Gas turbine engine with variable bypass means

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

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F02K 3/04 (2006.01) B64C 27/12 (2006.01) F02C 3/10 (2006.01) F02C 6/08 (2006.01) F02K 3/075 (2006.01)

Patent

CA 1279767

ABSTRACT OF THE DISCLOSURE GAS TURBINE ENGINE WITH VARIABLE BYPASS MEANS A gas turbine engine for a compound helicopter comprises; a core gas generator, an upstream fan, and a power turbine. Bypass air is selectively directable to either augmentor wings, or to a second power turbine which is mechanically coupled to the first power turbine.

543963

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