Assembly of a fuel injector in a combustion chamber for a gas turbine

A combustion chamber includes an upstream end wall having an aperture and a fuel injector. An air swirler (48) is mounted radially movable with respect to the aperture. An inner wall (50) of the air swirler (48) has a first portion (70). A fuel injector head of the fuel injector is arranged coaxiall...

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Bibliographische Detailangaben
1. Verfasser: Tentorio, Luca
Format: Patent
Sprache:eng ; fre ; ger
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