The invention provides an aircraft artificial sensing and balancing mechanism, which comprises a tubular shaft, a balancing mechanism, a balancing mechanism and a balancing mechanism, and is characterized in that the tubular shaft comprises an input rocker arm, an output rocker arm and a load mechanism rocker arm; the operation input pull rod is connected with the input rocker arm; one end of the first output pull rod is connected with the output rocker arm; the loading mechanism is connected with the loading mechanism rocker arm, and the composite mechanism is connected with the other end of the first output pull rod; the auxiliary actuator is connected with the composite mechanism; according to the artificial feeling and balancing mechanism for the aircraft, proper pre-tightening force is set in the loading mechanism in the mechanism to counteract reverse force transmission, the phenomenon of reverse force transmission is avoided, and the artificial feeling and balancing functions are provided; the control input of the auxiliary actuator of the stability augmentation system and the manual control input of the main control line system are integrated and then are controlled and output to the irreversible booster, and then the irreversible booster drives the control surface to deflect.
本申请提供了一种飞机人工感觉及配平机构,包括:管轴,包括输入摇臂、输出摇臂以及载荷机构摇臂;操纵输入拉杆,与所述输入摇臂连接;第一输出拉杆,所述第一输出拉杆的一端与所述输出摇臂连接;载荷机构,与所述载荷机构摇臂连接,复合机构,与所述第一输出拉杆的另一端连接;副作动器,与所述复合机构连接;本申请提供的一种飞机人工感觉及配平机构,通过在该机构中的载荷机构设置合适的预紧力抵消“反传力”,避免“反传力”现象,并提供人感及配平功能,以及将增稳系统的副作动器操纵输入与主操纵线系的人工操纵输入综合后操纵输出到不可逆助力器,再通过不可逆助力器驱动舵面偏转。
Aircraft artificial feeling and balancing mechanism
一种飞机人工感觉及配平机构
2023-08-08
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
FUSELAGE POSITIONING MECHANISM (VERSIONS), AIRCRAFT AND AIRCRAFT BALANCING METHOD (VERSIONS)
Europäisches Patentamt | 2019
|Online Contents | 2003
|Balancing of aircraft propellers
Engineering Index Backfile | 1941
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