Rocket rear fulcrum support adjustment system
A technology for adjusting the system and rear fulcrum, applied in rocket launchers, offensive equipment, weapon types, etc., can solve problems such as high maintenance costs and long infrastructure construction periods, improve efficiency, reduce the difficulty of docking and adjustment, and shorten the launch. effect of time
Active Publication Date: 2020-04-21
BEIJING LANDSPACETECH CO LTD
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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
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[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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The invention provides a rocket rear fulcrum support adjustment system. The rocket rear fulcrum support adjustment system comprises two rocket rear fulcrum support adjustment devices which are fixedlyarranged on two sides of an erecting arm in the width direction of the erecting arm, and the two rocket rear fulcrum support adjustment devices are symmetrical about the central axis of the length direction of the erecting arm; the rocket rear fulcrum support adjustment devices comprise rotary supports, rotary pushing units, supporting units and traction units; the rotary pushing units are arranged between the rotary supports and the erecting arm, and are used for pushing the rotary supports to rotate so as to make way for rocket take-off space; the supporting units are arranged on the rotarysupports, and are used for supporting rear fulcrums of a rocket; and the traction units are connected with the rotary supports and the supporting units, and in the process of rocket erecting, the support of the supporting units to the rocket is gradually converted into the traction of the traction units to the rocket. According to the rocket rear fulcrum support adjustment system, the multi degree of freedom of the rocket can be adjusted, the docking and adjustment difficulty of the rocket during the transfer is effectively reduced, and the docking efficiency of the rocket and a launching platform after the rocket is erected is significantly improved.
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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Login to View More 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