JPS60111093A - Surging preventing apparatus for axial-flow compressor - Google Patents
Surging preventing apparatus for axial-flow compressorInfo
- Publication number
- JPS60111093A JPS60111093A JP21614083A JP21614083A JPS60111093A JP S60111093 A JPS60111093 A JP S60111093A JP 21614083 A JP21614083 A JP 21614083A JP 21614083 A JP21614083 A JP 21614083A JP S60111093 A JPS60111093 A JP S60111093A
- Authority
- JP
- Japan
- Prior art keywords
- compressor
- pressure ratio
- pressure
- detector
- ratio
- 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
- Control Of Positive-Displacement Air Blowers (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の利用分野〕
この発明は軸流圧縮機に係り、特にサージング等n:、
縮機の不安定住fJJ域での運転を避ける必要のある場
合に好適な軸流圧縮機のサージング防IF、装置に関す
るものである。[Detailed Description of the Invention] [Field of Application of the Invention] The present invention relates to an axial flow compressor, and particularly to surging, etc.
This invention relates to a surging prevention IF and device for an axial flow compressor suitable for cases where it is necessary to avoid operation of the compressor in the unstable fJJ region.
近年、ガスタービンの高温化と共に、これに用いるl’
lll流圧縮機の高圧力比化が進んでおり、このため段
当り圧力比がt、3〜1.5に達するものも出現【7て
いる。これに伴ない安定作動域がせばまり、ガスタービ
ンの始動性や制御性に問題を生寸゛る場合がある。第1
図は通常の4nfr流圧縮流圧一般的特性を示す。第1
ト4において、曲%! 1. + 2・・・4は圧縮機
回転数一定の場合の流量と吐出圧力の特性を示し、点線
はサージングラインを示す7通り;(°の軸流圧縮機の
場合、点線の右側が安定作動域であるが、左側領域では
サージング、旋回失速などを生ずるため圧縮機の安定動
作が出来ない。このような圧縮機の不安定領域では圧縮
機内の圧力変動が急増して翼の振動や軸振動を増大させ
、はなはだしい時には翼の破損事故に至ることすらある
。In recent years, with the rise in temperature of gas turbines, the l'
The pressure ratio of 1/2 flow compressors is increasing, and as a result, some models with a per-stage pressure ratio of t, 3 to 1.5 have appeared [7]. As a result, the stable operating range becomes narrower, which may lead to problems in the startability and controllability of the gas turbine. 1st
The figure shows the general characteristics of a typical 4nfr flow compressed fluid pressure. 1st
In t4, the song%! 1. + 2...4 shows the characteristics of flow rate and discharge pressure when the compressor rotation speed is constant, and the dotted line shows the surging line in 7 ways; However, in the left side area, surging, rotational stall, etc. occur, so the compressor cannot operate stably.In such an unstable area of the compressor, pressure fluctuations inside the compressor rapidly increase, causing blade vibration and shaft vibration. In extreme cases, this can even lead to wing damage.
したがって圧縮機の作動点を変化させて使用する時には
、このような不安定域に入らぬよう監視制御する圧縮機
のサージング防止制御装置が必要となる。従来用いられ
ているサージング防止装置をそなえた軸流圧縮機の構成
を第2図に示す。軸流圧縮機はケージング6の内側に取
付けられた複数個の静翼列7と静翼列の間に動翼列8を
そなえて回転するロータ9から構成されている。第2図
の構成において、予め予備試験でめた圧縮機−の特性マ
ツプが記憶装置14に記憶されている。圧縮機の吐出圧
検出器11および流量検出器12からの出力は演算装置
13に導かれる。演算装置13からの出力は放風弁制御
装置]5に導かれ、圧縮機の作動点が前記記憶装置14
に記憶されている圧縮機特性マツプ上、安定域にあるか
不安定域にあるかを比較判定する。圧縮機の作動点を変
化させて使用する時、圧縮機作動点が圧縮機の安定域か
ら不安定域に到達すると放風弁10を開き、安定作動域
内に留るよう制御する、このようにしてサージング域/
\の突入を阻11−することが出来る。Therefore, when the compressor is used by changing its operating point, a surging prevention control device for the compressor is required to monitor and control the compressor to prevent it from entering such an unstable region. FIG. 2 shows the configuration of a conventional axial flow compressor equipped with a surging prevention device. The axial flow compressor is composed of a plurality of rows of stator blades 7 attached to the inside of a casing 6 and a rotor 9 that rotates with a row of rotor blades 8 provided between the rows of stator blades. In the configuration shown in FIG. 2, a compressor characteristic map determined in advance through a preliminary test is stored in the storage device 14. Outputs from the compressor discharge pressure detector 11 and flow rate detector 12 are led to an arithmetic unit 13. The output from the arithmetic device 13 is guided to the blow-off valve control device]5, and the operating point of the compressor is stored in the memory device 14.
