AW609民用倾转旋翼传动系扭转稳定性分析及认证试验活动

Ahmad Haidar, Luca Belluomini, A. Trezzini
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引用次数: 0

摘要

莱昂纳多直升机AW609倾转旋翼机的认证包括首次在民用飞机上对倾转旋翼机传动系统架构进行认证。本文提出了一种基于simulink的线性分析方法,可以预测整个飞行包线的扭转稳定性以及对重要设计参数的灵敏度。本文还介绍了在认证试验活动中进行的地面和飞行试验方法。总结了实验数据的后处理,并将认证测试活动的结果作为模型相关表示。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
AW609 Civil Tiltrotor Drive Train Torsional Stability Analysis and Certification Test Campaign 
The certification of the Leonardo Helicopters AW609 tiltrotor includes certifying, for the first time, the tiltrotor drive train architecture in a civilian aircraft. This paper presents a Simulink-based linear analysis that predicts torsional stability across the flight envelope as well as sensitivity to important design parameters. The paper also describes the ground and flight-test methodology carried out in the certification test campaign. The post-processing of experimental data is summarized, and results from the certification test campaign are presented as model correlation.
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