Rocket rear fulcrum support adjustment system

A technology for adjusting the system and the rear fulcrum, which is applied to rocket launchers, offensive equipment, weapon types, etc., can solve problems such as high maintenance costs and long infrastructure construction cycles, and achieve improved efficiency, reduced docking and adjustment difficulties, and shortened launches the effect of time

Active Publication Date: 2020-09-01
BEIJING LANDSPACETECH CO LTD
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0002] With the development of aerospace technology, especially the vigorous rise of commercial aerospace in recent years, the traditional "three vertical" launch mode has gradually revealed its shortcomings of long infrastructure construction period and high maintenance cost due to the need for a fixed launch tower. Therefore, a fast, flexible, and low-cost launch mode is needed to meet the launch requirements of commercial spaceflight at the present stage

Method used

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  • Rocket rear fulcrum support adjustment system
  • Rocket rear fulcrum support adjustment system
  • Rocket rear fulcrum support adjustment system

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Embodiment Construction

[0049] In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the following will clearly illustrate the spirit of the content disclosed in the application with the accompanying drawings and detailed descriptions. After any person skilled in the art understands the embodiments of the content of the application , when it can be changed and modified by the technology taught in the content of the application, it does not depart from the spirit and scope of the content of the application.

[0050] The exemplary embodiments and descriptions of the present application are used to explain the present application, but not to limit the present application. In addition, elements / members with the same or similar numbers used in the drawings and embodiments are used to represent the same or similar parts.

[0051] The terms "first", "second", ... etc. used herein do not specifically refer to a sequence or order, nor are they...

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Abstract

The application provides a rocket rear fulcrum support adjustment system, which includes two rocket rear fulcrum support adjustment devices fixedly arranged on both sides of the vertical arm along the width direction of the vertical arm, and the two relative to the length direction of the vertical arm The central axis is symmetrical; the rocket rear fulcrum support adjustment device includes a rotary support, a rotary push unit, a support unit, and a pulling unit; the rotary push unit is arranged between the rotary support and the vertical arm, and is used to push the rotary support to rotate to Make way for the rocket take-off space; the support unit is set on the slewing support, which is used to support the rear fulcrum of the rocket; the pulling unit is connected with the slewing support and the support unit. The support is gradually converted into the pulling of the rocket by the pulling unit. The application can adjust the rocket with multiple degrees of freedom, effectively reduce the difficulty of docking and adjustment when the rocket is reloaded, and significantly improve the efficiency of docking the rocket with the launch pad after erection.

Description

technical field [0001] The application belongs to the technical field of rocket auxiliary support adjustment systems, and in particular relates to a rocket rear fulcrum support adjustment system. Background technique [0002] With the development of aerospace technology, especially the vigorous rise of commercial aerospace in recent years, the traditional "three vertical" launch mode has gradually revealed its shortcomings of long infrastructure construction period and high maintenance cost due to the need for a fixed launch tower Therefore, a fast, flexible, and low-cost launch mode is needed to meet the launch requirements of commercial spaceflight at this stage. [0003] Most of the successful foreign commercial aerospace companies adopt the "three-level" test and launch mode, that is, the launch mode of horizontal assembly, horizontal transfer, horizontal test, and vertical launch. Therefore, it is particularly important and critical to reliably support the rocket body ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 张瑜张彦杰韩召洋韦银利杨俊吴雪
Owner BEIJING LANDSPACETECH CO LTD
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