A comparison is made to determine whether the compressor is in the stable region or the unstable region on the compressor characteristic map stored in the compressor characteristic map. When the operating point of the compressor is changed and used, when the compressor operating point reaches the unstable region from the stable region of the compressor, the blow-off valve 10 is opened and controlled so as to remain within the stable operating region. surging area/
It is possible to 11- block the intrusion of \.
従来の豪、トージンク防I]二装置では前述のごとく、
圧縮画の流量検出器イテ必要どずろ。通常の圧縮機に用
いる流づ、計は−7:IIf′i1精度上の観点から流
量a1の上、下流に11.管部(通常、」二干流合け−
で管径の20〜30倍の長さ)を要す。このため、圧縮
機の配管が長くなり配管費用が増大する欠点がある。As mentioned above, in the conventional Australian and Torzink Defense I] two devices,
It is necessary to use a compressed flow rate detector. The flow rate meter used in a normal compressor is -7:IIf'i1 From the viewpoint of accuracy, the flow rate is 11. Pipe part (usually ``Nihanryuagake-'')
(20 to 30 times the length of the pipe diameter). For this reason, there is a drawback that the piping of the compressor becomes long and the piping cost increases.
この発明は上述のJj項に基づきなされたもので。 This invention was made based on the above-mentioned item Jj.
安価でかつ確実な制御を行うことが出来る軸流圧縮機の
サージング防止装置を提供することを目的としている、
〔発明の(既要〕
この発明間軸流圧縮機の作動点の判定を圧縮機の流量を
吐出圧力により行う従来の方法に代え、修正回転数と圧
力比で判定することにより圧縮機流星測定用の長い配管
を設置することなく、確度の高いサージング域止が出来
るとこに着目してなされたものである。通常の軸流圧縮
機の特性図を第3図に示す。第3図では前述の第1図と
異なり、たて軸には圧縮機の圧力比π、横軸には修正流
量dパラメータ回転数には修正回転数百を用し)てしA
る。圧力比π、修正流量G、修正回転数にの定義式は以
下の通りである。The purpose of this invention is to provide a surging prevention device for an axial flow compressor that can perform inexpensive and reliable control. Instead of the conventional method of determining the flow rate based on discharge pressure, we focused on the fact that by determining the flow rate using corrected rotational speed and pressure ratio, it is possible to stop the surging region with high accuracy without installing long piping for measuring compressor meteors. The characteristic diagram of a normal axial flow compressor is shown in Fig. 3. In Fig. 3, unlike Fig. 1 described above, the vertical axis shows the pressure ratio π of the compressor, and the horizontal axis shows the pressure ratio π of the compressor. (Use the corrected number of revolutions for the corrected flow rate d parameter and the number of revolutions)
Ru. Definition formulas for the pressure ratio π, the corrected flow rate G, and the corrected rotational speed are as follows.
π= P d / P s ・・・・(1)Q = 、
”T” s / P s G == (2)n = n
/ 、斤1 ・・・・(3)ここに Pd:圧縮機吐
出圧力(kg/m2ab5)PS:++ 入口圧力(I
I)
Ts: II 入口湿度(I<)
G : 〃 流 量
n: 〃 回転数
一般に圧縮機の特性は圧縮機の父萼r力、入口温度によ
り影響を受けるが上述のように圧力比、修正流量、修正
回転数をパラメータにして特性を整理すれば圧縮機の入
口状態の影響は補正される。π= P d / P s ... (1) Q = ,
"T" s / P s G == (2) n = n
/, 1 loaf...(3) Here Pd: Compressor discharge pressure (kg/m2ab5) PS: ++ Inlet pressure (I
I) Ts: II Inlet humidity (I<) G: 〃 Flow rate n: 〃 Rotation speed In general, the characteristics of a compressor are affected by the compressor's calyx force and inlet temperature, but as mentioned above, the pressure ratio, correction If the characteristics are organized using the flow rate and corrected rotational speed as parameters, the influence of the compressor inlet condition can be corrected.
すなわち、第3図のようなマツプで整理すれば、π炉晶
452椋1+ X l−1(+能の鬼等を受けかい〜楠
正回転数一定ライン上で不安定域に突入する圧力比を読
み取り、横軸を修正回転数nでブロン1−すると第4図
に示すように表わされる。第4図ではサージラインの下
方に安定域、上方に不安定域がある。In other words, if we organize it in a map like the one shown in Figure 3, π furnace crystal 452 1 + When the ratio is read and the horizontal axis is plotted with the corrected rotational speed n, it is expressed as shown in Fig. 4. In Fig. 4, there is a stable region below the surge line and an unstable region above it.
