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Calibration device for simulating friction moment of spaceflight bearing under zero gravity

A technology of friction torque and simulated weightlessness, which is applied to bearing-related force sensors, measuring devices, mechanical bearing testing, etc., can solve problems such as excessive starting friction torque, cage deformation and fracture, and poor operation, and achieve low cost , short development cycle and long weightlessness time

Inactive Publication Date: 2016-06-29
YANSHAN UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The working conditions of aerospace bearings are very demanding, and they need to work frequently under conditions such as weightlessness, extreme temperature, and vacuum. In practical applications at home and abroad, there have been "stuck" phenomena. Due to extreme conditions such as gravity, extreme temperature and vacuum, ball bearings with repeated starts and low speeds cannot start and run poorly
The lagging ball bearing shaft ring cannot rotate relative to the seat ring, and even the failure behavior that the starting friction torque is too large leads to deformation and fracture of the cage

Method used

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  • Calibration device for simulating friction moment of spaceflight bearing under zero gravity
  • Calibration device for simulating friction moment of spaceflight bearing under zero gravity
  • Calibration device for simulating friction moment of spaceflight bearing under zero gravity

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Embodiment Construction

[0017] exist Figure 1 to Figure 7 In the schematic diagram of the present invention shown, the upper cover 8 and the lower cover 17 are connected through a column 13 and a guide rod 7 . The upper part of the lower cover is fixedly connected with the supporting seat 2, and the inside of the supporting seat is provided with a through hole, and the supporting platform 1 is placed inside the through hole of the supporting seat. The upper part of the support table is fixedly connected with the support frame 3 and the miniature pressure sensor 16 by screws, and the upper part of the support frame is provided with a fixed ultra-small flat pressure sensor 4 . The ball is placed in the middle of the ultra-small flat pressure sensor. The upper part of the miniature pressure sensor is provided with a shaft 12, and the lower end of the shaft is sleeved with a bearing sleeve 20, and the outside of the bearing sleeve is connected with the inner ring of the lower ring of the thrust ball be...

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Abstract

A space bearing friction torque calibration device under simulated weightlessness, mainly including a support platform, a support base, a support frame, an ultra-small flat pressure sensor, a positioning plate, a sliding sleeve, a guide rod, an upper cover, an adjusting gasket, a positioning bearing, an elastic Retaining ring lower cover, shaft, column, moving plate, electromagnet, miniature pressure sensor, lower cover, lower cover vertical plate, manual lifting platform and bearing sleeve, the weight loss time established by the present invention is relatively different from other tests for simulating weight loss It is relatively long, the development cycle is short, and the cost is very low.

Description

technical field [0001] The invention relates to a calibrating device for simulating the weightless environment in space for aerospace bearings. Background technique [0002] The working conditions of aerospace bearings are very demanding, and they need to work frequently under conditions such as weightlessness, extreme temperature, and vacuum. In practical applications at home and abroad, there have been "stuck" phenomena. Extreme conditions such as gravity, extreme temperature and vacuum cause ball bearings with repeated starts and low speeds to fail to start and run poorly. The stuck ball bearing shaft ring cannot rotate relative to the seat ring, and even the failure behavior that the starting friction torque is too large leads to deformation and fracture of the cage. In the current ground simulation test, only extreme temperature and vacuum are tested, and the bearing does not appear "stuck" phenomenon during start-up operation. It can be inferred that the cause of this...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01L5/00G01M13/04
CPCG01L5/0009G01M13/04
Inventor 陈恩平张鹏飞张尚斌
Owner YANSHAN UNIV
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