基于FADEC控制发动机高空模拟试验用的航电模拟器技术研究  

Study on Technology of Avionic Simulator Based on High-Altitude Simulation Test for FADEC Engine

作　　者：张向前 刘龙园 付细能 张文林 Zhang Xiangqian;Liu Longyuan;Fu Xineng;Zhang Weilin(AVIC Hongdu,Jiangxi Nanchang,330024)

机构地区：[1]航空工业洪都

出　　处：《教练机》2019年第3期57-60,共4页Trainer

摘　　要：介绍了某发动机的机载总线通讯环境,着重讨论了基于全权限电子控制(FADEC)控制发动机台架试验用航电模拟器技术,从航电模拟器与外界通讯环境建立、技术实现途径、实现的功能等角度进行了阐述,提出了航电模拟器研制的关键技术。This paper introduces the communication environment for the airborne bus of a certain type of engine, emphatically discusses the technology of the avionic simulator used for FADEC engine test on the test bed in terms of establishment of communication environment between the avionic simulator and periphery, the technology realization approach and functions for technology realization and puts forward the key technology for development of avionic simulator.

关 键 词：FADEC 航电模拟器 ECU 高空模拟试验 

分 类 号：V23[航空宇航科学与技术—航空宇航推进理论与工程]