民用飞机铁鸟高升力系统试验接口装置  

Test Interface Device for Iron Bird High Lift System for Civilian Aircraft

作　　者：许锦婷 XU Jin-ting(Shanghai Aircraft Design and Research Institute,State Key Laboratory of Airliner Integration Technology and Flight Simulation,Shanghai 201210)

机构地区：[1]上海飞机设计研究院大型客机集成技术与模拟飞行全国重点实验室,上海200126

出　　处：《航空精密制造技术》2024年第5期47-49,共3页Aviation Precision Manufacturing Technology

摘　　要：民用飞机高升力系统铁鸟试验的目的是在真实的高升力系统和其它模拟反映机上工作环境的条件下,验证高升力系统的功能需求、性能需求、接口等。本文研制一种可以用于民用飞机高升力系统铁鸟试验的襟缝翼计算机试验接口装置,对高升力系统襟缝翼计算机输入输出的ARINC429信号进行采集、存储、解析等,并仿真部分航电机载维护系统功能,用于支持高升力系统研发试验和系统需求验证试验。The high-lift system is one of the most important systems in civil aircraft.The purpose of the high-lift system experiment is to verify the function of the high-lift system under the real high-lift system and other simulated conditions.A flaped computer test interface device is developed.It can be used for iron bird tests of high-lift systems in civil aircraft.The ARINC429 signal from the input and output of the flap computer for the lift system is collected,stored,analyzed,etc.,and some of the aviation onboard maintenance system functions are simulated to support the research and development test of the lift system and the system requirements verification test.

关 键 词：民用飞机 高升力 试验接口装置 

分 类 号：V216.8[航空宇航科学与技术—航空宇航推进理论与工程]