METHOD AND APPARATUS TO IMPROVE HEAT TRANSFER IN TURBINE SECTION OF GAS TURBINE

PROBLEM TO BE SOLVED: To provide a gas turbine engine system having a combustion section and a turbine section.SOLUTION: A turbine section includes a turbine stage having a plurality of turbine blades coupled to a rotor, and an inner casing circumferentially disposed about the plurality of turbine b...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: OZGUR BOZKURT, BALLARD JR HENRY GRADY, BLACK KENNETH DAMON, RADU IOAN DANESCU
Format: Patent
Sprache:eng
Schlagworte:
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 OZGUR BOZKURT
BALLARD JR HENRY GRADY
BLACK KENNETH DAMON
RADU IOAN DANESCU
description PROBLEM TO BE SOLVED: To provide a gas turbine engine system having a combustion section and a turbine section.SOLUTION: A turbine section includes a turbine stage having a plurality of turbine blades coupled to a rotor, and an inner casing circumferentially disposed about the plurality of turbine blades. The turbine section includes an outer casing circumferentially disposed about the inner casing. The inner casing and the outer casing define a cavity comprising a volume configured to facilitate the distribution of air within the cavity to cool an outer surface of the inner casing and an inner surface of the outer casing. The outer casing comprises an air inlet, and the inner casing comprises an air outlet. A flange is provided within the cavity, and the flange flanks the air inlet and a flow guide.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2014181702A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2014181702A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2014181702A3</originalsourceid><addsrcrecordid>eNqNirEKwjAQQLN0EOs_HO5CUwW7nvViIjQXkqtrKRIn0UL9f3TQ3eHx4PEWijsSy0dA_yEEjCh9AmFwXYh8IbCEAhLRJ0MRnAfp48F5gkStOPbABk6YfrlUxW28z3n19VKtDUlrN3l6Dnmexmt-5NdwDnWld7rR-6rG7V_TG4mdLv0</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD AND APPARATUS TO IMPROVE HEAT TRANSFER IN TURBINE SECTION OF GAS TURBINE</title><source>esp@cenet</source><creator>OZGUR BOZKURT ; BALLARD JR HENRY GRADY ; BLACK KENNETH DAMON ; RADU IOAN DANESCU</creator><creatorcontrib>OZGUR BOZKURT ; BALLARD JR HENRY GRADY ; BLACK KENNETH DAMON ; RADU IOAN DANESCU</creatorcontrib><description>PROBLEM TO BE SOLVED: To provide a gas turbine engine system having a combustion section and a turbine section.SOLUTION: A turbine section includes a turbine stage having a plurality of turbine blades coupled to a rotor, and an inner casing circumferentially disposed about the plurality of turbine blades. The turbine section includes an outer casing circumferentially disposed about the inner casing. The inner casing and the outer casing define a cavity comprising a volume configured to facilitate the distribution of air within the cavity to cool an outer surface of the inner casing and an inner surface of the outer casing. The outer casing comprises an air inlet, and the inner casing comprises an air outlet. A flange is provided within the cavity, and the flange flanks the air inlet and a flow guide.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2014</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=20140929&amp;DB=EPODOC&amp;CC=JP&amp;NR=2014181702A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25551,76302</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20140929&amp;DB=EPODOC&amp;CC=JP&amp;NR=2014181702A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>OZGUR BOZKURT</creatorcontrib><creatorcontrib>BALLARD JR HENRY GRADY</creatorcontrib><creatorcontrib>BLACK KENNETH DAMON</creatorcontrib><creatorcontrib>RADU IOAN DANESCU</creatorcontrib><title>METHOD AND APPARATUS TO IMPROVE HEAT TRANSFER IN TURBINE SECTION OF GAS TURBINE</title><description>PROBLEM TO BE SOLVED: To provide a gas turbine engine system having a combustion section and a turbine section.SOLUTION: A turbine section includes a turbine stage having a plurality of turbine blades coupled to a rotor, and an inner casing circumferentially disposed about the plurality of turbine blades. The turbine section includes an outer casing circumferentially disposed about the inner casing. The inner casing and the outer casing define a cavity comprising a volume configured to facilitate the distribution of air within the cavity to cool an outer surface of the inner casing and an inner surface of the outer casing. The outer casing comprises an air inlet, and the inner casing comprises an air outlet. A flange is provided within the cavity, and the flange flanks the air inlet and a flow guide.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNirEKwjAQQLN0EOs_HO5CUwW7nvViIjQXkqtrKRIn0UL9f3TQ3eHx4PEWijsSy0dA_yEEjCh9AmFwXYh8IbCEAhLRJ0MRnAfp48F5gkStOPbABk6YfrlUxW28z3n19VKtDUlrN3l6Dnmexmt-5NdwDnWld7rR-6rG7V_TG4mdLv0</recordid><startdate>20140929</startdate><enddate>20140929</enddate><creator>OZGUR BOZKURT</creator><creator>BALLARD JR HENRY GRADY</creator><creator>BLACK KENNETH DAMON</creator><creator>RADU IOAN DANESCU</creator><scope>EVB</scope></search><sort><creationdate>20140929</creationdate><title>METHOD AND APPARATUS TO IMPROVE HEAT TRANSFER IN TURBINE SECTION OF GAS TURBINE</title><author>OZGUR BOZKURT ; BALLARD JR HENRY GRADY ; BLACK KENNETH DAMON ; RADU IOAN DANESCU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2014181702A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2014</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>OZGUR BOZKURT</creatorcontrib><creatorcontrib>BALLARD JR HENRY GRADY</creatorcontrib><creatorcontrib>BLACK KENNETH DAMON</creatorcontrib><creatorcontrib>RADU IOAN DANESCU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>OZGUR BOZKURT</au><au>BALLARD JR HENRY GRADY</au><au>BLACK KENNETH DAMON</au><au>RADU IOAN DANESCU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD AND APPARATUS TO IMPROVE HEAT TRANSFER IN TURBINE SECTION OF GAS TURBINE</title><date>2014-09-29</date><risdate>2014</risdate><abstract>PROBLEM TO BE SOLVED: To provide a gas turbine engine system having a combustion section and a turbine section.SOLUTION: A turbine section includes a turbine stage having a plurality of turbine blades coupled to a rotor, and an inner casing circumferentially disposed about the plurality of turbine blades. The turbine section includes an outer casing circumferentially disposed about the inner casing. The inner casing and the outer casing define a cavity comprising a volume configured to facilitate the distribution of air within the cavity to cool an outer surface of the inner casing and an inner surface of the outer casing. The outer casing comprises an air inlet, and the inner casing comprises an air outlet. A flange is provided within the cavity, and the flange flanks the air inlet and a flow guide.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_JP2014181702A
source esp@cenet
subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title METHOD AND APPARATUS TO IMPROVE HEAT TRANSFER IN TURBINE SECTION OF GAS TURBINE
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T01%3A38%3A47IST&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=OZGUR%20BOZKURT&rft.date=2014-09-29&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJP2014181702A%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