航空发动机控制系统的条款符合性方法研究

Method of Verifying Aircraft Engine Control System in Conformity with FAR

为促进我国自主研发的航空发动机控制系统快速发展,并顺利通过美国联邦航空局(FAA,Federal Aviation Administration)适航审定,对发动机控制系统开展了分析研究。以发动机控制系统的发展状况为背景,对FAA先后两次颁布的联邦航空条例(FAR,Federal Aviation Regulation)33.28条款进行梳理研究,从飞机提供的数据、飞机提供的电源、电子/电气零件三个方面提出了条款符合性验证方法的思路。

In order to promote the rapid development of aero-engine control system in China, and successfully pass the Federal Aviation Administration（FAA） airworthiness certification, this paper carries out analysis and study on engine control system. Based on the background of the development of engine control system, the paper studies the 33.28 clause of Federal Aviation Regulation （FAR） issued twice by FAA. The article provides the idea of the method verifying the conformity of the item from the data provided by the aircraft, the power supply provided by the aircraft and the electronic and electrical parts.