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Title: Combustor inlet flow conditioner

Patent ·
OSTI ID:1650992

A combustor includes an inlet flow conditioner. The inlet flow conditioner includes a sleeve that circumferentially surrounds a portion of a fuel nozzle assembly and that extends from a forward end of a combustion liner to an inner surface of an end cover. The sleeve defines a plurality of apertures circumferentially spaced about the sleeve. A portion of the inner surface of the end cover and the sleeve define a head end volume of the combustor. An inlet to a premix passage of at least one fuel nozzle of the fuel nozzle assembly is disposed within and is in fluid communication with the head end volume.

Research Organization:
This invention was made with Government support under Contract No. DE-FE0023965 awarded by the United States Department of Energy. The Government has certain rights in this invention.
Sponsoring Organization:
USDOE
DOE Contract Number:
FE0023965
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
10,677,466
Application Number:
15/292,485
OSTI ID:
1650992
Resource Relation:
Patent File Date: 10/13/2016
Country of Publication:
United States
Language:
English

References (21)

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Method of forming a microchannel cooled component patent-application August 2014
Combustor Can Flow Conditioner patent-application January 2011
Flow sleeve for a combustion module of a gas turbine patent-application September 2014
Air Biasing System in a Gas Turbine Combustor patent-application January 2012
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Gas turbine and the combustor thereof patent July 2005
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Combustor assembly comprising a combustor device, a transition duct and a flow conditioner patent July 2013
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Can-annular combustor burner with non-uniform airflow mitigation flow conditioner patent November 2018
System having a multi-tube fuel nozzle with an inlet flow conditioner patent March 2016
Air Flow Conditioner for a Combustor Can of a Gas Turbine Engine patent-application October 2007
Gas turbine combustor having bypass and annular gas passage for reducing uneven temperature distribution in combustor tail cross section patent March 2005
Endcover Assembly for a Combustor patent-application August 2018
Combustor patent-application June 2010
Gas turbine and gas turbine combustor patent October 2003
Combustor flow sleeve with optimized cooling and airflow distribution patent August 2009
Gas turbine combustor including a diffusion nozzle assembly with a double cylindrical structure patent September 1995
System for conditioning air flow into a multi-nozzle assembly patent-application January 2013