COMBUSTION CHAMBER ASSEMBLY FOR OPERATION WITH LIQUID AND/OR GASEOUS FUEL, GAS TURBINE ASSEMBLY AND METHOD
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United States of America Patent
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Issued Date -
Feb 15, 2024
app pub date -
Jul 25, 2023
filing date -
Aug 10, 2022
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Abstract
The invention concerns a combustion chamber assembly, in particular for use in an aircraft engine, including:
- a peripheral wall which borders a combustion space oriented along a longitudinal axis, andat least one, preferably a plurality of fuel nozzle(s) arranged on the input side of the combustion space for the supply of liquid fuel to the combustion space.
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