GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION AND CORRESPONDING METHOD
A gas turbine engine (20) includes a compressor (24), a combustor (56) fluidly connected to the compressor (24) via a primary flowpath (C), a turbine (28) fluidly connected to the combustor (56) via the primary flowpath (C), an engine controller (160) communicatively coupled to at least one sensor (...
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| creator | FEULNER, Matthew R |
| description | A gas turbine engine (20) includes a compressor (24), a combustor (56) fluidly connected to the compressor (24) via a primary flowpath (C), a turbine (28) fluidly connected to the combustor (56) via the primary flowpath (C), an engine controller (160) communicatively coupled to at least one sensor (70) in the gas turbine engine (20), the controller (160) including a non-transitory memory and a processor, and the at least one sensor (70) including an inlet temperature and/or pressure sensor, wherein the sensor (70) is disposed aft of a fan (130). |
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fre ; ger</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 ; MEASURING QUANTITY OF HEAT ; MEASURING TEMPERATURE ; MECHANICAL ENGINEERING ; PHYSICS ; TESTING ; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR ; WEAPONS</subject><creationdate>2020</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=20201223&DB=EPODOC&CC=EP&NR=3249199B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201223&DB=EPODOC&CC=EP&NR=3249199B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FEULNER, Matthew R</creatorcontrib><title>GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION AND CORRESPONDING METHOD</title><description>A gas turbine engine (20) includes a compressor (24), a combustor (56) fluidly connected to the compressor (24) via a primary flowpath (C), a turbine (28) fluidly connected to the combustor (56) via the primary flowpath (C), an engine controller (160) communicatively coupled to at least one sensor (70) in the gas turbine engine (20), the controller (160) including a non-transitory memory and a processor, and the at least one sensor (70) including an inlet temperature and/or pressure sensor, wherein the sensor (70) is disposed aft of a fan (130).</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>MEASURING QUANTITY OF HEAT</subject><subject>MEASURING TEMPERATURE</subject><subject>MECHANICAL ENGINEERING</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNikEKwjAQAHPxIOof9gMear3kmDbbNGA3YbM9l1LiSbRQ_48RfICngZnZK3YmgYzceEJAcl94uqGA4BCRTWkICSkFhjZQ591YpA8EhmwxzJhiIOvJwYDSB3tUu_v82PLpx4OCDqXtz3l9TXlb5yU_83vCWF-uutK6qeo_lg-e2i-k</recordid><startdate>20201223</startdate><enddate>20201223</enddate><creator>FEULNER, Matthew R</creator><scope>EVB</scope></search><sort><creationdate>20201223</creationdate><title>GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION AND CORRESPONDING METHOD</title><author>FEULNER, Matthew R</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3249199B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; 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| language | eng ; fre ; ger |
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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 MEASURING QUANTITY OF HEAT MEASURING TEMPERATURE MECHANICAL ENGINEERING PHYSICS TESTING THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR WEAPONS |
| title | GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION AND CORRESPONDING METHOD |
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