって正確に操
作環を案内する。 【構成】 静翼の軸にレバーを取付け、同レバー先端の
ピンを車室外周に設けた操作環20の円周溝に係合させ
ると共に、操作環20を軸方向に動かして翼角を変更す
るようにした静翼操作環であって、同操作環20の外周
に複数のピン25とローラ26よりなる突起を設け、一
方車室に固定したブラケット24には前記ローラ26が
嵌まり合う部分ネジ溝27を設け、操作環20を軸方向
に移動して静翼翼角を調整するようにしたものである。
(57) [Abstract] [Purpose] To accurately guide the operating ring by the low-cost axial movement type. [Structure] A lever is attached to the shaft of a stationary blade, and a pin at the tip of the lever is engaged with a circumferential groove of an operating ring 20 provided on the outer periphery of the vehicle compartment, and the operating ring 20 is moved in the axial direction to change the blade angle. In the stationary vane operation ring, a protrusion composed of a plurality of pins 25 and rollers 26 is provided on the outer periphery of the operation ring 20, and the roller 26 is fitted to the bracket 24 fixed to the vehicle compartment. A thread groove 27 is provided, and the operating ring 20 is moved in the axial direction to adjust the vane blade angle.

Description

【考案の詳細な説明】[Detailed description of the device]

【0001】[0001]

【産業上の利用分野】[Industrial applications]

本考案は圧縮機で複数の段の静翼取付角を運転中に操作する形式の静翼操作環 に関するものである。 The present invention relates to a stationary vane operating ring of a type in which a plurality of stages of stationary vane mounting angles are operated by a compressor during operation.

【0002】[0002]

【従来の技術】[Prior art]

従来より圧縮機において、複数の段の静翼取付角を運転中に随時変更する事は 、圧縮機の性能上要求される事がしばしばある。その場合静翼の軸にレバーを付 し、そのレバーの先端にピンを設け、そのピンを車室外周に設けた操作環の溝に 係合させると共に、同操作環を動かすことにより静翼取付角を変更するようにし ていた。この場合の操作環の動かし方に軸方向に動かすものと、回転させるもの との2種類がある。 操作環を軸方向に動かして翼角操作を行なう形式の従来例を図8及び図9に示 す。図9は静翼2のレバーと操作環1の関係を示しており、図8のD部拡大図で ある。操作環1は外周部を複数本の支持軸12にブッシュ13を介して軸方向摺 動可能に支えられており、同支持軸12は両端を車室に固定されている。以上の ようにして操作環1は軸方向に傾く事なく摺動可能に支えられ、サーボモータ1 1により軸方向に動かされる。なお、10は操作環1の移動方向を示す矢印、 図9における3は操作ピン、4は静翼軸である。 Conventionally, in a compressor, it is often required from the viewpoint of the performance of the compressor to change the mounting angles of a plurality of stages of stator vanes during operation. In that case, attach a stationary blade by attaching a lever to the shaft of the stationary blade, providing a pin at the tip of the lever, engaging the pin with the groove of the operating ring provided on the outer periphery of the vehicle compartment, and moving the operating ring. I was trying to change the corners. In this case, there are two types of movements of the operation ring: one that moves in the axial direction and one that rotates. 8 and 9 show a conventional example in which the operation ring is moved in the axial direction to operate the blade angle. FIG. 9 shows the relationship between the lever of the stationary blade 2 and the operating ring 1, and is an enlarged view of the D portion of FIG. The operation ring 1 is supported at its outer peripheral portion by a plurality of support shafts 12 via a bush 13 so as to be slidable in the axial direction, and both ends of the support shaft 12 are fixed to the vehicle compartment. As described above, the operation ring 1 is slidably supported without being tilted in the axial direction, and is moved in the axial direction by the servo motor 11. In addition, 10 is an arrow indicating the moving direction of the operating ring 1, 3 in FIG. 9 is an operating pin, and 4 is a stationary blade shaft.

