Gas turbine engine with power transfer and method

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

Patent

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Details

F02C 7/08 (2006.01) B64D 37/34 (2006.01) F01D 13/02 (2006.01) F02C 7/224 (2006.01) F02C 7/32 (2006.01) F02C 7/36 (2006.01)

Patent

CA 2625851

The gas turbine engine 10 comprises at least one electrical generator 30, 32 and an electrical heater 34, 26 associated with a gas path of the engine 10. The heater 34, 36 is powered by the generator 30, 32 to selectively add heat to the gas turbine cycle.

L'invention concerne une turbine à gaz (10) comprenant au moins un générateur électrique (30, 32) et un dispositif de chauffage électrique (34, 26) associé à un chemin de gaz de la turbine (10). Le dispositif de chauffage électrique (34, 36) est alimenté par le générateur (30, 32) afin d'apporter sélectivement de la chaleur au cycle de turbine à gaz.

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