Gas turbine engine oil system operation

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 25/20 (2006.01) F01D 15/10 (2006.01) F01D 25/12 (2006.01) F02C 7/06 (2006.01)

Patent

CA 2643489

A method of operating a gas turbine engine (10) having at least one electric machine (20) associated therewith, the engine (10) having an oil system communicating with an electric oil pump (24), at least one bearing cavity (30) of the engine (10) and a coolant passage of the electric machine (20), the method comprising the step of pumping oil intermittently to the oil system to cool the electric machine (20).

La présente invention concerne un procédé de fonctionnement d'un moteur à turbine à gaz (10) qui est associée à au moins une machine électrique (20), le moteur (10) possédant un circuit d'huile qui communique avec une pompe à huile électrique (24), au moins une cavité de palier (30) du moteur (10) et un passage de liquide de refroidissement de la machine électrique (20), le procédé comprenant l'étape consistant à pomper de l'huile en intermittence vers le circuit d'huile pour refroidir la machine électrique (20).

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