BURNERS FOR REHEAT COMBUSTION CHAMBERS

A burner for the reheat chamber of a dual-flow gas turbine jet engine, comprising a fuel-prevaporizing device having a feedpipe fed jointly from a liquid fuel source and a secondary air duct and having a discharge pipe opening into the reheat chamber to discharge thereinto a mixture of air from the...

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Hauptverfasser: ARMAND JEAN-BAPTISTE LACROIX, LOUIS JULES BAUGER
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A burner for the reheat chamber of a dual-flow gas turbine jet engine, comprising a fuel-prevaporizing device having a feedpipe fed jointly from a liquid fuel source and a secondary air duct and having a discharge pipe opening into the reheat chamber to discharge thereinto a mixture of air from the secondary duct and of fuel preheated by heat exchange with a primary flow of hot gases from the turbine.