Invention Grant
US08590317B2 Gas turbine engine starting method and control device 有权
燃气轮机起动方法和控制装置

Gas turbine engine starting method and control device
Abstract:
A method of starting a gas turbine engine by use of a start sequence is provided. Turbine speed and fuel delivery are coordinated so as to provide a fuel/air mixture at an ignition device allowing a successful ignition. If a successful ignition has not occurred by end of the start sequence the gas turbine engine is purged and the start sequence is repeated after the purging of the gas turbine engine.
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