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 t...