APPLICATION ON PREDICTING FATIGUE LIFE IN AIRCRAFT STRUCTURE BASED ON PHM TECHNOLOGY
Fatigue failure of the airframe structure occurs almost in the hole position of the fastener hole,Structural fatigue fracture will lead to a catastrophic accident. PHM( Prediction and Health Management) technology can be used to predict when fatigue failure may occur,thereby achieving self-service s...
Saved in:
Main Authors: | SONG Bo, ZHU QingYu, ZENG ZhaoYang |
---|---|
Format: | Article |
Language: | zho |
Published: |
Editorial Office of Journal of Mechanical Strength
2017-01-01
|
Series: | Jixie qiangdu |
Subjects: | |
Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.02.032 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
FATIGUE LIFE ANALYSIS OF SIMULATED AIRCRAFT BEAM STRUCTURE CONNECTION
by: ZHENG Jie, et al.
Published: (2020-01-01) -
ANALYSIS ON FATIGUE CRACK INITIATION LIFE OF COUPLER KNUCKLE OF RAILWAY HEAVY-HAUL WAGON
by: TIAN XiaoChen, et al.
Published: (2022-01-01) -
Simple criterion for predicting fatigue life under combined bending and torsion loading
by: K. Slámecka, et al.
Published: (2017-06-01) -
MODIFICATION METHOD OF STRAIN-LIFE CURVES UNDER DIFFERENT SURFACE CONDITIONS OF COMPONENTS (MT)
by: DUAN Heng, et al.
Published: (2022-01-01) -
ANALYSIS AND EXPERIMENTAL VERIFICATION OF THE EFFECТ OF ASSEMBLY STRESS ON THE RANDOM FATIGUE LIFE OF AIRCRAFT PIPELINE
by: ZHAO XuSheng, et al.
Published: (2024-02-01)