CRACK FAILURE ANALYSIS OF LOW PRESSURE TURBINE SHAFT OIL PASSAGE HOLE OF AERO-ENGINE

In order to investigate the nature and causes of the cracked passage hole of the low-pressure turbine shaft of aero-engine during the high and low circumference compound fatigue test, the low-pressure turbine shaft crack location was examined in appearance, fracture analysis, surface inspection, met...

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Bibliographic Details
Main Authors: WANG Xuemin, LU Xuping, SHEN Lian, GU Yuanxing, WU Chen, GUO Jianying, XU Jingpei
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2025-02-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2025.02.005
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