Abstract: A flap slat control lever and a method for operating the lever are disclosed. The lever includes: a first displacement sensor to detect a displacement of the flap slat control lever and generate a first displacement detection signal; a second displacement sensor to detect the displacement of the flap slat control lever and generate a second displacement detection signal; a first control command module to receive the first displacement detection signal; and a second control command module to receive the second displacement detection signal, wherein the first control command module is in a standby state and the second control command module is in a working state.
Type:
Grant
Filed:
December 26, 2017
Date of Patent:
July 26, 2022
Assignees:
COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD., SHANGHAI AIRCRAFT DESIGN AND RESEARCH INSTITUTE OF COMMERICAL AIRCRAFT CORPORATION OF CHINA
Inventors:
Weida Wang, Xiaoyi Wang, Shaobo Yan, Ji Zhao, Xiangrong Xu, Tong Liu