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Aviation spline vibration lubrication wear tester

A spline and experimental technology, applied in the direction of testing wear resistance, etc., can solve the problems of vibration wear, difficult monitoring and maintenance, inaccessibility of spline, etc., and achieve the effect of exquisite structure and accurate measurement

Active Publication Date: 2015-10-28
DALIAN UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the misalignment of the spline, the vibration and wear of the residual dynamic balance under the cantilever moment, the grease lubrication problem at high temperature, etc., together lead to the spline not reaching the expected service life
[0004] The vibration and wear of the spline is a slow-changing process, and the position of the spline is typically inaccessible. It is difficult to maintain and maintain it, and it is also difficult to monitor and repair it in actual operation, and it is even difficult to accurately understand its wear. Therefore, it is necessary to Realize the simulation and prediction of spline lubrication and wear through a suitable spline lubrication and wear tester

Method used

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  • Aviation spline vibration lubrication wear tester

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Embodiment Construction

[0016] The accompanying drawing is a structural schematic diagram of the aviation spline vibration lubrication and wear tester of the present invention. As shown in the figure, the aviation spline vibration lubrication and wear tester of the present invention consists of a static torque loading device 1, a double row angular contact bearing 2, a rigid coupling 3, a torque measuring instrument 4, a frequency converter 5, and an angular contact bearing 6 , motor 7, synchronous belt 8, synchronous wheel 9, driven wheel 10, speed sensor 11, outer ring support bearing 12, inner ring support bearing 13, preamplifier 14, signal acquisition instrument 15, industrial computer 16, vibration displacement sensor 17 , end cover 18, external spline 19, internal spline 20, temperature sensor 21, temperature insulation cover 22, vortex 23, torque loading shaft 24, foundation platform 25, rotor 26, main support 27, torque transmission rod 28 , Rigid connector 29, positioning pin 30, fastening ...

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Abstract

The invention discloses an aviation spline vibration lubrication abrasion tester, and belongs to the field of aerospace drive and lubrication. The aviation spline vibration lubrication abrasion tester consists of a static torque loader, a dual-row angular contact bearing, a rigid coupling, a torque measurement instrument, a frequency converter, an angular contact bearing, an electromotor, a synchronous belt, a synchronous wheel, a driven wheel, a revolution speed transducer, an outer ring back-up bearing, an inner ring back-up bearing, a pre-amplifier, a signal acquisition device, an industrial control machine, a vibration displacement sensor, an end cover, an outer spline, an inner spline, a temperature sensor, a temperature insulation cover, a vortex motion device, a torque loading shaft, a foundation platform, rotors, a main support, a torque transmission rod, a rigid connecting element, a positioning pin, a fastening screw, a movable support, a fastening bolt, a regulating screw, a temperature regulator and a fixed support. The aviation spline vibration lubrication abrasion tester has the advantages that the spline meshed relative vibration displacement, frequency and amplitude can be metered accurately; the spline transmission torque and working temperature can be measured and regulated; the structure is smart and the operation is reliable and stable.

Description

technical field [0001] The invention belongs to the field of aerospace transmission and lubrication, and relates to an aviation spline vibration lubrication wear tester. technical background [0002] The spline coupling has simple structure, high reliability, high transmission power per unit weight, simple lubrication and maintenance, and is an inevitable choice for aerospace transmission connections. [0003] However, the misalignment of the spline, the vibration and wear of the residual dynamic balance under the cantilever moment, the grease lubrication problem at high temperature, etc., together lead to the spline not reaching the expected service life. [0004] The vibration and wear of the spline is a slow-changing process, and the position of the spline is typically inaccessible. It is difficult to maintain and maintain it, and it is also difficult to monitor and repair it in actual operation, and it is even difficult to accurately understand its wear. Therefore, it is...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N3/56
Inventor 赵广苏钧聪韩清凯史妍妍李国权韦振祖
Owner DALIAN UNIV OF TECH