METHOD AND ARRANGEMENT FOR GAS TURBINE ENGINE SURGE CONTROL

The invention relates to a surge control method for a gas turbine engine. The method includes providing a gas turbine engine having a compressor, a combustor, downstream of the compressor, with a hot gas path, a turbine downstream of the combustor, with a hot gas path. The method further includes mo...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: WAELCHLI RENE, JAKOBY RALF, STEIGER ULRICH ROBERT, STUDERUS ADRIEN FRANZ
Format: Patent
Sprache:eng
Schlagworte:
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