Design of the Electronic Engine Control Unit Performance Test System of Aircraft

被引：3

作者：

Kho, Seonghee ^{[1
]}

Park, Hyunbum ^{[2
]}

机构：

[1] Howon Univ, Dept Def Sci & Technol Aeronaut, 64 Howondae 3gil, Impi 54058, Gunsan, South Korea

[2] Kunsan Natl Univ, Sch Mech Convergence Syst Engn, 558 Daehak Ro, Miryong Dong 54150, Gunsan, South Korea

来源：

AEROSPACE | 2021年 / 8卷 / 06期

基金：

新加坡国家研究基金会;

关键词：

test bench; EECU (electronic engine control unit); turbofan engine; CHALLENGES;

D O I：

10.3390/aerospace8060158

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this study, a real-time engine model and a test bench were developed to verify the performance of the EECU (electronic engine control unit) of a turbofan engine. The target engine is a DGEN 380 developed by the Price Induction company. The functional verification of the test bench was carried out using the developed test bench. An interface and interworking test between the test bench and the developed EECU was carried out. After establishing the verification test environments, the startup phase control logic of the developed EECU was verified using the real-time engine model which modeled the startup phase test data with SIMULINK. Finally, it was confirmed that the developed EECU can be used as a real-time engine model for the starting section of performance verification.

引用

页数：18

共 50 条

[11] Design and Test Evaluation of Full Authority Digital Electronic Control System for an Auxiliary Power Unit
Peng K.
Yang F.
Fan D.
Gou L.
Xiao H.
Jiao C.
Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2018, 36 (06): : 1102 - 1107
[12] The research based on the design of the electronic control unit of uc/os II engine
Qi, G. P.
ENERGY SCIENCE AND APPLIED TECHNOLOGY, 2016, : 139 - 142
[13] Design and verification of engine control system with digital electronic backup
Li, Chen
Wen, Binhe
Zuo, Wei
Gao, Minming
Han, Chongpeng
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2024, 39 (08):
[14] Optimum design, simulation and test of a new flow control valve with an electronic actuator for turbine engine fuel control system
Agh, Seyfoddin Mojallal
Pirkandi, Jamasb
Mahmoodi, Mostafa
Jahromi, Mehdi
FLOW MEASUREMENT AND INSTRUMENTATION, 2019, 65 : 65 - 77
[15] The engine performance LabVIEW virtual instrument test system design
Information and communication engineering instituteNorth university of China National Key Laboratory For Electronic Measurement Technology Taiyuan China Wang Xiao Han YanInstitute of Computer ApplicationShijiazhuang Railway InstituteShijiazhuang ChinaMao WanDuiUFIDA Software COLTDBeijingChinaSi XiaoHong
微计算机信息, 2008, (07) : 65 - 67
[16] Engine Speed Control Unit for an Aircraft Jet Engine with Coolant Injection into the Combustor
Tudosie, Alexandru-Nicolae
2018 INTERNATIONAL CONFERENCE ON APPLIED AND THEORETICAL ELECTRICITY (ICATE), 2018,
[17] The Power Supply Module Design for Diesel Electronic Control Unit's Lift Time Test System
Yin, Jinguan
Su, Tiexiong
Shen, Xiaoyan
Jia, Li
Liu, Tao
Lv, Hui
2017 INTERNATIONAL CONFERENCE ON MECHANICAL, AERONAUTICAL AND AUTOMOTIVE ENGINEERING (ICMAA 2017), 2017, 108
[18] PERFORMANCE ANALYSIS OF AN ENGINE-MOUNTED COMPRESSION SYSTEM FOR AIRCRAFT ENVIRONMENTAL CONTROL
van Heerden, Albert S. J.
Ippedico, Salvatore
Rajendran, David John
Anselmi-Palma, Eduardo
Roumeliotis, Ioannis
Pachidis, Vassilios
Sharpe, Richard
Howarth, Nicholas
PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 1, 2023,
[19] CONTROL UNIT DESIGN FOR A PNOMATIC ENGINE WORKING WITH AN ELECTROMAGNETIC VALVE AND ITS EFFECT ON PERFORMANCE OF THE ENGINE
Gunes, Haluk
Kunt, M. Akif
JOURNAL OF THE FACULTY OF ENGINEERING AND ARCHITECTURE OF GAZI UNIVERSITY, 2016, 31 (01): : 1 - 8
[20] System Design For Aircraft Fuel Control And Maintenance Test-bed
Zhang Chuntang
Wang Shaokun
26TH CHINESE CONTROL AND DECISION CONFERENCE (2014 CCDC), 2014, : 3478 - 3481

← 1 2 3 4 5 →