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Bearing assembly of floating end of spatial motion component shafting

A technology of space movement and bearing components, which is applied in the aerospace field, can solve problems such as mechanism jamming and lubrication failure, and achieve the effects of high reliability, reduced radial size, and improved utilization

Pending Publication Date: 2020-02-21
SHANGHAI INST OF TECHNICAL PHYSICS - CHINESE ACAD OF SCI
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] In order to solve the problem that due to the temperature difference of the shaft system on the rail, the bearing generates additional stress, which leads to lubrication failure and the mechanism is stuck on the rail
The invention provides a bearing assembly for the floating end of the shaft system of space moving parts, which solves the practical problems of aerospace engineering at present

Method used

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  • Bearing assembly of floating end of spatial motion component shafting

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Embodiment Construction

[0015] Attached below figure 1 It is described in detail in order to better illustrate the structural features and functional features of the present invention, but not to limit the protection scope of the present invention.

[0016] The floating end bearing assembly of the present invention adopts the inner, middle and outer three-layer bearing sleeve design in design. The inner and outer surfaces of the middle bearing sleeve 3 are friction pairs, and the materials used for the bearing sleeves are: the inner bearing sleeve 2 is made of 9Cr18 stainless steel, the middle bearing sleeve 3 is made of aluminum alloy or copper-based alloy and other materials with a large linear expansion coefficient, and the outer bearing sleeve 4 using 9Cr18 stainless steel material. The inner and outer surfaces of the middle bearing sleeve 3, the outer side of the inner bearing sleeve 2 and the inner ring of the outer bearing sleeve 4 are sprayed with molybdenum disulfide solid lubricating film ...

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Abstract

The invention discloses a bearing assembly of a floating end of a spatial motion component shafting. The assembly is formed by combining three layers of bearing sleeves and comprises an inner bearingsleeve, a middle bearing sleeve and an outer bearing sleeve. Molybdenum disulfide solid lubricating films are coated outside the inner bearing sleeve, inside and outside the middle bearing sleeve andinside the outer bearing sleeve, and the inner bearing sleeve and the middle bearing sleeve as well as the middle bearing sleeve and the outer bearing sleeve can relatively rotate. The bearing assembly of the floating end of the spatial motion component shafting has the advantages that the bearing assembly of the floating end is composed of the three layers of bearing sleeves, so that the problemthat the shafting is deformed due to violent temperature alternation of motion components on rails, the shafting bearing is abnormally stressed, and a jam fault occurs can be solved. A three-layer bearing sleeve type design is adopted on the assembly structure, the problem of additional stress caused by axial temperature difference and radial temperature difference on a bearing is solved, particularly the problem of additional radial stress of the bearing in a high-low temperature difference environment caused by mismatching of shaft, bearing and bearing seat materials is solved, and the reliability of the spatial motion components can be effectively improved.

Description

technical field [0001] The invention belongs to the field of aerospace, and relates to a bearing assembly used for the floating end of the shaft system of space moving parts, specifically to solve the additional problem caused by the deformation of the shaft system due to the high temperature difference and high vacuum of the motion mechanism outside the cabin in the space field. The stress causes the lubrication to fail or the friction torque to increase significantly, causing the mechanism to be stuck and the satellite or on-board instruments to fail. Therefore, this component can effectively improve the on-orbit life of moving parts in satellites or on-board instruments, and has great economic benefits. [0002] technical background [0003] With the continuous development of my country's aerospace industry, various types of spacecraft in my country have gradually changed from "experimental" satellites to "applied" satellites, which not only put forward higher requirements...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16C35/02F16C33/12F16C33/10
CPCF16C35/02F16C33/125F16C33/127F16C33/102F16C33/1095
Inventor 刘晓华陈陆淼姚劲刚杨桦郑庚
Owner SHANGHAI INST OF TECHNICAL PHYSICS - CHINESE ACAD OF SCI