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Cantilever multi-axis turntable for spacecraft attitude adjustment

A spacecraft and cantilever type technology, applied in the field of large-span cantilever type three-axis attitude adjustment turntable, can solve structural deformation and other problems, achieve the effect of avoiding structural deformation, meeting assembly and testing requirements, and realizing safety protection

Active Publication Date: 2020-02-18
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the above technical problems, the object of the present invention is to provide a large-span cantilever-type three-axis attitude-adjusting turntable for spacecraft, which solves the problem of structural deformation under the cantilever state of large-span and large-mass load, and effectively improves the assembly of products. The openness realizes the requirements of different attitudes of embedded products such as spacecraft high-thrust engines in the process of assembly and testing

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  • Cantilever multi-axis turntable for spacecraft attitude adjustment
  • Cantilever multi-axis turntable for spacecraft attitude adjustment
  • Cantilever multi-axis turntable for spacecraft attitude adjustment

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Embodiment Construction

[0030] The three-axis attitude adjustment platform of the large-span cantilever spacecraft of the present invention will be further described in detail below with reference to the accompanying drawings, but this is only exemplary and is not intended to limit the protection scope of the present invention in any way.

[0031] See Figure 3. Figure 3a It is a front view of a three-axis attitude adjustment platform for a large-span cantilever spacecraft in a specific embodiment of the present invention when the turning ring mechanism is in a vertical state; Figure 3b A side view of a three-axis attitude adjustment platform for a large-span cantilever spacecraft in a specific embodiment of the present invention when the turning ring mechanism is in a vertical state. The three-axis attitude adjustment turntable for a large-span cantilever spacecraft of the present invention includes a support platform (Mechanical frame) 1. Omni-directional moving gear train 2. Lifting system, turnover s...

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Abstract

The invention discloses a large-span cantilever type triaxial posture adjustment turntable for a spacecraft. The turntable comprises a supporting platform, an omnibearing travelling wheel system, a lifting system, an overturning system and a rotating mechanism, wherein the inner side of a C-type ring of an overturning rack is connected with the outer side of a rotating ring through a roller combination, the inner side of the C-type ring surrounds the outer side of the rotating ring, the rotating ring is adjusted to be in a proper assembling, testing or experimenting state, the spacecraft is locked dead by a locking device of the rotating ring, and then related working items of the spacecraft are carried out. According to the invention, opening assembly requirements of embedded products such as a high-thrust engine and the like as well as products such as narrow space pipes and the like of the spacecraft are met, reachability and convenience of operation are achieved, and the problem ofstructural deformation in the large-span and large-mass load cantilever state is solved.

Description

Technical field [0001] The invention belongs to the technical field of spacecraft assembly, and specifically relates to a cantilevered three-axis attitude adjustment turntable with a large span. The turntable can realize the openness of embedded products of the spacecraft and meet the requirements of product assembly and testing. Background technique [0002] With the development trend of large-scale spacecraft products, compact layout, and personalized appearance, the attitude adjustment requirements of spacecraft assembly are becoming more common, and a large turntable is needed to adjust the attitude of the spacecraft to meet the requirements of spacecraft assembly, testing and testing. Demand. [0003] At present, in order to meet the requirements of spacecraft assembly, testing and testing, it is routinely fixedly connected to the two-axis turntable through the bottom connecting flange of the spacecraft, and the spacecraft's attitude adjustment needs are realized through the r...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B25H1/10B25B27/00
CPCB25B27/00B25H1/10
Inventor 冯伟易旺民杨旺陈启威郑圣余王辰星唐赖颖王临政彭国华徐世峰
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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