Three degree of freedom aircrafts side steering column

• Main Authors: LIAO WENFENG, SUN MIN, WANG JINJIAN, LUO JINLIANG, ZHANG HAIDONG, SHEN WENJING, LONG SIHAI, XIANG XIAOPING, XU YINGHU, ZHU QINQIANG, SHI FEI, ZENG RONG, HUANG RUIQUAN
• Format: Patent
• Language: Chinese; English
• Published: 15.06.2018
• Subjects: AEROPLANES; AIRCRAFT; AVIATION; COSMONAUTICS; HELICOPTERS; PERFORMING OPERATIONS; TRANSPORTING

The utility model relates to a three degree of freedom aircrafts side steering column relates to aircraft design technical field for realize the comfortable driving of aircraft. Steering column divideinto steering column upper segment, steering column middle section and steering column hypomere, rotating displacement and load sensor and fixing on the steering column middle section, the hypomere at steering column is fixed to the fixed box of horizontal hunting, and rotate around the horizontal hunting axle of installing at the fixed box of horizontal hunting simultaneously in steering columnupper segment and steering column middle section, centre that horizontal hunting displacement and load sensor connection steering column middle section and horizontal hunting were fixed box, the utility model discloses a steering column has controlled every single move, lift -over and the driftage of aircraft, and the driver consumes physical power and lacks, accords with human engineering, is particularly suitable for the