Gas turbine engine with outer fans

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 5/22 (2006.01) F01D 5/02 (2006.01) F02K 3/04 (2006.01) F02K 3/077 (2006.01)

Patent

CA 2720157

A gas turbine engine comprising an outer fan system (401) is disclosed, having an outer fan first stage (431) having a circumferential row of outer fan first blades (142), an outer fan second stage (134) having a circumferential row of outer fan second blades (144) located axially aft from the outer fan first stage wherein the outer fan first stage and the outer fan second stage are adapted to rotate with a fan rotor (420).

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