BRENNKAMMERANORDNUNG

The invention concerns a combustion chamber for turbojet engines. The combustion chamber is of the annular type and consists of two coaxial flame tubes opening into a common dilution and mixing zone. The inner tube is designed for low operating ratings of the engine, the outer tube for high ratings....

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: JULES CARUEL,JACQUES EMILE, DENIS GASTEBOIS,PHILIPPE MARC
Format: Patent
Sprache:ger
Schlagworte:
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