Convertible turbo-fan/shaft aircraft propulsion engine

Details Convertible turbo-fan/shaft aircraft propulsion engine Convertible turbo-fan/shaft aircraft propulsion engine

F - Mech Eng,Light,Heat,Weapons

02

C

74/106

F02C 7/36 (2006.01) F01D 15/12 (2006.01) F02C 6/20 (2006.01) F02K 3/04 (2006.01)

Patent

CA 1280297

ABSTRACT A composite turbo-fan/ turbo-shaft gas turbine engine system is provided wherein the fan is driven through a variable geometry torque converter whose input is driven by the turbine power shaft supplied through a reduction gear. Actuation of the variable geometry of the torque converter provides a wide variety of operating modes including all power to the power output shaft and combinations in between.

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