A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability

A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability

A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability. The invention further relates to a new method for flame holding with least pressure drop and flame temperature, in gas turbine engine combustors, wherein the...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Deepika, V, Rajabharathi, N, Chakravarthy, S.R, Preethi, R.S, Muruganandam, T.M, Shanmugaprabhu, S
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
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 Deepika, V
Rajabharathi, N
Chakravarthy, S.R
Preethi, R.S
Muruganandam, T.M
Shanmugaprabhu, S
description A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability. The invention further relates to a new method for flame holding with least pressure drop and flame temperature, in gas turbine engine combustors, wherein the liner of the combustor is partially or fully replaced with a "swirl mesh". The invention has lean direct injection for fuel distribution over several points in gas turbine combustors along with swirl arrangement for air injection which provides low pollutant emission and low combustion instability.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_AU2017296362A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AU2017296362A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_AU2017296362A13</originalsourceid><addsrcrecordid>eNqNjMEKglAQRd20iOofBloHqWC0lCj6gFrLU0edmDdPnBHpI_rnRPqAVofLuZx19MlBJxoYPGoHjE6gpgErA5LXDAoCVZAKe4MmDLNUG6gcDWto2HmELnBN0i6WwwR9YB7NiQF6Up0DCk5q8GTUuiUYmrnpy1GXRaLmSmKy9zZaNY4Vdz9uov3t-rjcD9iHArV3FQpakT-TY3xKzlmaJXmc_vf6AhVLT-8</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability</title><source>esp@cenet</source><creator>Deepika, V ; Rajabharathi, N ; Chakravarthy, S.R ; Preethi, R.S ; Muruganandam, T.M ; Shanmugaprabhu, S</creator><creatorcontrib>Deepika, V ; Rajabharathi, N ; Chakravarthy, S.R ; Preethi, R.S ; Muruganandam, T.M ; Shanmugaprabhu, S</creatorcontrib><description>A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability. The invention further relates to a new method for flame holding with least pressure drop and flame temperature, in gas turbine engine combustors, wherein the liner of the combustor is partially or fully replaced with a "swirl mesh". The invention has lean direct injection for fuel distribution over several points in gas turbine combustors along with swirl arrangement for air injection which provides low pollutant emission and low combustion instability.</description><language>eng</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>2019</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=20190307&amp;DB=EPODOC&amp;CC=AU&amp;NR=2017296362A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20190307&amp;DB=EPODOC&amp;CC=AU&amp;NR=2017296362A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Deepika, V</creatorcontrib><creatorcontrib>Rajabharathi, N</creatorcontrib><creatorcontrib>Chakravarthy, S.R</creatorcontrib><creatorcontrib>Preethi, R.S</creatorcontrib><creatorcontrib>Muruganandam, T.M</creatorcontrib><creatorcontrib>Shanmugaprabhu, S</creatorcontrib><title>A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability</title><description>A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability. The invention further relates to a new method for flame holding with least pressure drop and flame temperature, in gas turbine engine combustors, wherein the liner of the combustor is partially or fully replaced with a "swirl mesh". The invention has lean direct injection for fuel distribution over several points in gas turbine combustors along with swirl arrangement for air injection which provides low pollutant emission and low combustion instability.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjMEKglAQRd20iOofBloHqWC0lCj6gFrLU0edmDdPnBHpI_rnRPqAVofLuZx19MlBJxoYPGoHjE6gpgErA5LXDAoCVZAKe4MmDLNUG6gcDWto2HmELnBN0i6WwwR9YB7NiQF6Up0DCk5q8GTUuiUYmrnpy1GXRaLmSmKy9zZaNY4Vdz9uov3t-rjcD9iHArV3FQpakT-TY3xKzlmaJXmc_vf6AhVLT-8</recordid><startdate>20190307</startdate><enddate>20190307</enddate><creator>Deepika, V</creator><creator>Rajabharathi, N</creator><creator>Chakravarthy, S.R</creator><creator>Preethi, R.S</creator><creator>Muruganandam, T.M</creator><creator>Shanmugaprabhu, S</creator><scope>EVB</scope></search><sort><creationdate>20190307</creationdate><title>A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability</title><author>Deepika, V ; Rajabharathi, N ; Chakravarthy, S.R ; Preethi, R.S ; Muruganandam, T.M ; Shanmugaprabhu, S</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_AU2017296362A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2019</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>Deepika, V</creatorcontrib><creatorcontrib>Rajabharathi, N</creatorcontrib><creatorcontrib>Chakravarthy, S.R</creatorcontrib><creatorcontrib>Preethi, R.S</creatorcontrib><creatorcontrib>Muruganandam, T.M</creatorcontrib><creatorcontrib>Shanmugaprabhu, S</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Deepika, V</au><au>Rajabharathi, N</au><au>Chakravarthy, S.R</au><au>Preethi, R.S</au><au>Muruganandam, T.M</au><au>Shanmugaprabhu, S</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability</title><date>2019-03-07</date><risdate>2019</risdate><abstract>A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability. The invention further relates to a new method for flame holding with least pressure drop and flame temperature, in gas turbine engine combustors, wherein the liner of the combustor is partially or fully replaced with a "swirl mesh". The invention has lean direct injection for fuel distribution over several points in gas turbine combustors along with swirl arrangement for air injection which provides low pollutant emission and low combustion instability.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_AU2017296362A1
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 A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-26T08%3A59%3A13IST&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=Deepika,%20V&rft.date=2019-03-07&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EAU2017296362A1%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