第4図の特性を予め測定し、ておけば、細流圧縮機の修
■回転数を圧力比から安定作動域か不安定作動域かの判
定が出来る。以上述べたごとく、この発明は圧縮機の修
正回転数と圧力比から圧縮機の安定、不安定の判定を行
うサージング防止装置を提供するものである。If the characteristics shown in FIG. 4 are measured in advance, it is possible to determine whether the rotational speed of the trickle compressor is in the stable operating region or unstable operating region from the pressure ratio. As described above, the present invention provides a surging prevention device that determines whether a compressor is stable or unstable based on the corrected rotational speed and pressure ratio of the compressor.
〔発明の実施例〕
以下、この発明の実施例を第5図に従い更にくわしく説
明する。Jl+流圧縮機はケーシング6の内側に取付け
られた複数個の静翼列7とこれら静翼列の間に動翼列8
をそなえて回転するロータ9から構成されている。圧縮
機の入口部には圧縮機入口圧力検出器16、入口温度検
出器17、圧縮機吐出圧力検出器1jが、また、ロータ
上には圧縮機ロータの回転数を検出する回転数検出器1
8が設けられている。また、入口圧力検出器J6、入口
温度検出器17、吐出圧力検出器11、回転数検出器1
8の出力は、演算装置13に導かれ、圧縮機の圧力比、
修正回転数を算出する。記憶装置14には予め行った予
備試験により圧縮機の修正回転数と限界圧力比の関係が
記憶されている。演算装置13から出力さ九る圧縮機の
作動点圧力比と記憶装置14の限界圧力比を比較し、圧
力比が限界圧力比に達すると放風弁制御装置15により
放風弁を開放し、サージング領域への突入を叩出するこ
とが出来る。[Embodiments of the Invention] Hereinafter, embodiments of the present invention will be described in more detail with reference to FIG. The Jl+ flow compressor has a plurality of stator blade rows 7 installed inside a casing 6 and a rotor blade row 8 between these stator blade rows.
It consists of a rotor 9 that rotates with a rotor 9. At the inlet of the compressor, there is a compressor inlet pressure detector 16, an inlet temperature detector 17, and a compressor discharge pressure detector 1j, and on the rotor there is a rotation speed detector 1 for detecting the rotation speed of the compressor rotor.
8 is provided. In addition, an inlet pressure detector J6, an inlet temperature detector 17, a discharge pressure detector 11, a rotation speed detector 1
The output of 8 is led to the calculation device 13, and the pressure ratio of the compressor,
Calculate the corrected rotation speed. The storage device 14 stores the relationship between the corrected rotational speed of the compressor and the critical pressure ratio based on a preliminary test conducted in advance. Comparing the operating point pressure ratio of the compressor output from the calculation device 13 with the limit pressure ratio of the storage device 14, and when the pressure ratio reaches the limit pressure ratio, the blow-off valve is opened by the blow-off valve control device 15, It is possible to strike out into the surging area.
以」二連へたごとく、この発明では従来のサージング防
止装置と異なり、流量、吐出圧力により圧縮機作動点の
判定を行う代りに、圧力比と修正回転数により圧縮機の
作動点の判定を行う。このため、圧縮機下流の長い流厭
配管が不要となり安価で確度の高い軸流圧縮機のサージ
ング防止装置4に提供できる効果がある。To summarize, this invention differs from conventional surging prevention devices in that instead of determining the compressor operating point based on the flow rate and discharge pressure, the compressor operating point is determined based on the pressure ratio and corrected rotation speed. conduct. Therefore, there is no need for a long flow pipe downstream of the compressor, and an inexpensive and highly accurate surging prevention device 4 for an axial flow compressor can be provided.
第1図、第3図、第4図は軸流圧縮機の特性装置の概略
図、第5図はこの発明のサージング防止装置の概略図で
ある。
6・・・々−シング、7・静翼列、8・動翼列、9・・
・ロータ、10・・・放風弁、11・−・吐出圧力4が
1出器、13・・演算装置、14・記憶装置、15・放
原、41制御装置、16・・・入[1圧力@t?、器、
17人「1温度検出器、18・・回もミ数検出器。
代理人 弁理−1,高樒明孟 \、
(、
第 1 図
;i−l (。
第 ZI1211
樋
第 3 ロ
イ1蒐ト正シ丸111′ zj下
VJ 4 口
]1, 3, and 4 are schematic diagrams of a characteristic device for an axial flow compressor, and FIG. 5 is a schematic diagram of a surging prevention device of the present invention. 6...Sing, 7. Stator blade row, 8. Moving blade row, 9..
