Gust compensation system and method for aircraft

• Main Authors: CAICEDO RAFAEL E, YAMASHIRO HISAKO, ABDEL-MOTAGALY KHALED, HO ALEXANDER C, STREFLING PAUL C, NAJMABADI KLOUMARS, SIU TZE L, DALLARA CHRISTOPHER D
• Format: Patent
• Language: Chinese; English
• Published: 21.12.2016
• Subjects: AEROPLANES; AIRCRAFT; AVIATION; CONTROLLING; COSMONAUTICS; HELICOPTERS; PERFORMING OPERATIONS; PHYSICS; REGULATING; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES; TRANSPORTING

A gust compensation system is disclosed and configured to adaptively reduce gust loads exerted into an aircraft. The gust compensation system may include a first sensor proximate to a front of the aircraft. The first sensor is configured to output a first signal. A second sensor may be distally located from the front of the aircraft. The second sensor is configured to output a second signal. A gust signal sub-system is configured to receive the first and second signals and generate a gust signal based on analysis of the first and second signals. The gust signal sub-system outputs the gust signal and may modify a load parameter signal in response to the gust signal exceeding a load alleviation threshold. 本申请公开种阵风补偿系统，其经配置以适应性地减小施加到飞行器内的阵风载荷。阵风补偿系统可以包括临近飞行器的前部的第传感器。第传感器经配置以输出第信号。第二传感器可以位于飞行器的前部的远侧。第二传感器经配置以输出第二信号。阵风信号子系统经配置以接收第和第二信号并且基于对第和第二信号的分析生成阵风信号。阵风信号子系统输出阵风信号并且可以响应于阵风信号超过载荷减轻阈值而修改载荷参数信号。