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A preloaded high-frequency vibration fatigue test device

A high-frequency vibration and fatigue test technology, which is applied in the direction of measuring devices, testing material strength by applying repetitive force/pulsation force, instruments, etc., can solve problems such as applied average stress

Active Publication Date: 2020-07-14
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of this invention is to provide a kind of preload high-frequency vibration fatigue test device, to solve the problem of applying average stress in the high-frequency fatigue test system based on the shaking table

Method used

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  • A preloaded high-frequency vibration fatigue test device
  • A preloaded high-frequency vibration fatigue test device
  • A preloaded high-frequency vibration fatigue test device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0034] This embodiment is a four-point bending fatigue test fixture.

[0035] Such as Figure 1-6 As shown, a preload high-frequency vibration fatigue test device of the present invention includes a sample 6 and a clamp, and the sample 6 is strip-shaped, which includes a test section A in the middle, and a holding section B at both ends of the test section A. The ends of the two clamping sections B are each connected with a stud 9; the fixture includes a fixture base 2 and two clamping blocks 3, the fixture base 2 is installed on the connecting plate 1 of the electric vibrating table, and is passed through a plurality of second bolts 7 is fixed on the connection plate 1; two ends of the fixture base 2 are respectively provided with a slot 8, and the opening width of the slot 8 is smaller than the width of the clamping section B of the sample 6; the studs 9 at both ends of the sample 6 are respectively snapped into In the two draw-in grooves 8, nuts 4 are installed at the ends...

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PUM

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Abstract

The invention discloses a preloaded high-frequency vibration fatigue testing device, which comprises a sample and a clamp, wherein the sample is strip-shaped, and comprises a test section located in the middle and holding sections at two ends of the test section; two studs are connected to ends of the holding sections respectively; the clamp comprises a clamp base and two clamping blocks; the clamp base is mounted on a connecting plate of an electric vibration table, and is fixedly connected to the connecting plate through a plurality of second bolts; two clamping grooves are formed in two ends of the clamp base respectively; the opening width of the clamping grooves is smaller than the width of the holding sections of the sample; the studs at the two ends of the sample are respectively inserted into the two clamping grooves in a clamped manner; nuts are mounted at ends of the studs; the outer diameter of the nuts is larger than the opening width of the clamping grooves; the two clamping blocks are respectively pressed on the two clamping grooves, and are fixed with the clamp base through a plurality of first bolts. According to the invention, the problem in applying an average stress in a vibration table-based high-frequency fatigue test system is effectively solved.

Description

technical field [0001] The invention relates to a preload high-frequency vibration fatigue test device, belonging to the field of material and structure fatigue tests. Background technique [0002] With the continuous improvement of modern industry's requirements for the safety, reliability and economy of gas turbine engines, the source, mechanism, prevention and maintenance of faults have long been the subject of continuous and in-depth research by scientific researchers. High cycle fatigue failure is a prominent issue in the structural integrity of modern gas turbine engines. During the working process of the gas turbine engine, the high-speed rotating fan, compressor and turbine blades not only bear the huge centrifugal force load, but also bear the high-frequency vibration load caused by the forced vibration of the airflow. Airflow excitation leads to vibratory load frequencies on the blades even exceeding 1000 Hz with cycles up to 10 7 The cycle is even higher, so tha...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N3/38
CPCG01N3/38G01N2203/0005G01N2203/0282
Inventor 宋迎东贾旭胡绪腾吴娜
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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