COMBUSTION ASSEMBLY

A combustion assembly for a gas turbine includes a flame tube and a fuel supply including a flow rate limiter supplying an injector. The flow rate limiter and the fuel injector are formed in one piece.

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Bibliographic Details
Main Authors LAVIGNOTTE, Stéphane, SAVARY, Nicolas, Roland, Guy, LAILHACAR, Christophe, LAMAISON, Olivier
Format Patent
LanguageEnglish
French
German
Published 27.03.2024
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
BURNERS
COMBUSTION APPARATUS
COMBUSTION ENGINES
COMBUSTION PROCESSES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A combustion assembly for a gas turbine includes a flame tube and a fuel supply including a flow rate limiter supplying an injector. The flow rate limiter and the fuel injector are formed in one piece.
Bibliography:Application Number: EP20210711937