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Testing device and method for performing fatigue test on spacer part

A fatigue test and spacer technology, applied in measuring devices, using repetitive force/pulse force to test the strength of materials, instruments, etc., can solve problems such as high cost and long test cycle

Active Publication Date: 2016-12-07
AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there is no fatigue test method for spacer parts alone. In order to assess whether the fatigue performance of spacer parts meets the requirements for use, the assembled elastic bearing is often used to carry out the overall component fatigue test. Although the overall component fatigue test method is relatively accurate and Reliable, but the test cycle is long and the cost is high

Method used

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  • Testing device and method for performing fatigue test on spacer part
  • Testing device and method for performing fatigue test on spacer part
  • Testing device and method for performing fatigue test on spacer part

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Embodiment Construction

[0021] The technical scheme of the present invention will be further described below in conjunction with accompanying drawing and embodiment:

[0022] See attached figure 1 As shown, the steps of the method are as follows:

[0023] (1) The material of the spacer parts is 0Cr18Ni9 stainless steel;

[0024] (2) Create a geometric model of the vibration structure of the spacer part in ANSYS software, and define the material properties of the 0Cr18Ni9 stainless steel spacer, including a density of 7.93g / cm 3 , Young's modulus 193000MPa, Poisson's ratio 0.26;

[0025] (3) ANSYS software has the function of dynamic analysis, which analyzes the motion characteristics of the structure in space, and determines the resulting stress, strain and deformation in the structure. In ANSYS software, the boundary conditions of the spacer part are set. In this embodiment, the maximum displacement of the vibration deformation of the 0Cr18Ni9 stainless steel spacer is set to 0.5mm;

[0026] (4)...

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Abstract

The invention discloses a testing device for performing a fatigue test on a spacer part. The testing device comprises a lower fixing base and a pressing piece which are used for fixing the spacer part, and a vibration pressing head for applying pressure to the flange fillet part of the spacer part, wherein the lower fixing base is mounted on a fatigue tester base body in a threaded connection manner, the spacer part is placed between the lower fixing base and the pressing piece, the fixing base, the spacer part and the pressing piece are connected through a locking bolt, the vibration pressing head is mounted on the vibration beam of the fatigue tester in a threaded connection manner, and the vibration pressing head contacts with the spacer part in a matched manner. A method using the testing device to perform the fatigue test on the spacer part includes: determining the material of the spacer part, using ANSYS software to analyze the load, deformation displacement and stress of the spacer part in a vibration structure, comparing the measured yield strength and tensile strength of the spacer part with a simulation analysis result to determine the load force of an actual vibration fatigue test, and carrying out the vibration fatigue test of the spacer part. The testing device is short in testing cycle, low in testing cost and accurate and scientific in testing result and can be used for evaluating the fatigue service life of the spacer part and guiding spacer part design.

Description

technical field [0001] The invention belongs to the technical field of component performance detection, and relates to a spacer component fatigue test test device and a test method. Background technique [0002] Helicopter spherical thrust elastic bearings (elastic bearings) are the core components of star-shaped flexible hubs and spherical flexible hubs, which can realize the waving, swinging and pitch-changing motion of the blades while bearing the huge centrifugal force generated by the rotation of the blades. The elastic bearing is composed of a large joint, a small joint and a plurality of spacer parts and rubber laminations. The spacer part and the rubber are bonded to form an elastic body, and the large joints, small joints and elastic body laminations are bonded to form a whole. The elastomeric laminate composed of spacer parts and rubber is a key part of the elastic bearing. In the work of the elastic bearing, it bears axial compression force, radial side pressure...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/32
CPCG01N3/32G01N2203/0005G01N2203/0073G01N2203/0282
Inventor 陈由红兰博王淑云李凯
Owner AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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