Control damping force adjusting mechanism for rotary accelerator platform

• Main Authors: WANG PING, HUANG WANLI, WU JUN, QIU KAIFANG, CHEN ENTAO, ZHANG QIJUN, LUO HENGYI
• Format: Patent
• Language: Chinese; English
• Published: 18.06.2024
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention provides a damping force adjusting mechanism for operation of a rotary accelerator platform. The damping force adjusting mechanism comprises a panel, a rotary knob assembly, a gear assembly I, a support I, a gear assembly II, an accelerator lever assembly and a base assembly, wherein the rotary knob assembly, the gear assembly I, the support I, the gear assembly II, the accelerator lever assembly and the base assembly are installed on the panel. The gear assembly I is meshed with the rotary knob assembly through a bevel gear, the gear assembly II is meshed with the gear assembly I through a cylindrical gear, the throttle lever assembly is installed between the gear assembly II and the base assembly, and the support I is located at the front end of the gear assembly II. The device has the characteristics that the control damping force can be continuously and steplessly adjusted, the damping force is convenient to adjust, the integration degree is high, and the requirements of different operators