GAS TURBINE OPTICAL IMAGING SYSTEM
A method and system for recreating a two-dimensional distribution of temperatures in an exhaust plane of a gas turbine engine. Light transmission and detection pairs may be arranged in the annulus of the exhaust of the turbine engine in such a way that the individual rays form a two-dimensional mesh...
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| creator | BASU SAMIT KUMAR HINCKLEY KEVIN MICHAEL YARAM VIJAY KUMAR CHEN WEIGUO WOODMANSEE MARK ALLEN GU YIKANG |
| description | A method and system for recreating a two-dimensional distribution of temperatures in an exhaust plane of a gas turbine engine. Light transmission and detection pairs may be arranged in the annulus of the exhaust of the turbine engine in such a way that the individual rays form a two-dimensional mesh of beams across a sector of the exhaust. Based on the absorption of the rays, the temperature of the sector of the exhaust through which the ray passes may be determined. Based on these determinations, an image that corresponds to the operation of the turbine engine may be generated. |
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Light transmission and detection pairs may be arranged in the annulus of the exhaust of the turbine engine in such a way that the individual rays form a two-dimensional mesh of beams across a sector of the exhaust. Based on the absorption of the rays, the temperature of the sector of the exhaust through which the ray passes may be determined. Based on these determinations, an image that corresponds to the operation of the turbine engine may be generated.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MEASURING ; MECHANICAL ENGINEERING ; PHYSICS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR ; WEAPONS</subject><creationdate>2010</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=20101028&DB=EPODOC&CC=US&NR=2010272557A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20101028&DB=EPODOC&CC=US&NR=2010272557A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BASU SAMIT KUMAR</creatorcontrib><creatorcontrib>HINCKLEY KEVIN MICHAEL</creatorcontrib><creatorcontrib>YARAM VIJAY KUMAR</creatorcontrib><creatorcontrib>CHEN WEIGUO</creatorcontrib><creatorcontrib>WOODMANSEE MARK ALLEN</creatorcontrib><creatorcontrib>GU YIKANG</creatorcontrib><title>GAS TURBINE OPTICAL IMAGING SYSTEM</title><description>A method and system for recreating a two-dimensional distribution of temperatures in an exhaust plane of a gas turbine engine. 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Based on these determinations, an image that corresponds to the operation of the turbine engine may be generated.</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>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MEASURING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</subject><subject>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2010</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBydwxWCAkNcvL0c1XwDwjxdHb0UfD0dXT39HNXCI4MDnH15WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgaGBkbmRqam5o6GxsSpAgC-1iNc</recordid><startdate>20101028</startdate><enddate>20101028</enddate><creator>BASU SAMIT KUMAR</creator><creator>HINCKLEY KEVIN MICHAEL</creator><creator>YARAM VIJAY KUMAR</creator><creator>CHEN WEIGUO</creator><creator>WOODMANSEE MARK ALLEN</creator><creator>GU YIKANG</creator><scope>EVB</scope></search><sort><creationdate>20101028</creationdate><title>GAS TURBINE OPTICAL IMAGING SYSTEM</title><author>BASU SAMIT KUMAR ; HINCKLEY KEVIN MICHAEL ; YARAM VIJAY KUMAR ; CHEN WEIGUO ; WOODMANSEE MARK ALLEN ; GU YIKANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2010272557A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2010</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>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MEASURING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</topic><topic>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BASU SAMIT KUMAR</creatorcontrib><creatorcontrib>HINCKLEY KEVIN MICHAEL</creatorcontrib><creatorcontrib>YARAM VIJAY KUMAR</creatorcontrib><creatorcontrib>CHEN WEIGUO</creatorcontrib><creatorcontrib>WOODMANSEE MARK ALLEN</creatorcontrib><creatorcontrib>GU YIKANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BASU SAMIT KUMAR</au><au>HINCKLEY KEVIN MICHAEL</au><au>YARAM VIJAY KUMAR</au><au>CHEN WEIGUO</au><au>WOODMANSEE MARK ALLEN</au><au>GU YIKANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE OPTICAL IMAGING SYSTEM</title><date>2010-10-28</date><risdate>2010</risdate><abstract>A method and system for recreating a two-dimensional distribution of temperatures in an exhaust plane of a gas turbine engine. Light transmission and detection pairs may be arranged in the annulus of the exhaust of the turbine engine in such a way that the individual rays form a two-dimensional mesh of beams across a sector of the exhaust. Based on the absorption of the rays, the temperature of the sector of the exhaust through which the ray passes may be determined. Based on these determinations, an image that corresponds to the operation of the turbine engine may be generated.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MEASURING MECHANICAL ENGINEERING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS |
| title | GAS TURBINE OPTICAL IMAGING SYSTEM |
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