ENVIRONMENTAL EVALUATION OF REPAIRS TO FUSELAGE LAP JOINTS

被引：12

作者：

MOLENT, L

BRIDGFORD, N

REES, D

JONES, R

机构：

[1] Aircraft Structures Division, Aeronautical Research Laboratory, Fishermens Bend, Vic. 3207

来源：

COMPOSITE STRUCTURES | 1992年 / 21卷 / 02期

关键词：

D O I：

10.1016/0263-8223(92)90047-G

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

This paper presents the results of a fatigue test programme undertaken to investigate repairs to multi-site damage in aircraft fuselage lap joints. It is demonstrated that a boron/epoxy composite doubler bonded over the joint should significantly increase the fatigue life of the structure and that environmental effects are negligible.

引用

页码：121 / 130

页数：10

共 6 条

[1]

Baker AA., 1988, BONDED REPAIR AIRCRA, DOI 10.1007/978-94-009-2752-0

[2] ANATOMICAL STUDIES OF THE SPINOCERVICAL TRACT OF THE RAT [J].