A Volterra Progression Model of Nonlinearity Dynamic Respondence of Aero Engine

SONG Zhi-ping; CHENG Li; WEI Rei-xuan

Volume 19 Issue 4

Aug. 2004

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SONG Zhi-ping, CHENG Li, WEI Rei-xuan. A Volterra Progression Model of Nonlinearity Dynamic Respondence of Aero Engine[J]. Journal of Aerospace Power, 2004, 19(4): 577-580.

Citation:

SONG Zhi-ping, CHENG Li, WEI Rei-xuan. A Volterra Progression Model of Nonlinearity Dynamic Respondence of Aero Engine[J]. Journal of Aerospace Power, 2004, 19(4): 577-580.

SONG Zhi-ping, CHENG Li, WEI Rei-xuan. A Volterra Progression Model of Nonlinearity Dynamic Respondence of Aero Engine[J]. Journal of Aerospace Power, 2004, 19(4): 577-580.

Citation:

SONG Zhi-ping, CHENG Li, WEI Rei-xuan. A Volterra Progression Model of Nonlinearity Dynamic Respondence of Aero Engine[J]. Journal of Aerospace Power, 2004, 19(4): 577-580.

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A Volterra Progression Model of Nonlinearity Dynamic Respondence of Aero Engine

1.
Electron and Information Engineering College,Xi'an Jiaotong University, Xi'an710049,China
2.
Engineering college,Air Force Engineering University,Xi'an710038,China

Received Date: 2003-12-17
Rev Recd Date: 2004-05-13
Publish Date: 2004-08-28

Abstract

Abstract

Modeling of nonlinearity dynamic respondence of the aero engine was studied.The dynamic process of the aero engine was described by using the Volterra progression model.And identification arithmetic of the Volterra progression model for aero engines was proposed.It was applied to a certain turbofan engine by imitating the dynamic respondence.The Volterra progression model can describe the dynamic process from low to high rotating speed of aeroengine.
- aerospace propulsion system,
- aero engine,
- nonlinearity dynamic model,
- Volterra progression