FUEL LANCE FOR A GAS TURBINE ENGINE
A fuel lance (7) for introducing fuel into a gas flow in a combustor (1) of a gas turbine engine includes a region of the lance (7) through which the fuel is introduced into the gas flow having a generally helical formation (12).
Saved in:
Main Authors | , , |
---|---|
Format | Patent |
Language | English |
Published |
01.04.2010
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | A fuel lance (7) for introducing fuel into a gas flow in a combustor (1) of a gas turbine engine includes a region of the lance (7) through which the fuel is introduced into the gas flow having a generally helical formation (12). |
---|---|
Bibliography: | Application Number: US20080241223 |