Closing system for an aircraft fan shroud
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United States of America Patent
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Jun 18, 2013
Grant Date -
Aug 5, 2010
app pub date -
Dec 2, 2009
filing date -
Dec 4, 2008
priority date (Note) -
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status (Latency Note)
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Abstract
A closing system for a fan cowling on a jet engine of an aircraft that has at least one assembly including a male contrivance integral with the cowling, and a female contrivance integral with the jet engine that has a lower element forming at least one first guide ramp and an upper element forming at least one second guide ramp, with the aforementioned female contrivance being suitable on the one hand for guiding the male contrivance during the opening and/or the closing of the fan cowling, and on the other hand providing a limitation of the radial and circumferential displacements of the male contrivance.
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