FHA method for VBV position control function of FADEC system based on aero-engine dynamic model

被引：0

作者：

Ding Shuiting ^{[1
]}

Qiu Tian ^{[1
]}

Liu Xiaofeng ^{[1
]}

Zhang Shuguang ^{[1
]}

机构：

[1] Beihang Univ, Airworthiness Technol Res Ctr, Beijing 100191, Peoples R China

来源：

2ND INTERNATIONAL SYMPOSIUM ON AIRCRAFT AIRWORTHINESS (ISAA) | 2011年 / 17卷

关键词：

airworthiness; aero-engine dynamic model; full authority digital engine control system; functional hazard assessment; VBV position control;

D O I：

10.1016/j.proeng.2011.10.070

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Traditional Functional Hazard Assessment (FHA) method is hard to identify those engine effects which lack of visualization. In order to solve this problem, this paper develops a model-based FHA method for Variable Bleed Valve (VBV) position control function, performs two groups of simulations by using aero-engine dynamic model, and introduces an exemplary FHA for VBV position control function based upon simulation results. The application of this method shows that it is feasible and effective. (C) 2011 Published by Elsevier Ltd. Selection and/or peer-review under responsibility of Airworthiness Technologies Research Center NLAA, and Beijing Key Laboratory on Safety of Integrated Aircraft and Propulsion Systems, China

引用

页数：13

共 50 条

[1] FHA method for FADEC system based on aero-thermodynamics model
Ding, Shui-Ting
Qiu, Tian
Liu, Xiao-Feng
Liu, Chuan-Kai
Gong, Lei
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2012, 27 (05): : 1185 - 1193
[2] Function Modelling and Simulation Analysis of Aero-engine VBV
Sun, Zhaorong
Wang, Xu
MANUFACTURING TECHNOLOGY, 2023, 23 (04): : 538 - 544
[3] FADEC TAKES OVER LEADING ROLE IN AERO-ENGINE CONTROL
不详
CONTROL AND INSTRUMENTATION, 1981, 13 (04): : 23 - 23
[4] Transient Control Method of Aero-Engine Based on Dynamic Optimization Data
Huang R.-Y.
Huang J.-Q.
Pan M.-X.
Tuijin Jishu/Journal of Propulsion Technology, 2021, 42 (02): : 459 - 466
[5] Aero-engine dynamic model based on an improved compact propulsion system dynamic model
Zheng, Qiangang
Wang, Yong
Jin, Chongwen
Zhang, Haibo
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2021, 235 (07) : 1036 - 1045
[6] An aero-engine U-control method based on LPV model
Chen, Jiajie
Wang, Jiqiang
Hu, Zhongzhi
Dimirovski, Georgi Marko
IFAC PAPERSONLINE, 2020, 53 (02): : 3886 - 3891
[7] Model predictive control based on ADMM for aero-engine
Shan R.
Li Q.
He F.
Feng H.
Guan T.
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 45 (06): : 1240 - 1247
[8] Dynamic model updating of an aero-engine casing
Ma, S.-C., 1600, Beijing University of Aeronautics and Astronautics (BUAA) (28):
[9] Fault Simulation and Function Verification of the Aero-engine Control System Based on Hardware in Loop
Li, Gengwei
Hao, Binbin
Dong, Jiuxiang
PROCEEDINGS OF THE 33RD CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2021), 2021, : 5393 - 5396
[10] Compensator based improved model predictive control for Aero-engine
Pang, Shuwei
Wang, Tao
Cong, Jingmei
Chen, Hongyi
Li, Qiuhong
Zhou, Wenxiang
Fu, Xueting
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2024,

← 1 2 3 4 5 →