Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same

A turbomachine combustor nozzle includes a monolithic nozzle component having a plate element and a plurality of nozzle elements. Each of the plurality of nozzle elements includes a first end extending from the plate element to a second end. The plate element and plurality of nozzle elements are for...

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Bibliographic Details
Main Authors STOIA LUCAS JOHN, VANSELOW JOHN DRAKE, MELTON PATRICK BENEDICT, WESTMORELAND JAMES HAROLD, JOHNSON THOMAS EDWARD, STEVENSON CHRISTIAN XAVIER
Format Patent
LanguageEnglish
Published 23.02.2016
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:A turbomachine combustor nozzle includes a monolithic nozzle component having a plate element and a plurality of nozzle elements. Each of the plurality of nozzle elements includes a first end extending from the plate element to a second end. The plate element and plurality of nozzle elements are formed as a unitary component. A plate member is joined with the nozzle component. The plate member includes an outer edge that defines first and second surfaces and a plurality of openings extending between the first and second surfaces. The plurality of openings are configured and disposed to register with and receive the second end of corresponding ones of the plurality of nozzle elements.
Bibliography:Application Number: US201213482540