・Rotor, 10... Air discharge valve, 11... Discharge pressure 4 is 1 output, 13... Arithmetic device, 14. Storage device, 15. Discharge, 41 Control device, 16... Input [1 Pressure @t? ,vessel,
17 people: 1 temperature detector, 18... time number detector. Agent: Patent attorney-1, Gao Akimeng \, (, Figure 1; i-l (. Round 111' zz lower VJ 4 mouths]
Claims (1)
器、入口温度を検出する人口温度検出器、圧縮機吐出圧
力を検出する吐出圧力検7j5器、圧縮機ロータの回転
数を検出する回転数検出器および前記入口圧力検出器、
人[1温度検出器、吐出圧力検出器、回転数検出器から
の出力を用いて圧縮機の圧力比、修正回転数を算出する
?t;【孫装置、才9よび予め前記圧Ii!機の限界圧
力比を記憶させた記憶装置、およびfi!f記演算装置
で算出した圧力比と前記記Fj、装置に記憶しである限
界圧力比とを比較し、前記算出圧力比が、前記限界圧力
比より大の時に前記放風弁の開度を増し、圧縮機の圧力
比が前記限界圧力比以内に留まるよう制御する放風弁制
御装置を設けたことを特徴とする軸流圧縮機のサージン
グ防止装冒。[Claims] Input pressure detector for detecting the pressure of the compressor, a population temperature detector for detecting the inlet temperature, a discharge pressure detector for detecting the compressor discharge pressure, a compression a rotation speed detector for detecting the rotation speed of the machine rotor and the inlet pressure detector;
[1] Calculate the pressure ratio and corrected rotation speed of the compressor using the outputs from the temperature detector, discharge pressure detector, and rotation speed detector? t; [Sun device, 9 years old and the above pressure Ii! A storage device that stores the machine's critical pressure ratio, and fi! Compare the pressure ratio calculated by the calculation device f with the limit pressure ratio stored in the device, and when the calculated pressure ratio is greater than the limit pressure ratio, adjust the opening degree of the blowoff valve. A surging prevention equipment for an axial flow compressor, further comprising a blow-off valve control device for controlling the pressure ratio of the compressor to remain within the limit pressure ratio.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21614083A JPS60111093A (en) | 1983-11-18 | 1983-11-18 | Surging preventing apparatus for axial-flow compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21614083A JPS60111093A (en) | 1983-11-18 | 1983-11-18 | Surging preventing apparatus for axial-flow compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS60111093A true JPS60111093A (en) | 1985-06-17 |
Family
ID=16683895
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP21614083A Pending JPS60111093A (en) | 1983-11-18 | 1983-11-18 | Surging preventing apparatus for axial-flow compressor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60111093A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102518598A (en) * | 2011-12-31 | 2012-06-27 | 北京时代科仪新能源科技有限公司 | Centrifugal air compressor and control method and system thereof |
ITFI20130064A1 (en) * | 2013-03-26 | 2014-09-27 | Nuovo Pignone Srl | "METHODS AND SYSTEMS FOR CONTROLLING TURBOCOMPRESSORS" |
US10202980B2 (en) | 2011-10-03 | 2019-02-12 | Ihi Rotating Machinery Engineering Co., Ltd. | Centrifugal compressor apparatus and method for preventing surge therein |
-
1983
- 1983-11-18 JP JP21614083A patent/JPS60111093A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10202980B2 (en) | 2011-10-03 | 2019-02-12 | Ihi Rotating Machinery Engineering Co., Ltd. | Centrifugal compressor apparatus and method for preventing surge therein |
CN102518598A (en) * | 2011-12-31 | 2012-06-27 | 北京时代科仪新能源科技有限公司 | Centrifugal air compressor and control method and system thereof |
ITFI20130064A1 (en) * | 2013-03-26 | 2014-09-27 | Nuovo Pignone Srl | "METHODS AND SYSTEMS FOR CONTROLLING TURBOCOMPRESSORS" |
WO2014154629A1 (en) * | 2013-03-26 | 2014-10-02 | Nuovo Pignone Srl | Methods and systems for controlling turbocompressors |
JP2016514789A (en) * | 2013-03-26 | 2016-05-23 | ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータNuovo Pignone S.R.L. | Method and system for controlling a turbo compressor |
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