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Multi-degree-of-freedom assembling system suitable for large size equipment assembly in cabin of spacecraft

An assembly system and a technology with a degree of freedom, which is applied to space navigation equipment, space navigation equipment, space navigation ground equipment, etc., can solve problems such as large subjective errors, excessive weight, and low positioning accuracy, so as to improve agility and Safety, reduction of human labor, high safety effect

Active Publication Date: 2019-11-22
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In the existing technology, first of all, the assembly of aerospace products mainly relies on manual operation, which leads to the quality of assembly heavily depending on the assembly technology and experience of the operator, which has a large subjective error and is time-consuming. force, which is not conducive to the completion of assembly work with quality and quantity
Secondly, the assembly process of aerospace products requires simple process equipment such as spreaders and support vehicles as tools for positioning and support. These process equipment are heavy and have poor precision, and there are problems such as unquantifiable component pose adjustment and low positioning accuracy.
At the same time, during the final assembly process of the manned space station project, there are many large and heavy loading equipment in the cabin. Due to their heavy weight and limited installation space, these loading equipment cannot be transported manually under the existing technology. For installation. It is necessary to borrow a certain labor-saving device
[0003] Finally, with the arrival of the final assembly task of the new space station system, the functions of the final assembly products tend to be integrated, the size is getting larger and heavier, and the diversification of the spacecraft body configuration makes the final assembly work conditions more complicated, which has exceeded the current In the stage technology, the manual lift or lifting method can be competent
[0004] At present, heavy-weight products of spacecraft can be assembled by hoisting, but in the cabin, the assembly of heavy-weight equipment products usually adopts the "hanging" hoisting assembly scheme. In the space, heavy products are hoisted by hanging, and the moving direction and reliability are poor
The adjustment of each position and angle depends entirely on the experience and cooperation of the operators, and cannot be quantified and controllable
The weight of the product is carried by hoisting, it is easy to shake during the assembly process, and it is easy to collide with other parts, and the safety is poor.

Method used

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  • Multi-degree-of-freedom assembling system suitable for large size equipment assembly in cabin of spacecraft

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Embodiment Construction

[0023] The multi-degree-of-freedom assembly system applicable to the assembly of equipment in a large cabin of a spacecraft is described below with reference to the accompanying drawings, but this description is only exemplary and is not intended to limit the protection scope of the present invention.

[0024] see figure 1 , figure 1 A two-dimensional schematic diagram of the assembly of the large cabin equipment of the spacecraft is shown. Among them, the multi-degree-of-freedom assembly system suitable for the assembly of large-scale spacecraft equipment in the present invention includes a horizontal track 1, a base 2, a slewing mechanism 3, a vertical track 4, a lifting mechanism 5, a boom drive 6, a small arm drive 7, End effector 8. Inside the cabin of the space station, there are instrument board structures in each area, forming a grid area one by one. In the process of final assembly, the section of the instrument board is transferred, the transfer board is laid, and ...

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Abstract

The invention discloses a multi-degree-of-freedom assembling system suitable for large size equipment assembly in cabin of a spacecraft. The system comprises a small arm drive, a large arm drive, a lifting mechanism, a vertical rail, a swing mechanism, a base, a horizontal rail and a tail end executing function mechanism. A horizontal sliding block device is connected with a guide rail above the horizontal rail, so that the movement of the base and the whole mechanism borne by the base in the horizontal direction is realized; a slewing bearing is fixed to the upper surface of the base, the vertical rail is fixedly connected to the slewing bearing of the swing mechanism, and the large arm drive is installed on the longitudinal guide rail through a vertical sliding block device and moves inthe vertical direction. The lifting mechanism is fixedly connected to the other opposite side face of the vertical rail, overall rotary motion is achieved through a gear installed in a winding drum, the small arm drive is connected with the large arm drive through a turbine speed reduction device, and the small arm drive is used for driving the tail end executing function mechanism to execute actions. According to the invention, the risk of easy shaking in the hoisting process is overcome, the safety is high, the manual labor is reduced, and the assembly agility and safety of the product are improved.

Description

technical field [0001] The invention belongs to the field of manned spaceflight assembly. Specifically, the invention relates to a manned spaceflight assembly method and system suitable for the assembly of equipment in a large cabin of a spacecraft, which can realize the assembly of large equipment in an effective space station in a sealed cabin . Background technique [0002] In the existing technology, first of all, the assembly of aerospace products mainly relies on manual operation, which leads to the quality of assembly heavily depending on the assembly technology and experience of the operator, which has a large subjective error and is time-consuming. Force, is not conducive to the completion of assembly work quality and quantity. Secondly, the assembly process of aerospace products requires simple process equipment such as spreaders and support vehicles as tools for positioning and support. These process equipment are bulky and have poor precision, and there are prob...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G5/00B64G1/12B64G1/22B25J9/10B25J9/16B25J18/00B23P19/00
CPCB23P19/001B25J9/102B25J9/104B25J9/1687B25J18/00B64G1/12B64G1/22B64G5/00
Inventor 王鹏飞易旺民张成立邢帅刘同辉张小东赵晋龙常冬林金晓亮孙振业张丹
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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