FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE COMBUSTOR

FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE COMBUSTOR

A fuel injection assembly (100) includes a fuel injector (200) having end walls (202) spaced apart from one another and side walls (204) extending between the end walls (202). The end walls (202) and the side walls (204) collectively define a first opening (210) for passage of air. At least one fuel...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: PENTECOST, Ronnie Ray, CLIFFORD, Robert Wade, GARCIA, Marissa Singley
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
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator PENTECOST, Ronnie Ray
CLIFFORD, Robert Wade
GARCIA, Marissa Singley
description A fuel injection assembly (100) includes a fuel injector (200) having end walls (202) spaced apart from one another and side walls (204) extending between the end walls (202). The end walls (202) and the side walls (204) collectively define a first opening (210) for passage of air. At least one fuel injection member (212) is disposed within the first opening (210) and extends axially between the end walls (202). The fuel injector (200) terminates at a radially inner surface (232). A boss (300) that is fixedly connected to the combustion liner (42) and extends radially through the cooling flow annulus (132) to a flange portion (306) positioned at the outer sleeve (44). The boss (300) defines a second opening (310) that provides for fluid communication between the fuel injector (200) and the second combustion zone (60). The radially inner surface (232) of the fuel injector (200) is sealingly connected to the flange portion (306) of the boss (300) such that the first opening (210) aligns with the second opening (310).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3974724A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3974724A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3974724A13</originalsourceid><addsrcrecordid>eNrjZDBxC3X1UfD083J1DvH091NwDA529XXyiVRw8w9ScFQICQ1y8vd1dPbw9HNVcPb3dQoNDvEP4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxpbmJuZGJo6GxkQoAQCB4Cch</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE COMBUSTOR</title><source>esp@cenet</source><creator>PENTECOST, Ronnie Ray ; CLIFFORD, Robert Wade ; GARCIA, Marissa Singley</creator><creatorcontrib>PENTECOST, Ronnie Ray ; CLIFFORD, Robert Wade ; GARCIA, Marissa Singley</creatorcontrib><description>A fuel injection assembly (100) includes a fuel injector (200) having end walls (202) spaced apart from one another and side walls (204) extending between the end walls (202). The end walls (202) and the side walls (204) collectively define a first opening (210) for passage of air. At least one fuel injection member (212) is disposed within the first opening (210) and extends axially between the end walls (202). The fuel injector (200) terminates at a radially inner surface (232). A boss (300) that is fixedly connected to the combustion liner (42) and extends radially through the cooling flow annulus (132) to a flange portion (306) positioned at the outer sleeve (44). The boss (300) defines a second opening (310) that provides for fluid communication between the fuel injector (200) and the second combustion zone (60). The radially inner surface (232) of the fuel injector (200) is sealingly connected to the flange portion (306) of the boss (300) such that the first opening (210) aligns with the second opening (310).</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2022</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220330&amp;DB=EPODOC&amp;CC=EP&amp;NR=3974724A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220330&amp;DB=EPODOC&amp;CC=EP&amp;NR=3974724A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PENTECOST, Ronnie Ray</creatorcontrib><creatorcontrib>CLIFFORD, Robert Wade</creatorcontrib><creatorcontrib>GARCIA, Marissa Singley</creatorcontrib><title>FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE COMBUSTOR</title><description>A fuel injection assembly (100) includes a fuel injector (200) having end walls (202) spaced apart from one another and side walls (204) extending between the end walls (202). The end walls (202) and the side walls (204) collectively define a first opening (210) for passage of air. At least one fuel injection member (212) is disposed within the first opening (210) and extends axially between the end walls (202). The fuel injector (200) terminates at a radially inner surface (232). A boss (300) that is fixedly connected to the combustion liner (42) and extends radially through the cooling flow annulus (132) to a flange portion (306) positioned at the outer sleeve (44). The boss (300) defines a second opening (310) that provides for fluid communication between the fuel injector (200) and the second combustion zone (60). The radially inner surface (232) of the fuel injector (200) is sealingly connected to the flange portion (306) of the boss (300) such that the first opening (210) aligns with the second opening (310).</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBxC3X1UfD083J1DvH091NwDA529XXyiVRw8w9ScFQICQ1y8vd1dPbw9HNVcPb3dQoNDvEP4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxpbmJuZGJo6GxkQoAQCB4Cch</recordid><startdate>20220330</startdate><enddate>20220330</enddate><creator>PENTECOST, Ronnie Ray</creator><creator>CLIFFORD, Robert Wade</creator><creator>GARCIA, Marissa Singley</creator><scope>EVB</scope></search><sort><creationdate>20220330</creationdate><title>FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE COMBUSTOR</title><author>PENTECOST, Ronnie Ray ; CLIFFORD, Robert Wade ; GARCIA, Marissa Singley</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3974724A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</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>PENTECOST, Ronnie Ray</creatorcontrib><creatorcontrib>CLIFFORD, Robert Wade</creatorcontrib><creatorcontrib>GARCIA, Marissa Singley</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PENTECOST, Ronnie Ray</au><au>CLIFFORD, Robert Wade</au><au>GARCIA, Marissa Singley</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE COMBUSTOR</title><date>2022-03-30</date><risdate>2022</risdate><abstract>A fuel injection assembly (100) includes a fuel injector (200) having end walls (202) spaced apart from one another and side walls (204) extending between the end walls (202). The end walls (202) and the side walls (204) collectively define a first opening (210) for passage of air. At least one fuel injection member (212) is disposed within the first opening (210) and extends axially between the end walls (202). The fuel injector (200) terminates at a radially inner surface (232). A boss (300) that is fixedly connected to the combustion liner (42) and extends radially through the cooling flow annulus (132) to a flange portion (306) positioned at the outer sleeve (44). The boss (300) defines a second opening (310) that provides for fluid communication between the fuel injector (200) and the second combustion zone (60). The radially inner surface (232) of the fuel injector (200) is sealingly connected to the flange portion (306) of the boss (300) such that the first opening (210) aligns with the second opening (310).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3974724A1
source esp@cenet
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 FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE COMBUSTOR
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-31T19%3A00%3A38IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=PENTECOST,%20Ronnie%20Ray&rft.date=2022-03-30&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3974724A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true