Aeroengine nacelle
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United States of America Patent
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-
Aug 15, 2006
Grant Date -
Dec 2, 2004
app pub date -
Oct 31, 2003
filing date -
Jun 2, 2003
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A nacelle (55) for a gas turbine engine (10), the engine (10) comprising accessories (34) mounted to a fan casing (28) and a core engine (9), the nacelle (55) substantially surrounds the engine (10) and comprises an intake (12) and a thrust reverser unit (31). The thrust reverser unit (31) is formed by two generally C-shaped portions (31a, 31b). The thrust reverser unit (31) is openable to provide access to the accessories (34) and the core engine (9). The nacelle (55) further comprises a fan containment casing (33) that is integral with the intake (12).
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