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...
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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. |
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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&date=20170530&DB=EPODOC&CC=US&NR=9664062B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170530&DB=EPODOC&CC=US&NR=9664062B2$$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. 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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> |
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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 |
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