JPS61281933A - Balance testing instrument for high-speed centrifugal compressor - Google Patents
Balance testing instrument for high-speed centrifugal compressorInfo
- Publication number
- JPS61281933A JPS61281933A JP12359285A JP12359285A JPS61281933A JP S61281933 A JPS61281933 A JP S61281933A JP 12359285 A JP12359285 A JP 12359285A JP 12359285 A JP12359285 A JP 12359285A JP S61281933 A JPS61281933 A JP S61281933A
- Authority
- JP
- Japan
- Prior art keywords
- casing
- rotor
- centrifugal compressor
- balancing test
- compressor
- 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
Links
Landscapes
- Testing Of Balance (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、定期検査時などにプラントの据付場所で常用
回転数で釣合試験を行い得るようにした高速遠心圧縮機
の釣合試験装置に関する@〔従来の技術〕
高性能、高圧、高速の遠心圧縮機のロータは、その−例
をあげれば15,000kW程度の軸動力を吸収するも
ので、約15.00 Orpmを常用回転数とし、この
回転数は2次と3次の軸危険速度の間にある。[Detailed Description of the Invention] [Field of Industrial Application] The present invention provides a balance test device for a high-speed centrifugal compressor that allows a balance test to be performed at a normal rotation speed at the installation site of a plant during periodic inspections, etc. [Conventional technology] The rotor of a high-performance, high-pressure, high-speed centrifugal compressor absorbs, for example, about 15,000 kW of shaft power, and has a normal rotational speed of about 15.00 Orpm. , this rotational speed lies between the secondary and tertiary shaft critical speeds.
このような高速遠心圧縮機では、インペラの僅かな変形
や軸の経年変化による曲りKよって不釣合が発生し、定
期点検時に不釣合の修正を必要とする場合がある。この
ときロータの常用回転数が、軸危険速度の2次と3次の
間にあるときには、低速回転によって不釣合を修正する
ことができず、常用回転状態で修正しなければならない
。In such a high-speed centrifugal compressor, unbalance may occur due to slight deformation of the impeller or bending K of the shaft due to aging, and the unbalance may need to be corrected during periodic inspection. At this time, when the normal rotational speed of the rotor is between the second and third order of the shaft critical speed, the unbalance cannot be corrected by low-speed rotation, and must be corrected in the normal rotational state.
一方圧縮機が高圧の場合には耐圧強度上、ケーシングが
軸方向に組立てられた垂直分割形いわゆるバレル形と−
ab、構造上の制約から、一般に釣合おもりの着脱は、
圧縮機が正規に組立てられた状態では、外部から行うこ
とができない。On the other hand, when the compressor is high pressure, due to its pressure resistance, the casing is vertically split, so-called barrel type, in which the casing is assembled in the axial direction.
ab.Due to structural constraints, the attachment and detachment of the counterweight is generally done as follows:
This cannot be done externally when the compressor is properly assembled.
このため従来の技術では、現地で常用使用時の状態で試
験するフィールドバランス法と、工場に持ち帰って常用
回転数で試験する方法が採られている。For this reason, conventional technology employs the field balance method, in which the vehicle is tested on-site under conditions of normal use, and the method of taking it back to the factory and testing it at the normal rotation speed.
しかし前者は不釣合量とその位置を発見することが困難
で、トライオン(Try−on )を繰返し、その都度
ケーシングの分解組立を行うために、経済面と工期面で
甚だ困難である。一方後者は駆動原動機に問題が伴って
いる。すなわち電動機で駆動する場合は、電動機が30
00又は3600 rpmの一定回転のため、極めて多
種類の増速歯車装置をもたねばならない。また、蒸気タ
ービンで駆動する場合も、同じ様に危険速度や翼の共振
回避又は強度上から運転範囲は制限され、過去に販売し
た圧縮機の種類何れをも対応可能である様に試験設備を
整えておく事は実用上容易ではない。又海外プラントで
はロータの工場への輸送と返送はその期間、費用、輸送
途上での事故の可能性と輸出入通関手続等多くの問題が
ある。However, in the former case, it is difficult to discover the amount of unbalance and its position, and the try-on is repeated, and the casing must be disassembled and reassembled each time, which is extremely difficult in terms of economy and construction time. On the other hand, the latter has problems with the driving engine. In other words, when driving with an electric motor, the motor is 30
Due to the constant rotation of 0.00 or 3600 rpm, it is necessary to have a very large variety of speed increasing gears. In addition, when driving with a steam turbine, the operating range is similarly limited due to critical speed, blade resonance avoidance, and strength considerations, and test equipment has been set up to be able to handle any type of compressor that has been sold in the past. In practice, it is not easy to keep it in order. In addition, in overseas plants, there are many problems in transporting rotors to and from the factory, such as the period, cost, possibility of accidents during transportation, and import/export customs clearance procedures.
