The air pressure launch canister comprises a canister body, a piston, a console, a first linear material and a second linear material, the canister body is a hollow cylindrical body, and the upper end and the lower end of the canister body are in an open state; the piston and the control console are installed in the cylinder at intervals, the control console is installed close to one opening side of the cylinder, and the space, located on the piston and the control console, in the cylinder is a medium filling area. The sides, close to each other, of the piston and the control table are connected through a first linear material and a second linear material, and the first linear material and the control table are driven by the control table to have a first connected state and a second separated state. When the position between the first linear material and the console is in a second state, the piston moves towards the other opening side of the barrel; and the second linear material is used for limiting the movement stroke of the piston towards the direction of the other opening side of the cylinder body. The launch of the catapult aircraft is realized through ingenious combination of the cylinder body and pneumatic driving.
本发明公开了一种弹射飞行器用气压发射筒,包括筒体、活塞、控制台、第一线性材料、第二线性材料,所述筒体为中空的筒状体,上下两端均为开口状态;所述活塞、控制台呈间隔安装在筒体内且所述控制台靠近筒体的一开口侧安装,所述筒体内位于活塞、控制台的空间为介质填充区;所述活塞、控制台相靠近的一侧通过第一线性材料、第二线性材料连接,通过控制台的驱动使得所述第一线性材料与控制台之间具有连接的第一状态、具有分离的第二状态;在所述第一线性材料与控制台之间为第二状态时,所述活塞朝所述筒体另一开口侧方向运动;所述第二线性材料用于对所述活塞朝所述筒体另一开口侧方向的运动行程进行限位。本发明通过筒体和气压驱动的巧妙结合实现弹射飞行器的发射。
Air pressure launch canister for catapult aircraft and catapult flight equipment
一种弹射飞行器用气压发射筒及弹射飞行设备
2025-05-16
Patent
Electronic Resource
Chinese
IPC: | B64U |
INCENDIARY WARHEAD LAUNCH CATAPULT, COMBUSTION EXPANSION FORCE CATAPULT, NUCLEAR CATAPULT
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