|Table of Contents|

Sensitivity analysis of controlling elements on a gas turbine performance test bench(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2009年05期
Page:
56-59
Research Field:
测控与试验
Publishing date:

Info

Title:
Sensitivity analysis of controlling elements on a gas turbine performance test bench
Author(s):
Zhao ZheLiu Baoqin
Beijing Aerospace Propulsion Institute,Beijing 100076,China
Keywords:
gas turbineperformance testlinear small deviation analysis
PACS:
V434
DOI:
-
Abstract:
This paper introduced a gas turbine performance test bench of a liquid rocket engiue. The mass fluxes of air,fuel,water and outlet pressure of the gas turbine were chosen to be the main controlling elements in the system.The dynamical model of every part was established.The effective elements on inlet pressure,inlet temperature and rotating speed of the gas turbine are aIla. 1yzed by using linear small deviation equations.The regulating rule of manual control Was confirmed. The inlet pressure of the gas turbine depended on the air flux.The inlet temperature related with both air flux and fuel flux.The rotating speed Was controlled by the water flux.

References:

[1]沈维道,蒋智敏,童钧耕.工程热力学[M].北京:高等 教育出版社.2001.
[2]樊思齐,徐芸华,盂庆明.航空推进系统控制[M].西 安:西北T业大学出版社.1995.
[3]格列克曼B①著.液体火箭发动机自动调节[M].顾明 初,郁明桂,邱明煜译.北京:宇航出版社。1995.
[4]张育林,刘昆,程谋森.液体火箭发动机动力学理论与 应用[M].北京:科学出版社,2005.
[5]薛定宇,陈阳泉.基于MA‘nAB/simulink的系统仿真技 术与应用[M].北京:清华大学出版社,2002.
[6]张志涌编著.精通MATLAB6.5版[M].北京:北京航空 航天大学出版社。2003.

Memo

Memo:
-
Last Update: 1900-01-01