Mechanical delay separation mechanism for missile body adapter of aircraft

• Main Authors: CHEN YILIN, ZHAN JINGHUA, GONG ZIHUA, FU JUNXING, HAO GUIZHEN, WU HUAQING, CHEN LEI, JIANG YUTAO, ZHAO YUKUN, LU JIE, YU YOUHAO, YAO PANPAN, CHEN YIYUN, LIU TAO, QU SHAOQI
• Format: Patent
• Language: Chinese; English
• Published: 19.09.2023
• 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 utility model relates to the technical field of aircraft adapter separation mechanism design, in particular to an aircraft missile body adapter mechanical delay separation mechanism which comprises an adapter, a push rod, a shape maintaining block, a compression spring, a supporting box, a covering cap and a rotary disc, and the aircraft missile body adapter mechanical delay separation mechanism achieves the function of aircraft adapter mechanical delay separation. And the adapter can be separated from the aircraft only after the turntable rotates by a certain angle, so that the purpose of delayed separation is achieved, and the launching safety is improved. The whole mechanism is compact in structure, and the internal space utilization rate of the projectile body is greatly improved. After the adapter is separated, the upper step of the shape maintaining block can fill the notch of the aircraft skin, and therefore the purpose of maintaining the shape of the outer surface of the aircraft is achieved. 本实用新