Ways and options for aircraft structural health management.

被引:110
作者
Boller, C [1 ]
机构
[1] EADS Mil Aircraft Business Unit, D-81663 Munich, Germany
关键词
Flight control systems;
D O I
10.1088/0964-1726/10/3/302
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
The number of aircraft is increasing worldwide as well as their age. This has Led to an increasing market of aging aircraft. The older an aircraft structure becomes, the more difficult it may be to predict under which conditions it will be flown and this especially when it is influenced by continuous upgrades in avionics, flight control systems or even engines, thus resulting in a possible change of flight envelopes. It is under these conditions that the aircraft structure needs increased care regarding monitoring and subsequent life management. This paper addresses the different means of how this can be done, starting with conventional inspection and gradually moving over to state-of-the-art loads and finally damage monitoring, where the latter is very much driven by ongoing smart materials and structures initiatives. Benefits either obtained or still to be expected from the different ways of monitoring are described.
引用
收藏
页码:432 / 440
页数:9
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