Modular fuel supply device for a gas turbine

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

Patent

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Details

F02C 9/26 (2006.01) F02C 7/32 (2006.01)

Patent

CA 2649330

The invention relates to a gas turbine, in particular a gas turbine aircraft engine with a fuel supply device (10) and a control system. According to the invention, at least parts of the control system, in particular of an engine control system, are integrated in the fuel supply device. Preferably the gas turbine has a motor-driven pump unit (11), a motor control unit (16), and an engine control unit (19) which are designed as line replaceable units.

La présente invention concerne une turbine à gaz, particulièrement un groupe motopropulseur à turbine à gaz, comprenant un dispositif d'alimentation en combustible (10) et un dispositif de régulation. Selon l'invention, au moins certaines pièces du dispositif de régulation, notamment d'un dispositif de régulation du groupe motopropulseur, sont intégrées dans le dispositif d'alimentation en combustible. De manière avantageuse, la turbine à gaz présente une unité moteur-pompe (11), une unité de régulation du moteur (16) et une unité de régulation du groupe motopropulseur (19) conçues comme des équipements remplaçables en escale.

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