Premixed Fuel Nozzle
A fuel injector assembly for a gas turbine engine is generally provided. The first fuel injector includes a first centerbody surrounding a first walled fuel injection circuit. A first fuel injection port is extended at least partially radially through the first centerbody in fluid communication with...
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Main Authors | , , , , , |
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Format | Patent |
Language | English |
Published |
04.06.2020
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Subjects | |
Online Access | Get full text |
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Abstract | A fuel injector assembly for a gas turbine engine is generally provided. The first fuel injector includes a first centerbody surrounding a first walled fuel injection circuit. A first fuel injection port is extended at least partially radially through the first centerbody in fluid communication with the first walled fuel injection circuit. The first centerbody defines a cooling circuit surrounding the first walled fuel injection circuit. The first centerbody defines a plurality of cooling openings at a downstream end of the first centerbody. The plurality of cooling openings is in fluid communication with the cooling circuit. The first centerbody defines an axially extended cooling outlet at the downstream end of the first centerbody. |
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AbstractList | A fuel injector assembly for a gas turbine engine is generally provided. The first fuel injector includes a first centerbody surrounding a first walled fuel injection circuit. A first fuel injection port is extended at least partially radially through the first centerbody in fluid communication with the first walled fuel injection circuit. The first centerbody defines a cooling circuit surrounding the first walled fuel injection circuit. The first centerbody defines a plurality of cooling openings at a downstream end of the first centerbody. The plurality of cooling openings is in fluid communication with the cooling circuit. The first centerbody defines an axially extended cooling outlet at the downstream end of the first centerbody. |
Author | Mishra, Ranjeet Kumar Boehm, Randall Charles Naik, Pradeep Lind, David Albin Boardman, Gregory Allen Patra, Ajoy |
Author_xml | – fullname: Naik, Pradeep – fullname: Patra, Ajoy – fullname: Lind, David Albin – fullname: Mishra, Ranjeet Kumar – fullname: Boardman, Gregory Allen – fullname: Boehm, Randall Charles |
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Notes | Application Number: US201816203997 |
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Snippet | A fuel injector assembly for a gas turbine engine is generally provided. The first fuel injector includes a first centerbody surrounding a first walled fuel... |
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SubjectTerms | BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
Title | Premixed Fuel Nozzle |
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