【0003】[0003]

【考案が解決しようとする課題】[Problems to be solved by the device]

一般に静翼取付角を運転中に操作するに際して最も大切な事は、何れの段もそ の段内の静翼2の全てが全部同じ角度を維持する事である。一列内で翼角にバラ ツキがあると、その段に前後する動翼は一回転する間に変動する流れの中を通過 する事になり、その周期的な変動力により疲労破断に至る事がある。 そこで各列内の翼角のバラツキを無くする為には、操作環は常に傾いたり、倒 れたりする事なく案内されながら動かなければならない。操作環には係合する各 静翼の流れの反力と各摺動部の摩擦力が働く。これらの力は翼毎に多少差はある ものの、翼は全て円周上等分に配されているので合力は大略中心にある。 Generally, the most important thing in operating the stationary blade mounting angle during operation is that all the stationary blades 2 in each stage maintain the same angle. If the blade angles vary within one row, the blades before and after that stage will pass through the flow that fluctuates during one rotation, and the cyclic fluctuating force may lead to fatigue fracture. is there. Therefore, in order to eliminate variations in blade angles within each row, the operating ring must always be guided and moved without tilting or falling. The reaction force of the flow of each stationary vane and the frictional force of each sliding part work on the operation ring. Although these forces are slightly different for each wing, the total force is roughly at the center because all the wings are evenly distributed on the circumference.

【0004】 一方操作力の着力点は操作環の外周にあるので、操作環1には常にモーメント が働き、そのモーメントは図8においては2個のブッシュ13で負担され、かつ 同モーメントは操作環1を傾けるように働く。またこのモーメントに抵抗する反 力は、ブッシュ13の間隔が短い程大きく、ブッシュ13と支持軸12の摩耗、 摩擦力の増加、支持軸12の変形の増加、或いはブッシュ13や支持軸12が摩 耗してガタを生じた時には、操作環1の傾きが大きくなるなどの問題があった。 従って操作環1を傾き難く支持する為には、モーメントに抵抗するブッシュ1 3間の距離を可能な限り大きくする事が望ましい。圧縮機の可変静翼段数は、そ の圧縮機の要求される性能により種々あるが、多くは前方数段程度である。そし てこの場合には図8に見られる様に、操作環1はその直径に比べて長さが短い。 即ち、操作力のモーメント(これは半径に比例する)に比べてブッシュ支持間隔 が短い事になり、操作環1は傾き易くなる。 従って短い操作環1に対しても、操作力によるモーメントに対し有効に抵抗す る、即ち支持間隔の長い、傾き難い支持方法が強く望まれていた。 本考案は前記従来の問題を解決するために提案されたものである。On the other hand, since the point of application of the operating force is on the outer circumference of the operating ring, a moment always acts on the operating ring 1, and the moment is borne by the two bushes 13 in FIG. Work like tilting one. Also, the reaction force that resists this moment increases as the distance between the bushes 13 decreases, causing wear of the bushes 13 and the support shaft 12, increase of frictional force, increase of deformation of the support shaft 12, or abrasion of the bushes 13 and the support shaft 12. There was a problem that the operating ring 1 was greatly tilted when it was worn and loosened. Therefore, in order to support the operation ring 1 so as not to tilt, it is desirable to increase the distance between the bushes 13 that resist moments as much as possible. The number of variable vane stages of the compressor varies depending on the performance required of the compressor, but most of them are about several stages forward. Then, in this case, as shown in FIG. 8, the operating ring 1 has a shorter length than its diameter. That is, the bush support interval is shorter than the moment of the operating force (which is proportional to the radius), and the operating ring 1 is likely to tilt. Therefore, even with respect to the short operating ring 1, a supporting method that effectively resists the moment due to the operating force, that is, the supporting interval is long and the inclination is difficult, has been strongly desired. The present invention has been proposed to solve the above conventional problems.

