Gas turbine engine fixed speed light-off system and method

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

Patent

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F02C 7/26 (2006.01)

Patent

CA 2234318

A gas turbine engine light-off system and method in which the gas turbine engine is operated at a fixed speed to provide a substantially constant supply of combustion air for light-off and the fuel flow is ramped up to achieve the correct fuel-to-air ratio for light-off.

Cette invention concerne un circuit et une méthode d'allumage de turbine à gaz lancée à vitesse constante pour obtenir une arrivée sensiblement constante d'air de combustion à l'allumage, le mélange combustible-air appropriée étant réalisé par accroissement progressif du débit de combustible.

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