Double bypass turbofan

Details Double bypass turbofan Double bypass turbofan

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 3/077 (2006.01) F02K 1/40 (2006.01)

Patent

CA 2576696

A variable cycle turbofan engine (10) includes first and second fans (14,16) independently joined to respective turbines (26,24). A first bypass duct (46) surrounds a core engine disposed in flow communication with the second fan (16). A second bypass duct (48) surrounds the first bypass duct (46) in flow communication with the first fan (14). A first exhaust nozzle (66) is joined to both the core engine and first bypass duct (46). And, a second exhaust nozzle (68) is joined to the second bypass duct (48).

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