The invention relates to the field of vibration reduction of helicopter control systems, in particular to a vibration reduction pedal device of a helicopter. The device comprises a damping pedal (1) with a pedal plate (4), a pedal mounting transverse pipe (2) and a pedal mounting vertical rod (3), the damping pedal (1) is mounted on the pedal mounting vertical rod (3) through the mounting transverse pipe (2); the damping pedal (1) is integrated with an anti-resonance vibration isolation design.
本发明涉及直升机操纵系统减振领域,特别涉及一种直升机减振脚蹬装置。该装置包括:具有脚蹬踏板(4)的减震脚蹬(1)、脚蹬安装横管(2)、脚蹬安装立杆(3);减振脚蹬(1)通过安装横管(2)安装在脚蹬安装立杆(3)上;减震脚蹬(1)融入反共振隔振设计。
Helicopter damping pedal device
一种直升机减振脚蹬装置
2023-08-01
Patent
Electronic Resource
Chinese
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