上記のように従来の釣合試験方法では、フィールドバラ
ンス法によると熟練者でも数回にわたるトライオンを行
わねばならずコストおよび工期面に問題があり、工場持
ち帰シ法によると高価な設備が必要となる。また多額の
費用を要する。As mentioned above, with the conventional balance test method, even an experienced person must carry out multiple try-ons using the field balance method, which poses problems in terms of cost and construction time, while the factory take-home method requires expensive equipment. Become. It also requires a large amount of cost.
したがりて本発明においては、遠心圧縮機の据付けられ
たその場所で常用速度での釣合試験を行うことができ、
しかも不釣合修正のための釣合おもりの着脱に伴うケー
シングの分解組立を不用とすることができることを解決
すべき技術的課題とする。Therefore, in the present invention, a balancing test can be performed at the location where the centrifugal compressor is installed at the normal speed,
Moreover, it is a technical problem to be solved that it is possible to eliminate the need for disassembling and assembling the casing when attaching and detaching the counterweight for unbalance correction.
本発明では、釣合おもり着脱用窓が形成された釣合試験
用ケーシングに高速遠心圧縮機の回転部分が収容される
。上記ケーシングは真空ポンプ等の減圧手段により真空
にされる。セして ′回転部分の主軸が貫通する
ケーシングの該当部位には真空状態が保持できるように
シール装置が設けられる。また圧縮機の回転部分は自在
継手により駆動機と結合される。この駆動機には実用機
が用いられる。In the present invention, a rotating portion of a high-speed centrifugal compressor is housed in a balance test casing in which a window for attaching and detaching a counterweight is formed. The casing is evacuated by a pressure reducing means such as a vacuum pump. Then, a sealing device is installed at the corresponding part of the casing through which the main shaft of the rotating part passes through, so as to maintain a vacuum state. Further, the rotating portion of the compressor is coupled to the drive machine by a universal joint. A practical machine is used for this drive machine.
上記の技術的手段においては、実用機が適用された駆動
機の駆動力を、自在継手を介して高速遠心圧縮機の回転
部分に伝達させ、同回転部分を常用回転させて釣合試験
を行う。この釣合試験においては、減圧手段によシケー
シング内が真空にされ、圧縮機の回転部分を高速回転さ
せた時の風損に依る発熱が防止される。そして釣合おも
りの着脱はケーシングに設けられた窓を使用して行われ
る。In the above technical means, the driving force of the drive machine to which the practical machine is applied is transmitted to the rotating part of the high-speed centrifugal compressor via a universal joint, and the rotating part is normally rotated to conduct a balance test. . In this balance test, the inside of the casing is evacuated by the pressure reducing means to prevent heat generation due to windage damage when the rotating part of the compressor is rotated at high speed. The counterweight is attached and detached using a window provided in the casing.
以下本発明に係る高速遠心圧縮機の釣合試験装置の一実
施例を第1図を参照して詳細に説明する。DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of a balance test device for a high-speed centrifugal compressor according to the present invention will be described in detail below with reference to FIG.
