Fatigue in aerostructures - where structural health monitoring can contribute to a complex subject

被引：49

作者：

Boller, Christian

Buderath, Matthias

机构：

[1] Univ Sheffield, Dept Mech Engn, Sheffield S1 3JD, S Yorkshire, England

[2] EADS Mil Air Syst, D-81663 Munich, Germany

来源：

PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES | 2007年 / 365卷 / 1851期

关键词：

fatigue; aircraft; structures; monitoring; sensors;

D O I：

10.1098/rsta.2006.1924

中图分类号：

O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];

学科分类号：

07 ; 0710 ; 09 ;

摘要：

An overview of the aircraft design and maintenance process is given with specific emphasis on the fatigue design as well as the phenomenon of the ageing aircraft observed over the life cycle. The different measures taken to guarantee structural integrity along the maintenance process are addressed. The impact of structural health monitoring as a means of possibly revolutionizing the current aircraft structural monitoring and design process is emphasized and comparison is made to jet engines and helicopters, where health monitoring has already found the respective breakthrough.

引用

页码：561 / 587

页数：27

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