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    • 90. 发明申请
    • ROTOR SYSTEM STRUCTURAL FAULT ESTIMATION
    • 转子系统结构故障估计
    • US20170073064A1
    • 2017-03-16
    • US15309361
    • 2015-03-05
    • SIKORSKY AIRCRAFT CORPORATION
    • Joshua D. Isom
    • B64C27/00G07C5/08G05B23/02G01L5/13
    • B64C27/006G01L5/0009G01L5/133G01M5/0016G01M5/0041G05B23/0221G05B23/0224G07C5/085
    • One aspect is a structural fault estimation system for a rotor system. The structural fault estimation system includes a plurality of sensors operable to provide a plurality of measured rotor loads and motion of the rotor system. A rotor loads and motion estimator is operable to produce a plurality of estimated rotor loads and motion for the rotor system. A rotor fault estimator is operable to determine residual rotor loads and motion as a difference between the measured rotor loads and motion and the estimated rotor loads and motion, and estimate fault magnitudes for the rotor system using least squares relative to fault models and the residual rotor loads and motion. The structural fault estimation system can perform structural fault estimation in real-time on an aircraft while in operation.
    • 一个方面是用于转子系统的结构故障估计系统。 结构故障估计系统包括可操作以提供多个测量的转子负载和转子系统的运动的多个传感器。 转子负载和运动估计器可操作以产生用于转子系统的多个估计的转子负载和运动。 转子故障估计器可操作以将剩余转子负载和运动确定为测量的转子负载与运动与估计的转子负载和运动之间的差值,并且使用相对于故障模型的最小二乘法和剩余转子来估计转子系统的故障幅度 负载和运动。 结构故障估计系统可以在飞机上实时执行结构故障估计。