Aeroengine nacelle

Details Aeroengine nacelle Aeroengine nacelle

2006-08-15

2006-08-15

Poon, Peter M. (Department: 3643)

Aeronautics and astronautics

Aircraft power plants

C244S054000

Reexamination Certificate

active

07090165

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).

REFERENCES:
patent: 4585189 (1986-04-01), Buxton
patent: 5157915 (1992-10-01), Bart
patent: 6227485 (2001-05-01), Porte
patent: 6334730 (2002-01-01), Porte

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