Supersonic particle deposition as a means for enhancing the structural integrity of aircraft structures

被引：25
作者：
Jones, R. [1 ]
Molent, L. [2 ]
Barter, S. [2 ]
Matthews, N. [3 ]
Tamboli, D. [1 ]
机构：
[1] Monash Univ, Dept Mech & Aeronaut Engn, Ctr Expertise Struct Mech, Clayton, Vic 3800, Australia
[2] Def Sci & Technol Org, Aerosp Div, Fisherrnans Bend, Vic 3207, Australia
[3] Rosebank Engn Australia, Bayswater, Vic 315, Australia
来源：
INTERNATIONAL JOURNAL OF FATIGUE | 2014年 / 68卷
关键词：
Supersonic particle deposition; Corrosion; LOV; Military transport aircraft; Combat aircraft; CRACK-GROWTH;
D O I：
10.1016/j.ijfatigue.2014.03.013
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The paper presents the results of experimental studies into the application of supersonic particle deposition (SPD) for repairing and enhancing the airworthiness and integrity of aging aircraft structures. Presented are the results of coupon tests on the application of SPD doublers to mechanically fastened joints and to simulated corrosion damage tested under constant amplitude fatigue loads. These successful tests are then supported by an application to an F/A-18 Hornet wing attachment centre barrel laboratory test article. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码：260 / 268
页数：9
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