Air input device for a turboprop engine

Details Air input device for a turboprop engine Air input device for a turboprop engine

2003-04-28

2008-12-09

Choi, Jacob Y. (Department: 4174)

Aeronautics and astronautics

Aircraft power plants

C244S03400R, C244S129400

Reexamination Certificate

active

07461813

ABSTRACT:
An air intake layout for a turboprop. A nacelle surrounding an intake section of the turboprop behind the fan propeller can be moved away from the main part of the nacelle and can be divided into two parts that may be extracted so as to leave full access to the panel leading to equipment in a central compartment, whereas the panel was partially covered by the air intake leading edge.

REFERENCES:
patent: 5427332 (1995-06-01), Rauckhorst et al.
patent: 5497961 (1996-03-01), Newton
patent: 5941061 (1999-08-01), Sherry et al.
patent: 6129509 (2000-10-01), Cousin et al.
patent: 0 971 111 (2000-01-01), None

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