Fan exhaust nozzle for turbofan engine

Details Fan exhaust nozzle for turbofan engine Fan exhaust nozzle for turbofan engine

2011-03-08

2011-03-08

Kim, Ted (Department: 3741)

Power plants

Reaction motor

Interrelated reaction motors

C060S770000, C239S265190

Reexamination Certificate

active

07900433

ABSTRACT:
The cross sectional flow area of a fan discharge nozzle on one side of a central plane of an associated gas turbine engine power plant is greater than the corresponding flow area of the fan discharge nozzle on an opposite side of the central plane to compensate for the blockage of fan airflow by a pylon.

REFERENCES:
patent: 3393518 (1968-07-01), Bridge
patent: 3721389 (1973-03-01), MacKinnon et al.
patent: 3806067 (1974-04-01), Kutney
patent: 4280587 (1981-07-01), Bhat
patent: 4449683 (1984-05-01), Gratzer et al.
patent: 5860276 (1999-01-01), Newton
patent: 7165744 (2007-01-01), Howarth et al.

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