Fatigue crack retardation in aluminium alloys by means of squeeze dimpling

被引：0

作者：

Sarchamy, D ^{[1
]}

Moss, S ^{[1
]}

Burns, MG ^{[1
]}

Lawford, K ^{[1
]}

Hunt, E ^{[1
]}

机构：

[1] BAc Airbus, Test & Dev Engn, Filton, England

来源：

ICAF 97: FATIGUE IN NEW AND AGEING AIRCRAFT, VOLS I AND II: VOL I: LECTURE PAPERS, VOL II: POSTER PAPERS | 1997年

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper demonstrates the effectiveness of squeeze dimpling as a fatigue crack retardation technique in 2024-T351 Al alloy under a constant amplitude loading regime. A comparison with results obtained employing the traditional Stop Drilled Hole retardation method (i.e, interference fit plugs - with and without cold expansion) is provided. An improvement in life - to - failure by a factor of at least 10 over that achieved by plain Stop Drilled Holes was observed.

引用

页码：707 / 718

页数：12