Small device for load bending fatigue testing and method

A bending fatigue and testing device technology, applied in the field of fatigue testing, can solve the problems of poor test accuracy, low bending frequency, long test time, etc., and achieve the effect of reasonable structure design, convenient operation and complete functions

Active Publication Date: 2019-02-19
CIVIL AVIATION UNIV OF CHINA
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AI Technical Summary

Problems solved by technology

Existing bending fatigue testing machines mostly use eccentric wheel or weight loading as the driving device. The defect of this device is that it can only perform strain control fatigue test, that is, low-cycle bending fatigue test, and the test accuracy of this loading method is poor, so it cannot pass The decrease of the bending resistance of the sample determines when fatigue cracks occur in the parts; the three-point bending/four-point bending fatigue test method cannot realize the bending fati

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  • Small device for load bending fatigue testing and method
  • Small device for load bending fatigue testing and method
  • Small device for load bending fatigue testing and method

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Embodiment Construction

[0020] The small load bending fatigue testing device and method provided by the present invention will be described in detail below in conjunction with the accompanying drawings and specific implementation.

[0021] like figure 1 As shown, the present invention adopts the cantilever beam method to carry out the bending fatigue test. The driving device is a linear motor module, and the motion directly acts on the cantilever end of the fatigue sample, so that the cantilever end of the fatigue sample can move up and down. The bearing in the fixture assembly overcomes the tensile / compressive stress generated by the fatigue specimen during the test, and overcomes the torsional stress generated by the cantilever end of the fatigue specimen through the bearing integrated in the specimen cantilever end fixture assembly, so that the fatigue specimen is tested Only bear cyclic bending stress or strain during the process; by setting the zero position and displacement stroke of the linear...

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Abstract

The invention discloses a small device for load bending fatigue testing and a method. The device comprises a base, a gantry, a linear motor module, a linear motor module bracket, a load sensor, a thrust rod guide wheel assembly, a thrust rod, a specimen fixed end clamp right support table, a specimen cantilever end clamp assembly, a displacement sensor test connective rod, a displacement sensor, adisplacement sensor bracket, a fatigue specimen, a specimen fixed end clamp assembly, an environmental chamber, a specimen fixed end clamp left support table, and control system. The small device forload bending fatigue testing and the method provided by the invention can realize fatigue testing of stress control, strain control, and stress/strain hybrid control, and achieve a bending fatigue performance testing with a stress ratio greater than zero, equal to zero, or less than zero. The advantages of the device are reasonable in structure design, complete in function, and convenient in operation.

Description

technical field [0001] The invention belongs to the technical field of fatigue testing, and in particular relates to a small-load bending fatigue testing device and method. Background technique [0002] Bending fatigue failure of mechanical parts due to cyclic bending stress or strain is one of the common failure modes. Using a bending fatigue testing machine to perform bending fatigue tests on parts, and to establish a relationship curve (S-N curve) between the maximum stress or strain and its failure cycle is an important method for evaluating the bending fatigue life of parts and ensuring the safety of equipment personnel. [0003] According to the number of failure cycles and the bending stress level of the component, bending fatigue can be divided into low cycle bending fatigue and high cycle bending fatigue. The fatigue of many parts under the action of variable amplitude cyclic bending stress is neither pure high cycle fatigue nor high cycle fatigue. Pure low cycle f...

Claims

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Application Information

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IPC IPC(8): G01N3/38
CPCG01N3/38G01N2203/0005G01N2203/0023G01N2203/005G01N2203/0073G01N2203/0278
Inventor 贾鹏费骏谢海超王志平
Owner CIVIL AVIATION UNIV OF CHINA
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