Transition nozzle combustion system

Transition nozzle combustion system

The present invention provides a combustion system for use with a cooling flow. The combustion system may include a head end, an aft end, a transition nozzle (110) extending from the head end to the aft end, and an impingement sleeve (160) surrounding the transition nozzle (110). The impingement sle...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Maldonado, Jaime Javier, Kim, Won-Wook, Mcmahan, Kevin Weston
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
ENGINE PLANTS IN GENERAL
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
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 Maldonado, Jaime Javier
Kim, Won-Wook
Mcmahan, Kevin Weston
description The present invention provides a combustion system for use with a cooling flow. The combustion system may include a head end, an aft end, a transition nozzle (110) extending from the head end to the aft end, and an impingement sleeve (160) surrounding the transition nozzle (110). The impingement sleeve (160) may define a first cavity (170) in communication with the head end for a first portion (210) of the cooling flow (200) and a second cavity (180) in communication with the aft end for a second portion (220) of the cooling flow (200). The transition nozzle (110) may include a number of cooling holes (230) thereon in communication with the second portion (220) of the cooling flow (200).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2647800A3</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2647800A3</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2647800A33</originalsourceid><addsrcrecordid>eNrjZFAOKUrMK84syczPU8jLr6rKSVVIzs9NKi0GixRXFpek5vIwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXACMzE3MLAwNHY2MilAAA4scmwQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Transition nozzle combustion system</title><source>esp@cenet</source><creator>Maldonado, Jaime Javier ; Kim, Won-Wook ; Mcmahan, Kevin Weston</creator><creatorcontrib>Maldonado, Jaime Javier ; Kim, Won-Wook ; Mcmahan, Kevin Weston</creatorcontrib><description>The present invention provides a combustion system for use with a cooling flow. The combustion system may include a head end, an aft end, a transition nozzle (110) extending from the head end to the aft end, and an impingement sleeve (160) surrounding the transition nozzle (110). The impingement sleeve (160) may define a first cavity (170) in communication with the head end for a first portion (210) of the cooling flow (200) and a second cavity (180) in communication with the aft end for a second portion (220) of the cooling flow (200). The transition nozzle (110) may include a number of cooling holes (230) thereon in communication with the second portion (220) of the cooling flow (200).</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; ENGINE PLANTS IN GENERAL ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2018</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=20180411&amp;DB=EPODOC&amp;CC=EP&amp;NR=2647800A3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20180411&amp;DB=EPODOC&amp;CC=EP&amp;NR=2647800A3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Maldonado, Jaime Javier</creatorcontrib><creatorcontrib>Kim, Won-Wook</creatorcontrib><creatorcontrib>Mcmahan, Kevin Weston</creatorcontrib><title>Transition nozzle combustion system</title><description>The present invention provides a combustion system for use with a cooling flow. The combustion system may include a head end, an aft end, a transition nozzle (110) extending from the head end to the aft end, and an impingement sleeve (160) surrounding the transition nozzle (110). The impingement sleeve (160) may define a first cavity (170) in communication with the head end for a first portion (210) of the cooling flow (200) and a second cavity (180) in communication with the aft end for a second portion (220) of the cooling flow (200). The transition nozzle (110) may include a number of cooling holes (230) thereon in communication with the second portion (220) of the cooling flow (200).</description><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAOKUrMK84syczPU8jLr6rKSVVIzs9NKi0GixRXFpek5vIwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXACMzE3MLAwNHY2MilAAA4scmwQ</recordid><startdate>20180411</startdate><enddate>20180411</enddate><creator>Maldonado, Jaime Javier</creator><creator>Kim, Won-Wook</creator><creator>Mcmahan, Kevin Weston</creator><scope>EVB</scope></search><sort><creationdate>20180411</creationdate><title>Transition nozzle combustion system</title><author>Maldonado, Jaime Javier ; Kim, Won-Wook ; Mcmahan, Kevin Weston</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2647800A33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Maldonado, Jaime Javier</creatorcontrib><creatorcontrib>Kim, Won-Wook</creatorcontrib><creatorcontrib>Mcmahan, Kevin Weston</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Maldonado, Jaime Javier</au><au>Kim, Won-Wook</au><au>Mcmahan, Kevin Weston</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Transition nozzle combustion system</title><date>2018-04-11</date><risdate>2018</risdate><abstract>The present invention provides a combustion system for use with a cooling flow. The combustion system may include a head end, an aft end, a transition nozzle (110) extending from the head end to the aft end, and an impingement sleeve (160) surrounding the transition nozzle (110). The impingement sleeve (160) may define a first cavity (170) in communication with the head end for a first portion (210) of the cooling flow (200) and a second cavity (180) in communication with the aft end for a second portion (220) of the cooling flow (200). The transition nozzle (110) may include a number of cooling holes (230) thereon in communication with the second portion (220) of the cooling flow (200).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2647800A3
source esp@cenet
subjects BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
ENGINE PLANTS IN GENERAL
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title Transition nozzle combustion system
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-17T02%3A02%3A22IST&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=Maldonado,%20Jaime%20Javier&rft.date=2018-04-11&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2647800A3%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