第1図において、複数個のインペラ1が焼ばめまたはキ
ーによシ主軸2に取シ付けられた高速遠心圧縮機のロー
タ20は、実用機の軸受3と軸受台4によって後部側が
支えられ、一方前部は自在継手5と駆動機側後部軸受6
の支持台7によって支えられている。ロータ20は、圧
縮機の据付場所において、複数個のリプ8で補強された
釣合試験用の円筒形ケーシング9内に収容される。また
主軸2がケーシング9を貫通する個所には夫々両側に気
密性の高いシール装置10が設けられる。このシール装
置10は実用機のものをそのiま使用するのが望ましい
が、試験装置専用のシール装置を使用してもよい。In FIG. 1, a rotor 20 of a high-speed centrifugal compressor, in which a plurality of impellers 1 are attached to a main shaft 2 by shrink fit or keys, is supported at the rear by bearings 3 and bearing stands 4 of a practical machine. , while the front part has a universal joint 5 and a rear bearing 6 on the drive side.
It is supported by a support stand 7. The rotor 20 is housed in a cylindrical balancing test casing 9 reinforced with a plurality of lips 8 at the compressor installation site. Furthermore, sealing devices 10 with high airtightness are provided on both sides of each location where the main shaft 2 passes through the casing 9. Although it is desirable to use the sealing device 10 of a practical device, a sealing device specifically designed for a test device may be used.
ケーシング9には減圧手段、例えば真空ポンプ(図示せ
ず)に接続される管7ランジ1ノと釣合おもり着脱用の
複数個の窓12が設けられる。The casing 9 is provided with a tube 7 flange 1 connected to a pressure reducing means, such as a vacuum pump (not shown), and a plurality of windows 12 for attaching and detaching the counterweight.
なおケーシング9は水平もしくは垂直面で2分割され7
ランノによって結合される。また自在継手5によって結
合される駆動機は実用機が使用され、蒸気ターピ/、電
動機、ガスタービン、回収タービン等測れでもよい。同
様に軸受6および自在継手5も実用機のものが使用され
る。Note that the casing 9 is divided into two on the horizontal or vertical plane.
Combined by Ranno. Further, the drive unit connected by the universal joint 5 may be a practical machine, such as a steam turbine, an electric motor, a gas turbine, or a recovery turbine. Similarly, the bearing 6 and the universal joint 5 are those of a practical machine.
さて、上記の構成においては、管7ランノ11に接続さ
れた図示せぬ真空ポンプによりケーシング9内が真空に
される。このケーシング9内の真空度はロータ20を高
速回転させた時の風損に依る発熱を防止するのに必要な
値であればよく、この状態はシール装置10によシ保持
される。そしてこの状態で、実用機である駆動機を駆動
し、その駆動力をロータ20に伝えることによ)同ロー
タ20を常用回転させて釣合試験を行う。この釣合試験
における釣合おもりの着脱は、窓12を介して行うこと
ができる。Now, in the above configuration, the inside of the casing 9 is evacuated by a vacuum pump (not shown) connected to the pipe 7 runno 11. The degree of vacuum within the casing 9 may be any value necessary to prevent heat generation due to wind damage when the rotor 20 is rotated at high speed, and this state is maintained by the sealing device 10. In this state, the rotor 20 is normally rotated (by driving a practical driving machine and transmitting its driving force to the rotor 20), and a balance test is performed. In this balancing test, the counterweight can be attached and detached through the window 12.
本発明によれば、高速遠心圧縮機の釣合試験が、その据
付場所で、しかも釣合おもりの着脱のためにケーシング
の分解組立を行うことなく、高精度且つ迅速に実行でき
る。また常用回転時の動力は真空中での空転損失のみで
極めて少なく、試験用ケーシングは耐圧強度を必要とし
ない真空容器ですむので極めて安価に製作できる。According to the present invention, a balance test of a high-speed centrifugal compressor can be performed quickly and accurately at the installation site, and without disassembling and reassembling the casing for attaching and detaching the balance weight. In addition, the power required during regular rotation is extremely small due to only idling loss in a vacuum, and the test casing can be manufactured at a very low cost since it is a vacuum container that does not require pressure resistance.
したがって本発明によれば、コストの低減、プランド休
転期間の短縮および信頼性の向上を図ることができる。Therefore, according to the present invention, it is possible to reduce costs, shorten the plant downtime period, and improve reliability.
