COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME
A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structur...
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| creator | GARDNER DONALD LEE THOMPSON JAMES EDWARD PATTERSON DAVID BRUCE WIEHE GLENN EDWARD YOUNG CRAIG DOUGLAS BROWN DANIEL DALE CORSMEIER DONALD MICHAEL |
| description | A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure. |
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The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBINED OPERATIONS ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINE TOOLS ; MECHANICAL ENGINEERING ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; OTHER WORKING OF METAL ; PERFORMING OPERATIONS ; TRANSPORTING ; UNIVERSAL MACHINE TOOLS ; WEAPONS</subject><creationdate>2013</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=20130404&DB=EPODOC&CC=US&NR=2013081270A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130404&DB=EPODOC&CC=US&NR=2013081270A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GARDNER DONALD LEE</creatorcontrib><creatorcontrib>THOMPSON JAMES EDWARD</creatorcontrib><creatorcontrib>PATTERSON DAVID BRUCE</creatorcontrib><creatorcontrib>WIEHE GLENN EDWARD</creatorcontrib><creatorcontrib>YOUNG CRAIG DOUGLAS</creatorcontrib><creatorcontrib>BROWN DANIEL DALE</creatorcontrib><creatorcontrib>CORSMEIER DONALD MICHAEL</creatorcontrib><title>COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME</title><description>A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBINED OPERATIONS</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINE TOOLS</subject><subject>MECHANICAL ENGINEERING</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>OTHER WORKING OF METAL</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>UNIVERSAL MACHINE TOOLS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB29vd1Cg0O8fT3UwiODA5x9VVw9HNR8HUN8fB3UfB3U3AMDnb1dfLx9HNXCPFwVQh29HXlYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXxocFGBobGBhaGRuYGjobGxKkCADRdJ9s</recordid><startdate>20130404</startdate><enddate>20130404</enddate><creator>GARDNER DONALD LEE</creator><creator>THOMPSON JAMES EDWARD</creator><creator>PATTERSON DAVID BRUCE</creator><creator>WIEHE GLENN EDWARD</creator><creator>YOUNG CRAIG DOUGLAS</creator><creator>BROWN DANIEL DALE</creator><creator>CORSMEIER DONALD MICHAEL</creator><scope>EVB</scope></search><sort><creationdate>20130404</creationdate><title>COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME</title><author>GARDNER DONALD LEE ; THOMPSON JAMES EDWARD ; PATTERSON DAVID BRUCE ; WIEHE GLENN EDWARD ; YOUNG CRAIG DOUGLAS ; BROWN DANIEL DALE ; CORSMEIER DONALD MICHAEL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2013081270A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2013</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBINED OPERATIONS</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINE TOOLS</topic><topic>MECHANICAL ENGINEERING</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>OTHER WORKING OF METAL</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>UNIVERSAL MACHINE TOOLS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GARDNER DONALD LEE</creatorcontrib><creatorcontrib>THOMPSON JAMES EDWARD</creatorcontrib><creatorcontrib>PATTERSON DAVID BRUCE</creatorcontrib><creatorcontrib>WIEHE GLENN EDWARD</creatorcontrib><creatorcontrib>YOUNG CRAIG DOUGLAS</creatorcontrib><creatorcontrib>BROWN DANIEL DALE</creatorcontrib><creatorcontrib>CORSMEIER DONALD MICHAEL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GARDNER DONALD LEE</au><au>THOMPSON JAMES EDWARD</au><au>PATTERSON DAVID BRUCE</au><au>WIEHE GLENN EDWARD</au><au>YOUNG CRAIG DOUGLAS</au><au>BROWN DANIEL DALE</au><au>CORSMEIER DONALD MICHAEL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME</title><date>2013-04-04</date><risdate>2013</risdate><abstract>A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBINED OPERATIONS COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINE TOOLS MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PERFORMING OPERATIONS TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS |
| title | COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME |
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