Inertia release device

• Main Authors: CAO QINGQUAN, YU ZHONGBO, SUI XIANGYING, ZHAO GUISHENG, JIANG HAIHUA, LIAO JINJUN
• Format: Patent
• Language: Chinese; English
• Published: 19.03.2024
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; PERFORMING OPERATIONS; TRANSPORTING

The invention provides an inertia release device, and relates to the technical field of ejection, the inertia release device comprises a track and a sliding unit, the sliding unit comprises a supporting main body, a turnover frame and an elastic supporting mechanism, and the supporting main body is slidably arranged on the track and has an acceleration mode and a deceleration mode. One side of the overturning frame is connected with the supporting body, the other side of the overturning frame is provided with a connecting part, and the overturning frame rotates relative to the supporting body. The elastic supporting mechanism is arranged on the supporting body, in the acceleration mode, the overturning frame deflects backwards to enable the connecting part to be located at the upper position and connected with the ejection part, and the overturning frame is connected with the elastic supporting mechanism so as to drive the ejection part to slide forwards through the connecting part. And in the speed reduction