INJECTOR HEAD WITH A RESONATOR FOR A GAS TURBINE ENGINE

A fuel injector for a combustor of a gas turbine engine is disclosed herein. In embodiments, the fuel injector includes an injector head adjoining a stem. The injector head includes a main premix passage, a main air inlet, vanes, and a main premix resonator. The main premix passage extends through t...

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Hauptverfasser:	Schuger, Ariel, Vega, Ashley, Blust, II, James Wilfrid, Arellano, Leonel
Format:	Patent
Sprache:	eng
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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creator	Schuger, Ariel Vega, Ashley Blust, II, James Wilfrid Arellano, Leonel
description	A fuel injector for a combustor of a gas turbine engine is disclosed herein. In embodiments, the fuel injector includes an injector head adjoining a stem. The injector head includes a main premix passage, a main air inlet, vanes, and a main premix resonator. The main premix passage extends through the injector head and the main air inlet directs compressed air into the main premix passage. The vanes are located within the main premix passage for swirling the compressed air. The main premix resonator is located adjacent to and downstream of the vanes.
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In embodiments, the fuel injector includes an injector head adjoining a stem. The injector head includes a main premix passage, a main air inlet, vanes, and a main premix resonator. The main premix passage extends through the injector head and the main air inlet directs compressed air into the main premix passage. The vanes are located within the main premix passage for swirling the compressed air. 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In embodiments, the fuel injector includes an injector head adjoining a stem. The injector head includes a main premix passage, a main air inlet, vanes, and a main premix resonator. The main premix passage extends through the injector head and the main air inlet directs compressed air into the main premix passage. The vanes are located within the main premix passage for swirling the compressed air. The main premix resonator is located adjacent to and downstream of the vanes.</description><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDD39PNydQ7xD1LwcHV0UQj3DPFQcFQIcg3293MEiboBsaOCu2OwQkhokJOnn6uCq587kOJhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfGhwUYGhhaGZsaWZuaOhsbEqQIAqj0oxA</recordid><startdate>20180614</startdate><enddate>20180614</enddate><creator>Schuger, Ariel</creator><creator>Vega, Ashley</creator><creator>Blust, II, James Wilfrid</creator><creator>Arellano, Leonel</creator><scope>EVB</scope></search><sort><creationdate>20180614</creationdate><title>INJECTOR HEAD WITH A RESONATOR FOR A GAS TURBINE ENGINE</title><author>Schuger, Ariel ; Vega, Ashley ; Blust, II, James Wilfrid ; Arellano, Leonel</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2018163967A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</creationdate><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Schuger, Ariel</creatorcontrib><creatorcontrib>Vega, Ashley</creatorcontrib><creatorcontrib>Blust, II, James Wilfrid</creatorcontrib><creatorcontrib>Arellano, Leonel</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Schuger, Ariel</au><au>Vega, Ashley</au><au>Blust, II, James Wilfrid</au><au>Arellano, Leonel</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>INJECTOR HEAD WITH A RESONATOR FOR A GAS TURBINE ENGINE</title><date>2018-06-14</date><risdate>2018</risdate><abstract>A fuel injector for a combustor of a gas turbine engine is disclosed herein. In embodiments, the fuel injector includes an injector head adjoining a stem. The injector head includes a main premix passage, a main air inlet, vanes, and a main premix resonator. The main premix passage extends through the injector head and the main air inlet directs compressed air into the main premix passage. The vanes are located within the main premix passage for swirling the compressed air. The main premix resonator is located adjacent to and downstream of the vanes.</abstract><oa>free_for_read</oa></addata></record>
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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
title	INJECTOR HEAD WITH A RESONATOR FOR A GAS TURBINE ENGINE
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