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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Bibliographic Details
Main Authors STALDER MARCEL, JOOS FRANZ
Format Patent
LanguageEnglish
Published 29.08.2006
Subjects
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