两种主动控制喘振现象作动机构的非线性分析

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (5): 38-43.

• 论文 • Previous Articles Next Articles

NONLINEAR ANALYSIS OF TWO ACTUATORS FOR ACTIVE CONTROL ON SURGE PHENOMENON

Nie Chaoqun Chen Jingyi¹

1. Faculty 404, Beijing University of Aeronautics and Astronautics, Beijing, 100083;2. Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, 100080

Received:1995-06-09 Revised:1995-12-03 Online:1996-10-25 Published:1996-10-25

Abstract

Abstract: The actuators with which the active control is applied to the surge phenomenon are discussed. The nonlinear equations of the compression system within the actuators are deduced, and the mechanism of additional small perturbation caused by the actuators is explained qualitatively. Then, the dynamically balanced points of the actual actuator are calibrated. Finally,the nonlinear coupled characteristics between the actual actuator and the centrifugal compression system are analysed in detail.

Key words: surg, active controlactuator, compression system

CLC Number:

Nie Chaoqun Chen Jingyi. NONLINEAR ANALYSIS OF TWO ACTUATORS FOR ACTIVE CONTROL ON SURGE PHENOMENON[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(5): 38-43.

[1]	Gaiqi LI, Dongyang MA, Du LI, Shaorong LIU, Yanmei YANG. Surge test on newly developing civil turboshaft engine under take⁃off condition [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(14): 628190-628190.
[2]	LIU Tingshen, FENG Lihao, WANG Jinjun. Dynamic characteristics of hammershock in S-shaped inlet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 121339-121339.
[3]	LI Zhiping, WANG Mengqi. Airworthiness certification method for aeroengine on stall and surge with inlet distortion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(9): 2947-2957.
[4]	ZHANG Kunyuan. Research progress of hypersonic inlet reverse design based on curved shock compression system [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 274-288.
[5]	Chen Yuchun;Liu Zhende;Yuan Ning;Yu Shouzhi. A New Method of Acceleration Control Law Design for Turbine Engines [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 29(2): 327-332.
[6]	HUANG Jin-quan;CAI Hong-wu. SIMULATION STUDY OF ADAPTIVE NEURAL NETWORK CONTROL FOR INTEGRATED FLIGHT/PROPULSION SYSTEMS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(4): 364-367.
[7]	Hu Jun. NEW SIMPLIFIED MODEL OF POST STALL TRANSIENTS IN AXIAL COMPRESSION SYSTEMS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(2): 207-209.
[8]	Sun Jian-guo;Hu Si-mingJiang;Cai-hong;Sun Wan-feng. A STUDY OF SURGE CONTROL BY USING PULSE CUT-OFF FOR DUAL SPOOL TURBO-JET ENGINE [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(1): 85-89.
[9]	Cui Ji-ya. DEVELOPMENTS OF SUPERSONIC AND TRANSONIC COMPRESSOR [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(6): 322-328.

NONLINEAR ANALYSIS OF TWO ACTUATORS FOR ACTIVE CONTROL ON SURGE PHENOMENON

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 9

Recommended Articles

Metrics

Comments