直升机飞行参数记录系统设计及典型故障分析研究  

Research on the Design of Helicopter Flight Data Recording System and Typical Fault Diagnosis

作　　者：潘永生[1] 张凤梅 张录龙 Pan Yongsheng Zhang Fengmei Zhang Lulong(Naval Military Representative Office in Harbin, Harbin 150066, China Engineering Department, Harbin Aircraft Industry Group Co. , Ltd. , Harbin 150066, China)

机构地区：[1]海军驻哈尔滨地区航空军事代表室,哈尔滨150066 [2]哈尔滨飞机工业集团有限公司工程技术部,哈尔滨150066

出　　处：《航空工程进展》2017年第1期109-114,共6页Advances in Aeronautical Science and Engineering

摘　　要：飞行参数记录系统能有效提高飞行训练的安全性。根据直升机飞行安全需要,结合工程经验,对直升机加装飞行参数记录系统进行分析研究,介绍飞行参数记录系统的基本组成和原理、加装原则和相关标准以及飞行参数的校准方法;对飞行参数记录系统两个典型故障进行诊断分析,并提出解决方案。飞行参数记录系统相关设计的研究能够为工程技术人员在进行设计应用时提供一种思路和参考。The flight data recording system is an efficient way to improve the safety of flight training.According to flight safety requirements of the helicopter,combined with the engineering experiences,the basic composition and principle of the flight data recording system,recording parameters selection principle and flight parameter calibration method are discussed.Two typical fault diagnosis and solution methods in the application of flight data recording system are listed.This research can provide reference for engineers in the design and application of helicopter flight data recording system.

关 键 词：飞行参数记录系统 记录器 标校 故障诊断 直升机 

分 类 号：V248.2[航空宇航科学与技术—飞行器设计]