Monitoring of aircraft landing gear structure
2008 ◽
Vol 112
(1131)
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pp. 275-278
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Keyword(s):
The Past
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Abstract Landing gear structure is developed predominantly using safe life design criteria. Health monitoring and structural prognosis techniques for landing gear cannot focus on crack detection; techniques for determining input loads and calculating damage or methods for directly measuring material damage must be employed. This paper will discuss Messier-Dowty’s research into structural monitoring over the past several years. Principally, direct damage detection systems and load monitoring systems will be discussed.
Keyword(s):
2012 ◽
Vol 226
(4)
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pp. 315-327
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Keyword(s):
2009 ◽
Vol 2009
(0)
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pp. 321-322
Keyword(s):
1986 ◽
Vol 58
(7)
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pp. 14-24
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