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A 6-DOF Parallel Attitude Adjustment Platform with Overlapped Installation Space and Single-Stage Stroke

A technology with installation space and degrees of freedom, which is applied in the field of docking and assembly of large and heavy equipment, and can solve problems such as insufficient structural space, large structural size, and structural size limitations of the attitude-adjusting platform.

Active Publication Date: 2021-09-14
YANSHAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Insufficient structural space is a common problem in existing attitude-adjusting platforms, especially the structural size in the height direction is large and difficult to lower
Large-scale aerospace components are mostly heavy-duty equipment, and the assembly is subject to multiple restrictions such as site size, supporting equipment, and interface height space, so the structural size of the attitude-adjusting platform is also strictly limited

Method used

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  • A 6-DOF Parallel Attitude Adjustment Platform with Overlapped Installation Space and Single-Stage Stroke
  • A 6-DOF Parallel Attitude Adjustment Platform with Overlapped Installation Space and Single-Stage Stroke
  • A 6-DOF Parallel Attitude Adjustment Platform with Overlapped Installation Space and Single-Stage Stroke

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Embodiment Construction

[0030] Below in conjunction with embodiment the present invention is described in further detail:

[0031] In order to detail the technical content, structural features, achieved goals and effects of the present invention, the following will be described in detail in conjunction with the accompanying drawings.

[0032] Such as Figure 1 to Figure 3 Shown: a 6-degree-of-freedom parallel attitude-adjusting platform with overlapping single-stage strokes in installation space, including a 6-degree-of-freedom branch chain leg 1, a moving platform 6, a control system cabinet 7 for controlling the movement of the parallel attitude-adjusting platform, and a control system cabinet 7. Power storage battery 8, the moving platform 6 is a rectangular or rhombus frame structure, the 6 degrees of freedom branch chain legs 1 are provided with four and symmetrically arranged at the corners of the front end and the rear end of the moving platform 6, and the moving platform 6 The corners of the...

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Abstract

The invention discloses a 6-degree-of-freedom parallel attitude adjustment platform with coincident installation space and single-stage stroke, which includes a 6-degree-of-freedom branch chain leg, a moving platform, a control system cabinet for controlling the movement of the parallel attitude adjustment platform, and a power supply for the control system cabinet. The battery, the 6-DOF branch chain leg includes an X-direction horizontal movement module, a Y-direction horizontal movement module, a Z-direction lifting module and a ball pair outrigger module, and the Z-direction lifting module is located between the X-direction horizontal movement module and the Y-direction horizontal movement module. In the middle of the mobile module, the control system cabinet realizes the six-degree-of-freedom attitude adjustment of the attitude adjustment platform by controlling the movement of the X-direction horizontal movement module and the Y-direction horizontal movement module and the lifting of the Z-direction lifting module. The present invention adopts a modular structure and Combination of spatial positions can not only transform and reorganize the existing platform technical equipment to increase its attitude adjustment function, but also can be used as an independent 6-degree-of-freedom attitude adjustment platform.

Description

technical field [0001] The invention belongs to the technical field of butt joint assembly of large and heavy equipment, in particular to a parallel posture adjustment platform with overlapping single-stage strokes and 6 degrees of freedom for installation spaces. Background technique [0002] In the field of aerospace, such as satellite large components, spacecraft cabins, launch vehicles, etc., all involve attitude adjustment and docking assembly of large and heavy components and equipment. The traditional posture-adjusting docking assembly is mainly manual operation with the aid of auxiliary equipment, and the assembly efficiency and precision are low, which has become a bottleneck in the development of the industry. [0003] The butt assembly of large aerospace components needs to be completed by adjusting the six degrees of freedom of the components. At present, in order to realize the 6-DOF movement of the component to be adjusted, that is, the space 3-DOF movement an...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B25J9/00B25H1/14
CPCB25H1/14B25J9/0033
Inventor 邱雪松毕宫鑫琦周玉林李卓冯英琦周子安
Owner YANSHAN UNIV