【0005】[0005]

【課題を解決するための手段】[Means for Solving the Problems]

このため本考案は、圧縮機の静翼取付角を可変にするものであって、静翼の軸 にレバーを取付け、同レバー先端のピンを車室外周に設けた操作環の円周溝に係 合させると共に、同操作環を軸方向に動かして翼角を変更するようにした静翼操 作環において、同操作環の外周に複数の突起を設け、一方その突起に嵌まり合う 部分ネジ溝を設けたブラケットを車室に固定するか、ブラケットに突起を設け、 操作環に突起が嵌まり込むネジ溝を設けて同操作環を回転させることにより、操 作環が軸方向に移動して静翼翼角を調整するもので、これを課題解決のための手 段とするものである。 For this reason, the present invention makes the stator blade mounting angle of the compressor variable.A lever is attached to the shaft of the stator blade, and a pin at the tip of the lever is installed in the circumferential groove of the operating ring provided on the outer periphery of the vehicle compartment. In a stationary vane operating ring in which the operating ring is moved in the axial direction to change the blade angle, a plurality of protrusions are provided on the outer periphery of the operating ring, and a partial screw that fits into the protrusion Fix the bracket with the groove in the vehicle compartment, or provide the bracket with a projection and provide a screw groove in which the projection fits into the operation ring and rotate the operation ring to move the operation ring in the axial direction. It adjusts the vane angle of the stationary blade, and this is the means to solve the problem.

【0006】[0006]

【作用】 本考案では周上に複数個の突起と、それに嵌まり合う部分ネジ溝を持ったブラ ケットを設け、それにより操作環を支えて回転させる。本考案ではネジ溝のリー ドを適当に選定する事により、所要軸方向の移動量に対して周方向操作量をサー ボモータに好ましい値に任意に決定出来ると云う効果が得られる。In the present invention, a plurality of protrusions and a bracket having a partial thread groove to be fitted to the protrusions are provided on the circumference, and the operation ring is supported and rotated by the bracket. According to the present invention, by appropriately selecting the lead of the thread groove, it is possible to arbitrarily determine the amount of circumferential operation with respect to the amount of movement in the required axial direction to a value preferable for the servomotor.

【0007】[0007]

【実施例】【Example】

以下本考案を図面の実施例について説明すると、図1〜図7は本考案の実施例 を示す。20は操作環で外周に突起、即ち図ではピン25とローラ26を設ける 。一方車室に固定されたブラケット24には部分ネジ溝27を設ける。そしてブ ラケット24の内周側は、また操作環20の外周の支持面を兼ねている。この支 持面は操作力の大きさによっては、適当な転がり軸受を利用して摩擦力を減らす 事も可能である。またローラ26は、ブラケット24の部分ネジ溝27に嵌まり 込み、操作環20を周方向に回転させる事により、ネジの進み分軸方向に移動す る。一方ブラケット24に突起を設け、操作環20に突起が嵌まり込むネジ溝を 設けて、操作環20を回転させるようにしてもよい。 The present invention will be described below with reference to the embodiments of the drawings. FIGS. 1 to 7 show the embodiments of the present invention. Reference numeral 20 denotes an operation ring, which is provided with a protrusion on the outer circumference, that is, a pin 25 and a roller 26 in the figure. On the other hand, the bracket 24 fixed to the vehicle compartment is provided with a partial thread groove 27. The inner peripheral side of the bracket 24 also serves as the outer peripheral support surface of the operation ring 20. Depending on the magnitude of the operating force, this bearing surface can also reduce the frictional force by using an appropriate rolling bearing. Further, the roller 26 is fitted in the partial thread groove 27 of the bracket 24 and rotates the operation ring 20 in the circumferential direction, so that the roller advances in the screw advancement axis direction. On the other hand, the bracket 24 may be provided with a projection, the operation ring 20 may be provided with a screw groove into which the projection is fitted, and the operation ring 20 may be rotated.

