STUDY ON FLAW DEPTH STATISTICS AND CORRESPONDING FATIGUE LIFE OF HELICOPTER ALUMINIUM ALLOY STRUCTURE
Surface defect is the main fatigue failure source of helicopter metal dynamic components. Depth data of impact pit defects on surface of aluminum alloy critical dynamic parts of helicopter were collected,and statistical analysis was conducted. Statistic results show that the depth of impact pits obe...
Saved in:
Main Authors: | NI Yang, ZHOU ChuWei, YU JianJian, ZOU Jing |
---|---|
Format: | Article |
Language: | zho |
Published: |
Editorial Office of Journal of Mechanical Strength
2020-01-01
|
Series: | Jixie qiangdu |
Subjects: | |
Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2020.04.029 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
STUDY ON LIFE PREDICTION AND FATIGUE TEST OF ZM6 MATERIAL WITH IMPACT PIT
by: LI Jian, et al.
Published: (2021-01-01) -
Statistical flaws of the fitness-fatigue sports performance prediction model
by: Alexandre Marchal, et al.
Published: (2025-01-01) -
SRESS AND FATIGUE LIFE OF PITTING DEFECTS ON PUMPING UNIT GEAR
by: BAI YunSong, et al.
Published: (2022-01-01) -
Multiaxial fatigue of in-service aluminium longerons for helicopter rotor-blades
by: A. Shanyavskiy, et al.
Published: (2016-06-01) -
Multiaxial fatigue of in-service aluminium longerons for helicopter rotor-blades
by: A. Shanyavskiy, et al.
Published: (2018-07-01)