F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
244/37, 60/82
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
Hall John M.
Jordan Terence
Fetherstonhaugh & Co.
Hall John M.
Jordan Terence
Rolls-Royce Plc
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