【0008】 図8に示した従来例では、長さ方向にモーメントに抵抗する2点の支持点を設 けたので、支持点間隔を広く採る事が出来ない。 本考案の実施例では、図2に示す様に円周上に支持点を配する。ところで操作 環20を支持するには、モーメントに有効に抵抗する様でなければならない事は 勿論であるが、先ず常に操作環20が傾斜しないで案内されていなければならな い。 そこで本考案では、周上に複数個の突起(幾何学的に平面は3点で定まる。従 って支持点は少なくとも3点でなければならない。また4点以上であると、全て が正しく同じ寸法でないと今度は不静定支持になる。実際には弾性変形や多少の ガタは避けられないので、4個所、5個所、…も採用される。)と、それに嵌ま り合う部分ネジ溝(円周の一部分)27を持ったブラケット24を設け、それで 操作環20を支える。そして操作環20を回転させる。In the conventional example shown in FIG. 8, since two supporting points that resist moment in the length direction are provided, it is not possible to set a wide supporting point interval. In the embodiment of the present invention, supporting points are arranged on the circumference as shown in FIG. By the way, in order to support the operation ring 20, it is needless to say that the operation ring 20 must effectively resist the moment, but first, the operation ring 20 must always be guided without being tilted. Therefore, in the present invention, a plurality of protrusions on the circumference (geometrically, the plane is determined by three points. Therefore, the supporting points must be at least three points. If there are four or more points, all are the same. If it is not the size, it will become statically indeterminate support. In reality, elastic deformation and some backlash are unavoidable, so 4 places, 5 places, etc. are also adopted.) A bracket 24 having (part of the circumference) 27 is provided to support the operation ring 20. Then, the operation ring 20 is rotated.

【0009】 すると各支持点でネジの進みに応じた分だけ、軸方向に操作環20を移動させ る。各支持点が幾何学的に等しいネジ溝を持っていれば、操作環20は傾く事な く軸方向に移動する。なお、操作環20は横方向にも固定されねばならないので 、図2〜図7ではブラケット内周は横方向の移動を阻止し、軸方向のみの動きを 許す案内を兼ねている。また突起は摩擦力を減らす為ローラを用いてある。Then, the operation ring 20 is moved in the axial direction by an amount corresponding to the advance of the screw at each support point. If each support point has a geometrically equal thread groove, the operating ring 20 moves in the axial direction without tilting. Since the operating ring 20 must be fixed laterally, the inner circumference of the bracket in FIGS. 2 to 7 also serves as a guide that prevents lateral movement and allows movement only in the axial direction. The protrusions use rollers to reduce friction.

【0010】[0010]

【考案の効果】[Effect of device]

以上詳細に説明した如く本考案によると、操作環の形式は前記の如く軸方向に 操作するものと、周方向に操作するものがあるが、周方向に操作する形式では操 作環に静翼1本宛に対応したレバーのピン穴に係合する穴を半径方向に設けねば ならない。しかしこの半径方向に多数の穴を正確な位置に加工するのは著しくコ ストが高くなる。製作コストからは軸方向移動形が有利である。ところが軸方向 移動形は傾いたり、倒れない様に正確に案内する事が、周方向移動形に比べて困 難である。 しかし本考案によると軸方向移動形式でも、従来に比べて高い正確さで操作環 を案内する事が出来る。なお、ブラケット、ピン、コロなどの製作コストは従来 の支持軸や、それを支える座、ブッシュと大差はない。 As described in detail above, according to the present invention, there are two types of operating rings, one operating in the axial direction and the other operating in the circumferential direction as described above. A hole must be provided in the radial direction that engages with the pin hole of the corresponding lever. However, it is extremely costly to machine a large number of holes in the radial direction at precise positions. The axial movement type is advantageous in terms of manufacturing cost. However, it is more difficult for the axial movement type to guide accurately so that it does not tilt or fall than the circumferential movement type. However, according to the present invention, even with the axial movement type, the operation ring can be guided with higher accuracy than before. The manufacturing cost of brackets, pins, rollers, etc. is not much different from that of conventional support shafts, seats and bushes that support them.

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

【図1】本考案の実施例を示す静翼操作環の1部断面側
面図である。
FIG. 1 is a partial sectional side view of a vane operating ring showing an embodiment of the present invention.

【図2】図1の1部断面正面図である。FIG. 2 is a sectional front view of part 1 in FIG.

【図3】図1のA部の拡大断面図である。FIG. 3 is an enlarged cross-sectional view of a portion A of FIG.

