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Oil film static eccentric loading device and method of extrusion oil film damper-rotor test system

A technology of extrusion oil film damping and test system, which is applied in the direction of measuring device, machine/structural component test, instrument, etc., can solve the problems of low efficiency, low test repeatability, low eccentricity loading accuracy, etc., and achieve easy installation and use , Good repeatability, avoiding the effect of repeated assembly and disassembly

Active Publication Date: 2021-01-15
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] At present, the main means of loading different oil film eccentricities on the tester is to pre-process oil film casings with different eccentricities. A large number of parts need to be processed to achieve different eccentricities. At the same time, the oil film casing needs to be replaced every time a group of tests are completed. The test process It also needs to be assembled and disassembled many times, and the efficiency is low
In addition, limited by the processing accuracy and the uncertainty of each assembly, the eccentricity loading accuracy is low, and the test repeatability is low

Method used

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  • Oil film static eccentric loading device and method of extrusion oil film damper-rotor test system
  • Oil film static eccentric loading device and method of extrusion oil film damper-rotor test system
  • Oil film static eccentric loading device and method of extrusion oil film damper-rotor test system

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Embodiment Construction

[0036] The preferred implementation of the device and method of the present invention will be further fully and detailedly described below in conjunction with the accompanying drawings.

[0037] Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0038] Please combine figure 1 As shown, the present invention provides a static eccentric oil film loading device for a squeeze oil film damper-rotor test system. The loading device includes a test bench 1, a squeeze oil film damper-rotor tester 2, a rope holder 3, a fixed pulley 4, a loading tray 5, and a rope 6. The squeeze oil film damper-rotor tester 2 is installed on the test bench 1 placed horizontally through the support 21 and the support 22, and each su...

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Abstract

The invention relates to an oil film static eccentric loading device of an extrusion oil film damper-rotor test system. The oil film static eccentric loading device comprises an extrusion oil film damper-rotor tester, a rope retainer, a fixed pulley, a loading tray and a rope. The rope retainer is mounted on a rotating shaft; the rope retainer comprises two annular clamping blocks which surround and are fixed on the rotating shaft, a second bearing which is fixed between the two clamping blocks, and a rope fixing ring which is arranged around the second bearing; one end of the rope is hung onthe fixing ring and penetrates through the fixed pulley, the other end of the rope extends downwards and is provided with the loading tray in a hanging mode, weights are placed in the loading tray, the designated squeeze oil film damper can generate different static eccentricity ratios by loading the weights of different masses, and compared with a traditional loading means, a plurality of groupsof damper shells do not need to be processed, so that the total number of parts is reduced, and the test cost is reduced. The invention further discloses a loading method using the loading device.

Description

technical field [0001] The invention relates to the field of aero-engines, in particular to the field of experimental research on the dynamic characteristics of the aero-engine rotor-support system. Background technique [0002] As the "heart" of the aircraft, the safety and reliability of the aero-engine has been widely concerned. As the core component of an aero-engine, the rotor-support system’s vibration characteristics play a key role in the overall performance of the aero-engine, and statistical data also show that more than 90% of aero-engine structural strength failures are caused by or related to vibration. The supporting structure of aero-engines mostly adopts a combination scheme of rolling bearing + elastic support + squeeze film damper. [0003] Squeeze oil film damper has been widely used because of its simple structure, small space occupation and good vibration reduction effect. Static eccentricity occurs. The existence of static eccentricity will affect th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/00G01M15/02G01M15/14
CPCG01M13/00G01M15/02G01M15/14
Inventor 韩佳奇王飞陈伟罗贵火刘璐璐赵振华
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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