Method for igniting the combustion chamber of a gas turbine unit and an ignition device for carrying out the method
In a method for igniting the combustion chamber of a gas turbine unit, a safely working ignition and a long lifetime of the ignition device ( 10 ) is achieved by discharging a compressed gas with a supercritical pressure ratio through a nozzle ( 21 ) and heating it up to a temperature sufficient to...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
29.08.2006
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Subjects | |
Online Access | Get full text |
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