Fan exhaust nozzle for turbofan engine

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

B - Operations, Transporting

64

D

B64D 29/00 (2006.01) B64D 33/04 (2006.01) F02K 1/78 (2006.01)

Patent

CA 2598304

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.

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