High-cycle fatigue test method for blisk

An integral blisk and high-cycle fatigue technology, which is applied in the testing of machine/structural components, vibration testing, and testing of material strength by applying repetitive force/pulsation force, etc., can solve the difference between the boundary conditions of the blade test and the boundary conditions of the use environment Far, blisk damage, test data impact and other problems, to achieve the effect of shortening the test period, reducing the test cost, and reducing the error of the test data

Active Publication Date: 2019-08-20
陕西陕航环境试验有限公司
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Problems solved by technology

The blade fatigue test of the overall blisk has so far been cutting the blade from the blisk, and then doing the fatigue life/limit of each blade. There are several problems in this test: one is that the blisk is completely d

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  • High-cycle fatigue test method for blisk
  • High-cycle fatigue test method for blisk
  • High-cycle fatigue test method for blisk

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Embodiment Construction

[0045] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0046] Such as figure 1 Shown, a kind of high cycle fatigue test method of blisk among the present invention, comprises the following steps:

[0047] Step S01, fixture design and manufacture.

[0048] Step S02, performing modal calculation, modal test, and frequency response test on the fixture.

[0049] The fixture is installed on the vibrating table, and the excitation force of 0.5g is used to scan the frequency from low frequency to high frequency. The first few resonance frequencies of the fixture appear in the frequency sweep results, such as figure 2 As shown, they are 1700Hz, 2000Hz, 2346Hz...

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Abstract

The invention discloses a high-cycle fatigue test method for a blisk. The method comprises the following steps that: a clamp is designed and manufactured; modal calculation, modal testing and frequency response testing are performed on the clamp, and the first-order inherent frequency, damping ratio and vibration mode of the blisk are tested under free and holding states; a blade maximum stress area is calculated through a finite element method; a blade maximum stress point is determined through a strain gage bonding method; the relation curve of blade tip maximum displacement and stress is calibrated; blade frequency weight balancing design is carried out; test accompanying blades are monitored simultaneously by a monitoring system; and a fatigue test is started from a blade with the smallest frequency. Compared with a traditional blade cutting fatigue test method, the test method of the invention has the advantages that: the testing boundary condition of the blades of the blisk is closer to an actual using condition; the blisk is not damaged; test data errors caused by blade cutting surfaces are reduced; a test period is shortened; and test costs are reduced.

Description

technical field [0001] The invention relates to the technical field of mechanical vibration testing, in particular to a high-cycle fatigue testing method for an integral blisk. Background technique [0002] The overall blisk is a combination of blades and blisks through advanced technology. Compared with conventional blisks, the connecting tenons and tenon grooves are omitted, which greatly simplifies the structure, reduces the weight, and reduces the failure rate. The engine's thrust-to-weight ratio It has been improved, but the vibration and fatigue damage of the overall blisk are extremely prominent. The blade fatigue test of the overall blisk has so far been cutting the blade from the blisk, and then doing the fatigue life / limit of each blade. There are several problems in this test: one is that the blisk is completely destroyed after the test; The second is that the boundary conditions of the blade test are far from the boundary conditions of the use environment; the t...

Claims

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Application Information

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IPC IPC(8): G01M7/02G01N3/04G01N3/32
CPCG01M7/025G01N3/04G01N3/32G01N2203/0073
Inventor 郭紫龙高星伟雷青娟钱军良王同乐曹谋
Owner 陕西陕航环境试验有限公司
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