Rocket supporting platform and rocket pose adjusting method

A technology for supporting platforms and rockets, applied in the directions of rocket launchers, servo motors, servo motor components, etc., and can solve problems such as vertical deflection of core-stage engines

Active Publication Date: 2022-06-24
东方空间技术(山东)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The main purpose of the present invention is to provide a rocket support platform and a rocket attitude adjustment method to solve the problem in the related art that the verticality of the core stage engine is deflected after the booster stage engine is assembled

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  • Rocket supporting platform and rocket pose adjusting method

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Embodiment Construction

[0024] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0025] It should be noted that the terminology used herein is for the purpose of describing specific embodiments only, and is not intended to limit the exemplary embodiments according to the present application. As used herein, unless the context clearly dictates ot...

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Abstract

The invention provides a rocket supporting platform and a rocket pose adjusting method, and the rocket supporting platform is used for supporting a rocket. The rocket supporting platform comprises an oil supply pipeline and an oil return pipeline. The first supporting cylinder group is supported at the bottom of the core body part, the first supporting cylinder group comprises a plurality of first lifting cylinders, first oil inlets of the plurality of first lifting cylinders are all communicated with the oil supply pipeline, and first oil outlets of the plurality of first lifting cylinders are all communicated with the oil return pipeline; and the second supporting cylinder set is supported at the bottom of the boosting part and comprises a plurality of second lifting cylinders, second oil inlets of the second lifting cylinders communicate with the oil supply pipeline, and second oil outlets of the second lifting cylinders communicate with the oil return pipeline. According to the technical scheme, the problem that the perpendicularity of a core-level engine deflects after a boosting-level engine is assembled in the related technology is effectively solved.

Description

technical field [0001] The invention relates to the technical field of aerospace ground support equipment, in particular to a rocket support platform and a method for adjusting the position and attitude of a rocket. Background technique [0002] Vertical assembly and vertical transfer in rocket assembly and transfer transportation have gradually become a trend. Compared with horizontal assembly and horizontal transfer transportation, this saves erection time and equipment, and saves costs to a large extent. In the vertical state ground test, it is close to the state of launch. In this ground test state, the obtained parameters are also more valuable. During vertical assembly, multiple support points are required on the rocket support platform to support the rocket engine. With the installation of different stages of engines, the center of gravity of each stage of the engine will bring about changes in verticality or horizontality. [0003] After completing the assembly of t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F15B11/16F15B13/02F41F3/04
CPCF15B11/16F15B13/02F41F3/04
Inventor 吴考布向伟王永刚李曦黄亚军邢春雷王亚男郝丁
Owner 东方空间技术(山东)有限公司
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