Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system

An attachment system for attaching at least one exhaust diffuser downstream from a turbine assembly in a gas turbine engine is disclosed. The attachment system may include at least one attachment flange extending from a downstream edge and attached to a spring plate diffuser support structure and at...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Graber Daryl J, Finneran John W, Leagon Jonathan M, Porter Matthew R, Munshi Mrinal, Shteyman Yevgeniy
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 Graber Daryl J
Finneran John W
Leagon Jonathan M
Porter Matthew R
Munshi Mrinal
Shteyman Yevgeniy
description An attachment system for attaching at least one exhaust diffuser downstream from a turbine assembly in a gas turbine engine is disclosed. The attachment system may include at least one attachment flange extending from a downstream edge and attached to a spring plate diffuser support structure and at least one attachment flange extending from side edges of the exhaust diffuser to couple sections of the exhaust diffuser together. The diffuser may also include a thermal barrier/cooling system for controlling a temperature of an outer case of the gas turbine engine. The thermal barrier/cooling system may form a flow path for an ambient air flow cooling.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US9664062B2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US9664062B2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US9664062B23</originalsourceid><addsrcrecordid>eNqNjE0KwjAQRrtxIeod5gKCVCm4VfzZq-syrdN2JJmEZoJ6Aq9tSj2Aqwcf73vT7HPCABr7ioWApB3wZO3ARqPsDUHtrHdCokCvDmNQuHPTxEA9OE89KksLLMmTR5Ra2clYQAEXNWk1BgK0FY-RNAma5DszXMM7KNl5NmnQBFr8OMvgeLjuz0vyrqTgsSYhLW-XbVFsVkW-y9d_KF-WEEzU</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system</title><source>esp@cenet</source><creator>Graber Daryl J ; Finneran John W ; Leagon Jonathan M ; Porter Matthew R ; Munshi Mrinal ; Shteyman Yevgeniy</creator><creatorcontrib>Graber Daryl J ; Finneran John W ; Leagon Jonathan M ; Porter Matthew R ; Munshi Mrinal ; Shteyman Yevgeniy</creatorcontrib><description>An attachment system for attaching at least one exhaust diffuser downstream from a turbine assembly in a gas turbine engine is disclosed. The attachment system may include at least one attachment flange extending from a downstream edge and attached to a spring plate diffuser support structure and at least one attachment flange extending from side edges of the exhaust diffuser to couple sections of the exhaust diffuser together. The diffuser may also include a thermal barrier/cooling system for controlling a temperature of an outer case of the gas turbine engine. The thermal barrier/cooling system may form a flow path for an ambient air flow cooling.</description><language>eng</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2017</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=20170530&amp;DB=EPODOC&amp;CC=US&amp;NR=9664062B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20170530&amp;DB=EPODOC&amp;CC=US&amp;NR=9664062B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Graber Daryl J</creatorcontrib><creatorcontrib>Finneran John W</creatorcontrib><creatorcontrib>Leagon Jonathan M</creatorcontrib><creatorcontrib>Porter Matthew R</creatorcontrib><creatorcontrib>Munshi Mrinal</creatorcontrib><creatorcontrib>Shteyman Yevgeniy</creatorcontrib><title>Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system</title><description>An attachment system for attaching at least one exhaust diffuser downstream from a turbine assembly in a gas turbine engine is disclosed. The attachment system may include at least one attachment flange extending from a downstream edge and attached to a spring plate diffuser support structure and at least one attachment flange extending from side edges of the exhaust diffuser to couple sections of the exhaust diffuser together. The diffuser may also include a thermal barrier/cooling system for controlling a temperature of an outer case of the gas turbine engine. The thermal barrier/cooling system may form a flow path for an ambient air flow cooling.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</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>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjE0KwjAQRrtxIeod5gKCVCm4VfzZq-syrdN2JJmEZoJ6Aq9tSj2Aqwcf73vT7HPCABr7ioWApB3wZO3ARqPsDUHtrHdCokCvDmNQuHPTxEA9OE89KksLLMmTR5Ra2clYQAEXNWk1BgK0FY-RNAma5DszXMM7KNl5NmnQBFr8OMvgeLjuz0vyrqTgsSYhLW-XbVFsVkW-y9d_KF-WEEzU</recordid><startdate>20170530</startdate><enddate>20170530</enddate><creator>Graber Daryl J</creator><creator>Finneran John W</creator><creator>Leagon Jonathan M</creator><creator>Porter Matthew R</creator><creator>Munshi Mrinal</creator><creator>Shteyman Yevgeniy</creator><scope>EVB</scope></search><sort><creationdate>20170530</creationdate><title>Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system</title><author>Graber Daryl J ; Finneran John W ; Leagon Jonathan M ; Porter Matthew R ; Munshi Mrinal ; Shteyman Yevgeniy</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US9664062B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2017</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</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>Graber Daryl J</creatorcontrib><creatorcontrib>Finneran John W</creatorcontrib><creatorcontrib>Leagon Jonathan M</creatorcontrib><creatorcontrib>Porter Matthew R</creatorcontrib><creatorcontrib>Munshi Mrinal</creatorcontrib><creatorcontrib>Shteyman Yevgeniy</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Graber Daryl J</au><au>Finneran John W</au><au>Leagon Jonathan M</au><au>Porter Matthew R</au><au>Munshi Mrinal</au><au>Shteyman Yevgeniy</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system</title><date>2017-05-30</date><risdate>2017</risdate><abstract>An attachment system for attaching at least one exhaust diffuser downstream from a turbine assembly in a gas turbine engine is disclosed. The attachment system may include at least one attachment flange extending from a downstream edge and attached to a spring plate diffuser support structure and at least one attachment flange extending from side edges of the exhaust diffuser to couple sections of the exhaust diffuser together. The diffuser may also include a thermal barrier/cooling system for controlling a temperature of an outer case of the gas turbine engine. The thermal barrier/cooling system may form a flow path for an ambient air flow cooling.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US9664062B2
source esp@cenet
subjects BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-26T17%3A44%3A34IST&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=Graber%20Daryl%20J&rft.date=2017-05-30&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS9664062B2%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