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Low-temperature high-speed bearing test device for liquid rocket engine

A test device, high-speed bearing technology, applied in the direction of mechanical bearing testing, etc., can solve the problems of increased labor costs and test costs, inability to meet the requirements of various types of low-temperature bearing tests, inconvenient disassembly, etc., to achieve simple structure and improved Utilization, ease of disassembly and maintenance effects

Pending Publication Date: 2022-03-01
LANDSPACE TECH HUZHOU CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, there is already a test device for low temperature bearings in this technical field, but this test device can only test fixed types of bearings, and cannot meet the requirements for testing various types of low temperature bearings
And because of the design of the device structure, it is inconvenient to disassemble, which greatly increases the labor cost and test cost

Method used

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  • Low-temperature high-speed bearing test device for liquid rocket engine
  • Low-temperature high-speed bearing test device for liquid rocket engine
  • Low-temperature high-speed bearing test device for liquid rocket engine

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Embodiment Construction

[0032] Various exemplary embodiments of the present invention will now be described in detail. The detailed description should not be considered as a limitation of the present invention, but rather as a more detailed description of certain aspects, features and embodiments of the present invention.

[0033] It will be apparent to those skilled in the art that various modifications and changes can be made in the specific embodiments of the present invention described herein without departing from the scope or spirit of the present invention. Other embodiments will be apparent to the skilled person from the description of the present invention. The specification and examples in this application are exemplary only.

[0034] Such as figure 2 Shown is the low-temperature high-speed bearing test device for the liquid rocket engine provided by the present invention. In the specific embodiment of the test device, the test device includes: a main casing 1, a bearing shaft assembly 2,...

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Abstract

The invention provides a low-temperature high-speed bearing test device for a liquid rocket engine, and the device comprises a main housing which is internally provided with a bearing shafting assembly, and the bearing shafting assembly is provided with a to-be-detected test bearing. And an axial load loading assembly is arranged outside the main shell, is parallel to or coaxial with the axis of the bearing shafting assembly, and is used for applying an axial load to the tested bearing. A radial load loading assembly is further arranged outside the main shell, is perpendicular to the axis of the bearing shafting assembly and is used for applying a radial load to the tested bearing. A medium inlet assembly communicated with the interior of the main shell is arranged on the main shell and used for providing a cooling medium for the interior of the main shell. A front middle sleeve and a rear middle sleeve are arranged between the main shell and the bearing shafting assembly and used for fixing the bearing shafting assembly. The test device is good in compatibility, high in utilization rate and convenient to disassemble and assemble, the test efficiency is greatly improved, and the test cost and the labor cost are reduced.

Description

technical field [0001] The invention relates to the technical field of bearing testing devices, in particular to a low-temperature and high-speed bearing testing device, in particular to a low-temperature and high-speed bearing testing device for a liquid rocket engine. Background technique [0002] The high-speed turbo pump is an important component of the liquid rocket engine, and the low-temperature bearing is the key part of the turbo pump. The reliability of the low-temperature bearing is the basis for the stable, safe and reliable use of the engine. According to the operating conditions of the liquid rocket engine turbopump, it is necessary to carry out assessment tests on whether the performance and effect of the low temperature bearing under simulated rated and over-speed conditions meet the design requirements. The life of low temperature bearings is related to factors such as speed, cooling flow of low temperature medium, axial and radial loads and temperature. Th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/04
CPCG01M13/04
Inventor 杨军张小平郑国真姜圣杰张宏伟张士强任荣波
Owner LANDSPACE TECH HUZHOU CO LTD