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Testing device and testing method for fretting fatigue of end-tooth structure

A technology of fretting fatigue and test equipment, which is applied in the testing of machine gears/transmission mechanisms, testing the strength of materials by applying repetitive force/pulsation force, and testing the strength of materials by applying stable tension/pressure, which can solve the problems of fatigue life decline, Loading normal force changes, threaded connection loosening and other problems, to achieve the effect of reducing test cost, saving cost, and large driving force

Active Publication Date: 2015-01-21
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The end-tooth structure is widely used in aeromechanical turbine engine transmission spindles and transmission devices of various high-speed, large-scale and heavy-duty mechanical equipment. It has the advantages of fewer transmission teeth, compact structure, and high load-bearing capacity. In the middle, the fretting fatigue between the mating contact surfaces of the concave and convex teeth will lead to a significant decrease in the fatigue life
However, it is difficult to conduct fretting fatigue test research on three-dimensional structural parts of end teeth, mainly because of two technical problems: (1) the end tooth structure needs to be processed by a special gear grinding machine, and the processing cost of three-dimensional structural parts is too high; (2) For the fatigue test of three-dimensional structural parts, it is necessary to consider the actual stress of the end tooth structure, mainly including axial preload, torque and centrifugal force. If it is necessary to completely simulate the stress of its real three-dimensional structure, a rotation test is required In the non-rotating test, when considering the preload and torque alone, it is also necessary to use a multi-axis fatigue testing machine to achieve
[0004] The existing loading device for fretting fatigue test with uniaxial fatigue testing machine mostly adopts the loading ring structure and loads through bolts, but the driving force of the thread loading scheme is small, and various factors such as vibration during the fatigue process are likely to cause the thread The connection is loose, causing a change in the loading normal force

Method used

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  • Testing device and testing method for fretting fatigue of end-tooth structure
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  • Testing device and testing method for fretting fatigue of end-tooth structure

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Embodiment Construction

[0040] Please refer to Figure 1 to Figure 7 As shown, the end tooth structure fretting fatigue test device of the present invention includes a concave tooth fixing assembly 1 , a convex tooth clamping assembly 2 and a normal force loading assembly 3 .

[0041] The concave tooth fixing assembly 1 includes an upper clamp body 12 and a concave tooth test piece 11 installed on the upper clamp body 12, an M10 compression bolt 13 and a concave tooth pressure plate 14, wherein the upper clamp body 12 includes a hollow lower part 120 and a lower part. The upper part 121 above 120, wherein the upper end of the upper part 121 can be clamped on the upper chuck 43 of a common uniaxial fatigue testing machine, and is integrated with the upper crossbeam 41 of the testing machine, and can be raised and lowered in the vertical direction thereupon. The lower part 120 is formed with a rectangular hole 122 penetrating through the front, rear and lower surfaces of the lower part 120 . A rectang...

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Abstract

The invention discloses a testing device and a testing method for the fretting fatigue of an end-tooth structure. The testing device comprises a concave tooth fixing assembly, a convex tooth clamping assembly and a normal force loading assembly, wherein the concave tooth fixing assembly is used for realizing the fixation of a concave tooth test piece; the convex tooth clamping assembly is used for realizing the loading of a convex tooth test piece; the normal force loading assembly is used for realizing the application of a load in a horizontal direction; a fretting fatigue testing level loading device adopts a symmetrical structure layout and the load is realized by a hydraulic loading system; the hydraulic loading system adopts a closed force system framework structure and has no output of external force, and the load of a fatigue tester in the vertical direction is not influenced; and a concave tooth test piece bears a pre-tightening force load in the horizontal direction and is tightly pressed by a concave tooth pressing plate in the vertical direction, so that the loading direction in the horizontal direction of a loading process keeps unchanged. According to the testing device, a common single-shaft fatigue tester is matched by similarly simulating the stress condition of end teeth under an actual working environment, so that a fretting fatigue test of an end-tooth structure simulating piece can be carried out and the experiment cost is reduced.

Description

Technical field: [0001] The invention relates to an end tooth structure fretting fatigue test device and a test method, which belong to the technical field of life evaluation tests of materials and structural parts. Background technique: [0002] The end-tooth structure is widely used in aeromechanical turbine engine transmission spindles and transmission devices of various high-speed, large-scale and heavy-duty mechanical equipment. It has the advantages of fewer transmission teeth, compact structure, and high load-bearing capacity. Among them, the fretting fatigue between the mating contact surfaces of the concave and convex teeth will lead to a significant decrease in fatigue life. However, it is difficult to conduct fretting fatigue test research on three-dimensional structural parts of end teeth, mainly because of two technical problems: (1) the end tooth structure needs to be processed by a special gear grinding machine, and the processing cost of three-dimensional str...

Claims

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Application Information

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IPC IPC(8): G01N3/36G01N3/10G01M13/02
Inventor 李爱民崔海涛李奇璇
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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