
基本信息:
- 专利标题: 一种巡飞弹气动发射筒机构
- 专利标题(英):Pneumatic launching canister mechanism for loitering munition
- 申请号:CN201711220886.0 申请日:2017-11-29
- 公开(公告)号:CN107966072A 公开(公告)日:2018-04-27
- 发明人: 罗天培 , 李茂 , 张家仙 , 尹奇志 , 王成刚 , 孙凤伟 , 刘瑞敏 , 张佳 , 尚凯伦 , 孔凡超 , 李伟乐
- 申请人: 北京航天试验技术研究所
- 申请人地址: 北京市丰台区云岗田城中里1号
- 专利权人: 北京航天试验技术研究所
- 当前专利权人: 北京航天试验技术研究所
- 当前专利权人地址: 北京市丰台区云岗田城中里1号
- 主分类号: F41F1/00
- IPC分类号: F41F1/00
The invention provides a pneumatic launching canister structure used for providing an initial speed during launching of loitering munition. The pneumatic launching canister structure comprises a canister body, a piston, a flow-limiting orifice plate, a tying rope, gas generators, an inner bottom plate, a controller, an outer bottom plate and an adjustment lead screw, wherein two gas generators arearranged, and the controller is used for controlling a starting time interval of the two gas generators. The pneumatic launching canister structure provided by the invention has the following beneficial effects: the gas generators are started in succession and release high-pressure gas under the action of the controller after receiving starting signals, the high-pressure gas pushes the piston andthe loitering munition to carry out accelerated movement together through the flow-limiting orifice plate, when the piston moves to the edge of the canister body, the tying rope is tensioned, the piston is separated from the loitering munition under the tension of the tying rope, and rapidly decelerates and stays in a canister, and no overflow of the high-pressure gas is ensured, so that a soundless and lightless launching effect can be realized; in addition, the axial position of the inner bottom plate can be adjusted through the adjustment lead screw, the inside capacity of a launching cavity is changed, and then the effect of changing a launching speed is achieved; and a gas release speed can be controlled through changing the orifice diameter of the flow-limiting orifice plate, and then the effect of changing an overload during launching is achieved.
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F41 | 武器 |
----F41F | 自身管发射子弹或导弹的发射装置,例如加农炮(轻武器入F41C);导弹或鱼雷发射装置;捕鲸炮 |
------F41F1/00 | 用于自身管发射弹丸或导弹的发射装置,例如加农炮;捕鲸炮 |