The invention provides a missile pylon, and relates to the technical field of missile carrying, a missile body is provided with a first connecting part, a guide rail is fixedly arranged in a missile storage cabin, a moving frame is slidably connected with the guide rail, the moving frame has a first state and a second state, and in the first state, the moving frame is fixed to the missile storage cabin; in the second state, the moving frame is separated from the missile storage cabin and slides to the cabin outlet along the guide rail, the starting mechanism is connected with the moving frame and drives the moving frame to be switched from the first state to the second state, the missile connecting piece has a third state and a fourth state, and in the third state, the missile connecting piece is connected with the moving frame and the first connecting part. And when the separating mechanism is in the fourth state, the missile connecting piece is separated from the first connecting part so that the missile can be projected along the hatch outlet, the separating mechanism drives the missile connecting piece to be switched from the third state to the fourth state under the action of mechanical external force, and the separating mechanism is mechanically designed, does not need to be driven by an electric signal, and is reliable in strength and low in failure rate.
本申请提供一种导弹挂架,涉及导弹运载技术领域,导弹本体上设有第一连接部,包括导轨固定设置在储弹舱内,移动架与导轨滑动连接,移动架具有第一状态和第二状态,处于第一状态时,移动架与储弹舱固定;处于第二状态时,移动架与储弹舱分离且沿导轨滑动至出舱口,启动机构与移动架连接,驱动移动架由第一状态切换至第二状态,导弹连接件具有第三状态和第四状态,处于第三状态时,导弹连接件分别与移动架和第一连接部连接,处于所述第四状态时,所述导弹连接件与第一连接部分离,以使导弹沿所述出舱口投射,分离机构受机械外力驱动导弹连接件由第三状态切换至第四状态,分离机构采用机械设计,无需电信号驱动,强度可靠,故障率低。
Guided missile hanging frame
一种导弹挂架
2025-01-17
Patent
Electronic Resource
Chinese
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