第1図は本発明の一実施例に係る高速遠心圧縮機の釣合
試験装置の断面図である。
2・・・主軸、5・・・自在継手、9・・・ケーシング
、10・・・シール装置、12・・・窓、20・・・ロ
ータ。FIG. 1 is a sectional view of a balance test device for a high-speed centrifugal compressor according to an embodiment of the present invention. 2... Main shaft, 5... Universal joint, 9... Casing, 10... Seal device, 12... Window, 20... Rotor.
Claims (1)
ングと、このケーシングに設けられた釣合おもり着脱用
窓と、上記回転部分の主軸が貫通する上記ケーシングの
該当部位に設けられたシール装置と、上記ケーシング内
を真空にする減圧手段と、上記圧縮機の回転部分に駆動
機の駆動力を伝達する自在継手とを具備し、上記駆動機
に実用機を用い、圧縮機の据付場所において常用回転で
釣合試験を行うようにしたことを特徴とする高速遠心圧
縮機の釣合試験装置。A balance test casing that accommodates the rotating part of a high-speed centrifugal compressor, a window for attaching and removing the counterweight provided in this casing, and a sealing device provided in the corresponding part of the casing through which the main shaft of the rotating part passes through. and a pressure reducing means for evacuating the inside of the casing, and a universal joint for transmitting the driving force of the drive machine to the rotating part of the compressor, using a practical machine as the drive machine, and installing the compressor at the location where the compressor is installed. A balance test device for a high-speed centrifugal compressor, characterized in that the balance test is performed under normal rotation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12359285A JPS61281933A (en) | 1985-06-07 | 1985-06-07 | Balance testing instrument for high-speed centrifugal compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12359285A JPS61281933A (en) | 1985-06-07 | 1985-06-07 | Balance testing instrument for high-speed centrifugal compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS61281933A true JPS61281933A (en) | 1986-12-12 |
Family
ID=14864417
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP12359285A Pending JPS61281933A (en) | 1985-06-07 | 1985-06-07 | Balance testing instrument for high-speed centrifugal compressor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS61281933A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8808096B2 (en) | 2009-03-27 | 2014-08-19 | Ricardo Uk Limited | Flywheel |
US9273755B2 (en) | 2009-03-27 | 2016-03-01 | Ricardo Uk Limited | Method and apparatus for balancing a flywheel |
CN105486453A (en) * | 2015-11-26 | 2016-04-13 | 中国航空工业集团公司哈尔滨空气动力研究所 | Test equipment for measuring inertial load of aircraft under vacuum condition |
US9391489B2 (en) | 2010-11-17 | 2016-07-12 | Ricardo Uk Limited | Magnetic coupler having magnets with different magnetic strengths |
CN106930958A (en) * | 2015-12-31 | 2017-07-07 | 中国核动力研究设计院 | The dynamic balance test method of mass of medium in a kind of simulation pump impeller channel |
US9704631B2 (en) | 2009-03-27 | 2017-07-11 | Ricardo Uk Limited | Flywheel |
US9718343B2 (en) | 2011-04-20 | 2017-08-01 | Ricardo Uk Limited | Energy storage system having a flywheel for a vehicle transmission |
-
1985
- 1985-06-07 JP JP12359285A patent/JPS61281933A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8808096B2 (en) | 2009-03-27 | 2014-08-19 | Ricardo Uk Limited | Flywheel |
US9273755B2 (en) | 2009-03-27 | 2016-03-01 | Ricardo Uk Limited | Method and apparatus for balancing a flywheel |
US9704631B2 (en) | 2009-03-27 | 2017-07-11 | Ricardo Uk Limited | Flywheel |
US9391489B2 (en) | 2010-11-17 | 2016-07-12 | Ricardo Uk Limited | Magnetic coupler having magnets with different magnetic strengths |
US9718343B2 (en) | 2011-04-20 | 2017-08-01 | Ricardo Uk Limited | Energy storage system having a flywheel for a vehicle transmission |
CN105486453A (en) * | 2015-11-26 | 2016-04-13 | 中国航空工业集团公司哈尔滨空气动力研究所 | Test equipment for measuring inertial load of aircraft under vacuum condition |
CN106930958A (en) * | 2015-12-31 | 2017-07-07 | 中国核动力研究设计院 | The dynamic balance test method of mass of medium in a kind of simulation pump impeller channel |
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