Integrated airbreathing and non-airbreathing engine system

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

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Details

F02K 9/78 (2006.01) F02K 1/12 (2006.01) F02K 1/78 (2006.01) F02K 9/97 (2006.01)

Patent

CA 2578554

An engine assembly includes a gas-turbine engine having a tailcone portion and a bypass duct, a rocket engine combustion assembly located at the tailcone portion of the gas-turbine engine, and a movable nozzle segment subassembly that is selectively engageable with the gas-turbine engine bypass duct in an open position and with the rocket engine combustion assembly in a closed position.

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