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...
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Patent |
Sprache: | eng ; fre ; ger |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Schreiben Sie den ersten Kommentar!