Burner assembly for a burner of a gas turbine

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United States of America Patent

PATENT NO 10859270
APP PUB NO 20180080653A1
SERIAL NO

15710093

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Abstract

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A burner assembly of a gas turbine comprising: a tubular body defining the flow path for the hot gas of the combustion during the turbine operation; an aperture for a fuel lance; a wearing ring of a sacrificial material configured to correspond to the edge of the aperture; a contacting leg extending from the wearing ring on the tubular body; a pre-tension system configured to contact the contacting leg in order to provide a pre-tension force on the ring.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC TECHNOLOGY GMBH5400 BADEN

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bizic, Igor Birr, CH 1 2
De, Jonge Jeffrey Alan Birr, CH 1 2
Druzak, Vedran Karlovac, HR 1 2
Imfeld, Jost Baden, CH 16 48
Markovic, Alen Karlovac, HR 4 13
Ruggieri, Giancarlo Baden, CH 1 2

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