COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER

COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER

PROBLEM TO BE SOLVED: To provide a combustion chamber (10) for a gas turbine, having a plurality of first and second premixed fuel supply devices (11, 12) connected to a combustion device (13), which has a first zone (14) connected with the first premixed fuel supply devices (11) and a second zone (...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: EROGLU ADNAN, KNOEPFEL HANS PETER
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 EROGLU ADNAN
KNOEPFEL HANS PETER
description PROBLEM TO BE SOLVED: To provide a combustion chamber (10) for a gas turbine, having a plurality of first and second premixed fuel supply devices (11, 12) connected to a combustion device (13), which has a first zone (14) connected with the first premixed fuel supply devices (11) and a second zone (15) connected with the second premixed fuel supply devices (12).SOLUTION: The second premixed fuel supply devices (12) are shifted along a longitudinal axis (16) of a combustion device with respect to the first premixed fuel supply devices (11). The first zones (14) are disposed at the upstream of the second premixed fuel supply devices (12) with respect to the longitudinal axis of the combustion device.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2012068015A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2012068015A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2012068015A3</originalsourceid><addsrcrecordid>eNrjZLBz9vd1Cg0O8fT3U3D2cPR1cg3SUXD0c1HwdQ3x8HdR8HdT8A9wDXIM8fRzV8BUy8PAmpaYU5zKC6W5GZTcXEOcPXRTC_LjU4sLEpNT81JL4r0CjAwMjQzMLAwMTR2NiVIEAJPhKlM</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER</title><source>esp@cenet</source><creator>EROGLU ADNAN ; KNOEPFEL HANS PETER</creator><creatorcontrib>EROGLU ADNAN ; KNOEPFEL HANS PETER</creatorcontrib><description>PROBLEM TO BE SOLVED: To provide a combustion chamber (10) for a gas turbine, having a plurality of first and second premixed fuel supply devices (11, 12) connected to a combustion device (13), which has a first zone (14) connected with the first premixed fuel supply devices (11) and a second zone (15) connected with the second premixed fuel supply devices (12).SOLUTION: The second premixed fuel supply devices (12) are shifted along a longitudinal axis (16) of a combustion device with respect to the first premixed fuel supply devices (11). The first zones (14) are disposed at the upstream of the second premixed fuel supply devices (12) with respect to the longitudinal axis of the combustion device.</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>2012</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=20120405&amp;DB=EPODOC&amp;CC=JP&amp;NR=2012068015A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20120405&amp;DB=EPODOC&amp;CC=JP&amp;NR=2012068015A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>EROGLU ADNAN</creatorcontrib><creatorcontrib>KNOEPFEL HANS PETER</creatorcontrib><title>COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER</title><description>PROBLEM TO BE SOLVED: To provide a combustion chamber (10) for a gas turbine, having a plurality of first and second premixed fuel supply devices (11, 12) connected to a combustion device (13), which has a first zone (14) connected with the first premixed fuel supply devices (11) and a second zone (15) connected with the second premixed fuel supply devices (12).SOLUTION: The second premixed fuel supply devices (12) are shifted along a longitudinal axis (16) of a combustion device with respect to the first premixed fuel supply devices (11). The first zones (14) are disposed at the upstream of the second premixed fuel supply devices (12) with respect to the longitudinal axis of the combustion device.</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>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLBz9vd1Cg0O8fT3U3D2cPR1cg3SUXD0c1HwdQ3x8HdR8HdT8A9wDXIM8fRzV8BUy8PAmpaYU5zKC6W5GZTcXEOcPXRTC_LjU4sLEpNT81JL4r0CjAwMjQzMLAwMTR2NiVIEAJPhKlM</recordid><startdate>20120405</startdate><enddate>20120405</enddate><creator>EROGLU ADNAN</creator><creator>KNOEPFEL HANS PETER</creator><scope>EVB</scope></search><sort><creationdate>20120405</creationdate><title>COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER</title><author>EROGLU ADNAN ; KNOEPFEL HANS PETER</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2012068015A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2012</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>EROGLU ADNAN</creatorcontrib><creatorcontrib>KNOEPFEL HANS PETER</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>EROGLU ADNAN</au><au>KNOEPFEL HANS PETER</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER</title><date>2012-04-05</date><risdate>2012</risdate><abstract>PROBLEM TO BE SOLVED: To provide a combustion chamber (10) for a gas turbine, having a plurality of first and second premixed fuel supply devices (11, 12) connected to a combustion device (13), which has a first zone (14) connected with the first premixed fuel supply devices (11) and a second zone (15) connected with the second premixed fuel supply devices (12).SOLUTION: The second premixed fuel supply devices (12) are shifted along a longitudinal axis (16) of a combustion device with respect to the first premixed fuel supply devices (11). The first zones (14) are disposed at the upstream of the second premixed fuel supply devices (12) with respect to the longitudinal axis of the combustion device.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_JP2012068015A
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 COMBUSTION CHAMBER, AND METHOD OF OPERATING COMBUSTION CHAMBER
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T15%3A59%3A07IST&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=EROGLU%20ADNAN&rft.date=2012-04-05&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJP2012068015A%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