【図4】図2のB部の拡大断面図である。FIG. 4 is an enlarged cross-sectional view of portion B of FIG.

【図5】図3のC〜C断面図である。5 is a sectional view taken along line CC of FIG.

【図6】図5におけるブラケットの斜視図である。FIG. 6 is a perspective view of the bracket in FIG.

【図7】図3に示す突起を設けた操作環の1部を示す斜
視図である。
7 is a perspective view showing a part of the operation ring provided with the protrusion shown in FIG.

【図8】従来の圧縮機における操作環部の側断面図であ
る。
FIG. 8 is a side sectional view of an operating ring portion in a conventional compressor.

【図9】図8におけるD部の詳細図である。9 is a detailed view of a D portion in FIG.

【符号の説明】[Explanation of symbols]

20 操作環 21 操作耳 22 サーボモータにより操作する方向 23 操作杆の動く方向 24 ブラケット 25 ピン 26 ローラ 27 ネジ溝 28 ブラケットを車室に固定するボルト 20 Operating Ring 21 Operating Ear 22 Direction Operating by Servo Motor 23 Moving Direction of Operating Rod 24 Bracket 25 Pin 26 Roller 27 Screw Groove 28 Bolt for fixing the bracket to the passenger compartment

───────────────────────────────────────────────────── フロントページの続き (72)考案者 藤岡 渡 兵庫県高砂市荒井町新浜二丁目8番25号 高菱エンジニアリング株式会社内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Wataru Fujioka 2-8-25, Niihama, Arai-cho, Takasago-shi, Hyogo Takahishi Engineering Co., Ltd.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】 圧縮機の静翼取付角を可変にするもので
あって、静翼の軸にレバーを取付け、同レバー先端のピ
ンを車室外周に設けた操作環の円周溝に係合させると共
に、同操作環を軸方向に動かして翼角を変更するように
した静翼操作環において、同操作環の外周に複数の突起
を設け、一方その突起に嵌まり合う部分ネジ溝を設けた
ブラケットを車室に固定するか、ブラケットに突起を設
け、操作環に突起が嵌まり込むネジ溝を設けて同操作環
を回転させることにより、操作環が軸方向に移動して静
翼翼角を調整することを特徴とする静翼操作環。
Claim: What is claimed is: 1. A stator blade mounting angle of a compressor is variable, wherein a lever is attached to the shaft of the stator blade, and a pin at the tip of the lever is engaged with a circumferential groove of an operating ring provided on the outer periphery of the vehicle compartment. In the stationary vane operating ring in which the operating ring is moved in the axial direction to change the blade angle, a plurality of protrusions are provided on the outer periphery of the operating ring, and a partial thread groove that fits into the protrusion is provided. By fixing the provided bracket to the passenger compartment, or by providing the bracket with a projection and providing a screw groove into which the projection fits, and rotating the operation ring, the operation ring moves in the axial direction and the stationary blade A stationary vane operating ring characterized by adjusting the angle.
JP7884092U 1992-10-21 1992-10-21 Stationary operation ring Withdrawn JPH0637596U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7884092U JPH0637596U (en) 1992-10-21 1992-10-21 Stationary operation ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7884092U JPH0637596U (en) 1992-10-21 1992-10-21 Stationary operation ring

Publications (1)

Publication Number Publication Date
JPH0637596U true JPH0637596U (en) 1994-05-20

Family

ID=13673028

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7884092U Withdrawn JPH0637596U (en) 1992-10-21 1992-10-21 Stationary operation ring

Country Status (1)

Country Link
JP (1) JPH0637596U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI582313B (en) * 2014-07-10 2017-05-11 Mitsubishi Hitachi Power Sys Maintenance and maintenance method of adjustable stator blade device and adjustable blade device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI582313B (en) * 2014-07-10 2017-05-11 Mitsubishi Hitachi Power Sys Maintenance and maintenance method of adjustable stator blade device and adjustable blade device
US10858993B2 (en) 2014-07-10 2020-12-08 Mitsubishi Hitachi Power Systems, Ltd. Variable vane device maintenance method and variable vane device

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