Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber

A CG A C An aerodynamic injection system for injecting an air/fuel mixture into a turbomachine combustion chamber comprises a tubular structure of axis XX′ that opens out at a downstream end for delivering the air/fuel mixture, at least one air feed channel that opens out into the structure so as to...

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Bibliographische Detailangaben

Hauptverfasser:	Mantchenkov, Igor, Noel, Thomas, Novikov, Alexander, Orlov, Vladimir, Pikalov, Valery, Rollin, Gilles
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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