MATHEMATICAL MODELLING AND DYNAMIC ANALYSIS OF A BOOSTER STATION DRIVEN BY WZ5G AEROENGINES

Lu Zehua; Ye Bosheng; Yang Yiming; Xu Chaoqun

Volume 2 Issue 3

Jul. 1987

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Article Navigation > Journal of Aerospace Power > 1987 > 2(3): 270-272,287-288

Lu Zehua, Ye Bosheng, Yang Yiming, Xu Chaoqun. MATHEMATICAL MODELLING AND DYNAMIC ANALYSIS OF A BOOSTER STATION DRIVEN BY WZ5G AEROENGINES[J]. Journal of Aerospace Power, 1987, 2(3): 270-272,287-288.

Citation:

Lu Zehua, Ye Bosheng, Yang Yiming, Xu Chaoqun. MATHEMATICAL MODELLING AND DYNAMIC ANALYSIS OF A BOOSTER STATION DRIVEN BY WZ5G AEROENGINES[J]. Journal of Aerospace Power, 1987, 2(3): 270-272,287-288.

Lu Zehua, Ye Bosheng, Yang Yiming, Xu Chaoqun. MATHEMATICAL MODELLING AND DYNAMIC ANALYSIS OF A BOOSTER STATION DRIVEN BY WZ5G AEROENGINES[J]. Journal of Aerospace Power, 1987, 2(3): 270-272,287-288.

Citation:

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MATHEMATICAL MODELLING AND DYNAMIC ANALYSIS OF A BOOSTER STATION DRIVEN BY WZ5G AEROENGINES

1.
Tsinghua University
2.
Wuxi Aeroengine Research Institute

Received Date: 1986-06-01
Publish Date: 1987-07-28

Abstract

Abstract

A split-shaft gas turbine adapted from WZ5G aeroengine is quite suitable for driving a booster compressor station in a long gas pipeline. A mathematical model is established for a booster station with two series centrifugal compressors driven separatelyby the split-shaft gas tnrbine of WZ5G aeroegine. The model is simplified by a static state optimization. Its transfer functions are obtained through a nonsin-gulartransformation. The model is applied to analysing the stability and dynamic responses of the system. Some conclusions are drawn which are helpful to controllingof the long gas pipeline.