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

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

A turbomachine combustor nozzle includes a monolithic nozzle component 80 having a plate element 100 and a plurality of nozzle elements 104. Each of the plurality of nozzle elements includes a first end 106 extending from the plate element 100 to a second end. The plate element and plurality of nozz...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Stoia, Lucas John, Vanselow, John Drake, Stevenson, Christian Xavier, Melton, Patrick Benedict, Westmoreland, James Harold, Johnson, Thomas Edward
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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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Beschreibung
Zusammenfassung:A turbomachine combustor nozzle includes a monolithic nozzle component 80 having a plate element 100 and a plurality of nozzle elements 104. Each of the plurality of nozzle elements includes a first end 106 extending from the plate element 100 to a second end. The plate element and plurality of nozzle elements are formed as a unitary component. A plate member 83 is joined with the nozzle component 80. The plate member 83 includes an outer edge that defines first and second surfaces and a plurality of openings 120 extending between the first and second surfaces. The plurality of openings 120 are configured and disposed to register with and receive the second end of corresponding ones of the plurality of nozzle elements 104.