A docking device and aerial bomb

A technology of a docking device and a projectile body is applied in the field of aviation bombs to achieve the effects of convenient and fast operation, small vertical occupation space, and easy processing.

Active Publication Date: 2020-12-18
北京航天飞腾装备技术有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is: to overcome the deficiencies of the prior art, to provide a docking device and an aerial bomb, which is suitable for the docking and separation operation of the wing assembly and the missile body in the aviation weapon with the gliding wing. The technical solution invented can quickly and conveniently realize the docking and separation of the gliding wing and the missile body, avoiding the problems of complicated parts, cumbersome operation and long time-consuming in the previous docking form

Method used

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  • A docking device and aerial bomb
  • A docking device and aerial bomb
  • A docking device and aerial bomb

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Embodiment Construction

[0035] In order to make the object, technical solution and advantages of the present invention clearer, the implementation manner of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0036] figure 1 is an assembly drawing of the aerial bomb according to the present invention; figure 2 is the general assembly drawing of the glider wing assembly according to the present invention; image 3 It is an exploded schematic view of some structural members of the glider wing assembly according to the present invention; Figure 4 is a general assembly drawing of the projectile according to the present invention.

[0037] The aerial bomb 1 according to the present invention comprises: a gliding wing assembly 2 , a projectile body assembly 4 , the projectile body assembly is the projectile body, and a docking device 13 for docking and separating the wing assembly 2 and the projectile body assembly 4 .

[0038] The glider wi...

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Abstract

The invention discloses a docking device. The docking device comprises two hooks, a bracket, a screw member, two connecting rods and a nut member. The screw member comprises a first connecting section, a second connecting section and a third connecting section, and the first connecting section, the second connecting section and the third connecting section are fixedly connected. The first connecting section is rotatably and fixedly connected with the bracket. The second connecting section is connected with the nut member in a threaded mode. The third connecting section is connected with an external hanging beam in a threaded mode. The thread screwing direction between the second connecting section and the nut member is the same with the thread screwing direction between the third connecting portion and the external hanging beam. The two ends of the nut member are correspondingly and rotatably connected with first end rods of the two connecting rods. Second end rods of the two connecting rods are correspondingly and rotatably connected with first hinged portions of the two hooks. Second hinged portions of the two hooks are rotatably and fixedly connected with the external hanging beam. The docking device is convenient and quick to operate, and the docking and separating operation of a gliding missile wing assembly and a bomb body can be completed only by operating a single structural member.

Description

technical field [0001] The invention relates to a docking device and an aerial bomb, belonging to the field of aerial bombs. Background technique [0002] As the main tool for aircraft to carry out combat missions, aviation weapons, after nearly a century of development, have developed from few to many, from near to far, from small to large, and from weak to strong. , A series of weapons with different uses. Among them, the types of weapons used for air-to-ground attacks are mainly aerial bombs. [0003] In order to increase the strike distance and realize the strike outside the defense zone, the most commonly used method for ordinary aerial bombs is to use gliding wings. The connection forms of the gliding projectile wing and the projectile body include band connection, transfer lug connection, and bolt connection, but the above connection forms all have the problems of complicated connection forms, cumbersome installation operations, and long-term application. Contents...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B10/38F42B25/00
CPCF42B10/38F42B25/00
Inventor 李晓伟宋永刚张俊冯谦何鸿霏刘海静刘国昌宗俊杰张雷曾屹荣
Owner 北京航天飞腾装备技术有限责任公司
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