Fuel Lance for a Gas Turbine Engine

The invention relates to a fuel lance (7) for introducing fuel into a gas flow in a combustor (1) of a gas turbine engine, whereby a region of the lance (7) through which the fuel is introduced into the gas flow comprises a generally helical formation (12).

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Bibliographic Details
Main Authors KELSALL, GREGORY JOHN, EROGLU, ADNAN, POYYAPAKKAM, MADHAVAN NARASIMHAN
Format Patent
LanguageEnglish
French
German
Published 24.12.2014
Subjects
BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:The invention relates to a fuel lance (7) for introducing fuel into a gas flow in a combustor (1) of a gas turbine engine, whereby a region of the lance (7) through which the fuel is introduced into the gas flow comprises a generally helical formation (12).
Bibliography:Application Number: EP20090171054