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Arrow body connector capture device

A capture device and connector technology, which is applied in the direction of weapon types, offensive equipment, projectiles, etc., can solve the problems that the connector cannot be used twice, affects the reliability of rocket launch, and damages to accessory products, so as to achieve safe and reliable capture action, The structure is simple and the effect of reducing the accident rate

Active Publication Date: 2020-08-04
BEIJING LANDSPACETECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The detached connector will swing in the air. On the one hand, the detached connector in this way may be baked by the rocket tail flame, making the connector unable to be used again, resulting in a waste of resources; on the other hand, the swinging back and forth The connector may also cause damage to the rocket body and accessories on the rocket body, affecting the reliability of rocket launch

Method used

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  • Arrow body connector capture device
  • Arrow body connector capture device
  • Arrow body connector capture device

Examples

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Embodiment Construction

[0027] Various exemplary embodiments of the present invention are now described in detail, which should not be construed as limitations of the invention, but rather as more detailed descriptions of certain aspects, features, and embodiments of the invention.

[0028] It will be apparent to those skilled in the art that various modifications and changes can be made in the specific embodiments of the present invention described herein without departing from the scope or spirit of the present invention. Other embodiments will be apparent to the skilled person from the description of the present invention. The specification and examples in this application are exemplary only.

[0029] Such as figure 1 Shown is a structural diagram of an arrow body connector capture device provided by the present invention. In the embodiment shown in the drawing, the catching device includes: a frame 2 , a front net assembly 3 , a door swing structure 4 and a rear net assembly 5 . Wherein, the f...

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PUM

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Abstract

The invention provides a rocket connector capturing device. The capturing device comprises a frame, a front net assembly, a door swinging structure and a rear net assembly, wherein the frame is used for being fixedly connected with a rocket lifting arm so as to provide a mounting platform, the front net assembly with a first interception net and an energy storage device is arranged on the frame, wherein the energy storage device is used for bouncing the first interception net to intercept a connector with a pulling structure, the door swinging structure is arranged on the frame and is used forguiding the connector to enter interception space through the pulling structure of the connector, and the rear net assembly with a second interception net is arranged on the frame and is used for forming the interception space with the front net assembly for intercepting the connector. The connector capturing device is simple in structure, high in capturing success rate and easy to produce and maintain, and can be used repeatedly.

Description

technical field [0001] The invention relates to the technical field of rocket launchers, in particular to a rocket body connector capture device. Background technique [0002] Usually, the liquid launch vehicle needs to be connected and refueled through the connector before take-off, and the connector needs to be separated from the rocket body after the refilling is completed. In some existing types of rockets, the disconnection of the connector is achieved by relying on external force to separate the plug before the rocket is ignited, such as using a motor to drive a mechanical plug-in mechanism, an electromagnetic pin spring plug-in mechanism, etc. The detached connector will swing in the air. On the one hand, the detached connector in this way may be baked by the rocket tail flame, making the connector unable to be used again, resulting in a waste of resources; on the other hand, the swinging back and forth The connector may also cause damage to the rocket body and acces...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B15/36
CPCF42B15/36
Inventor 韩召洋吴雪韦银利杨俊张瑜张彦杰
Owner BEIJING LANDSPACETECH CO LTD