Method of instrumenting a component
A method of instrumenting a first component ( 210 ) for use in a combustion turbine engine ( 10 ) wherein the first component ( 210 ) has a surface contacted by a second component during operation of the combustion turbine engine ( 10 ). The method may include depositing an insulating layer ( 260 )...
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creator | SUBRAMANIAN RAMESH SABOL STEPHEN M |
description | A method of instrumenting a first component ( 210 ) for use in a combustion turbine engine ( 10 ) wherein the first component ( 210 ) has a surface contacted by a second component during operation of the combustion turbine engine ( 10 ). The method may include depositing an insulating layer ( 260 ) on the surface of the first component ( 210 ) and depositing a first conductive lead ( 232, 254 ) on the insulating layer ( 260 ). A piezoelectric material ( 230 ) may be deposited in electrical communication with the first conductive lead ( 232, 254 ) and a second conductive lead ( 236, 256 ) may be deposited in electrical communication with the piezoelectric material ( 230 ) and be insulated from the first conductive lead ( 232, 254 ) to form a sensor ( 50 ) for detecting pressure exerted on the surface of the first component ( 210 ) during operation of the combustion turbine engine ( 10 ). |
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The method may include depositing an insulating layer ( 260 ) on the surface of the first component ( 210 ) and depositing a first conductive lead ( 232, 254 ) on the insulating layer ( 260 ). A piezoelectric material ( 230 ) may be deposited in electrical communication with the first conductive lead ( 232, 254 ) and a second conductive lead ( 236, 256 ) may be deposited in electrical communication with the piezoelectric material ( 230 ) and be insulated from the first conductive lead ( 232, 254 ) to form a sensor ( 50 ) for detecting pressure exerted on the surface of the first component ( 210 ) during operation of the combustion turbine engine ( 10 ).</description><edition>7</edition><language>eng</language><subject>BLASTING ; ELECTRICITY ; ENGINE PLANTS IN GENERAL ; HEATING ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2005</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=20051229&DB=EPODOC&CC=US&NR=2005287386A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20051229&DB=EPODOC&CC=US&NR=2005287386A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SUBRAMANIAN RAMESH</creatorcontrib><creatorcontrib>SABOL STEPHEN M</creatorcontrib><title>Method of instrumenting a component</title><description>A method of instrumenting a first component ( 210 ) for use in a combustion turbine engine ( 10 ) wherein the first component ( 210 ) has a surface contacted by a second component during operation of the combustion turbine engine ( 10 ). The method may include depositing an insulating layer ( 260 ) on the surface of the first component ( 210 ) and depositing a first conductive lead ( 232, 254 ) on the insulating layer ( 260 ). A piezoelectric material ( 230 ) may be deposited in electrical communication with the first conductive lead ( 232, 254 ) and a second conductive lead ( 236, 256 ) may be deposited in electrical communication with the piezoelectric material ( 230 ) and be insulated from the first conductive lead ( 232, 254 ) to form a sensor ( 50 ) for detecting pressure exerted on the surface of the first component ( 210 ) during operation of the combustion turbine engine ( 10 ).</description><subject>BLASTING</subject><subject>ELECTRICITY</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LAYERED PRODUCTS</subject><subject>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</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>PERFORMING OPERATIONS</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2005</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFD2TS3JyE9RyE9TyMwrLikqzU3NK8nMS1dIVEjOzy3IzwNyeRhY0xJzilN5oTQ3g7Kba4izh25qQX58anFBYnJqXmpJfGiwkYGBqZGFubGFmaOhMXGqAIoeJ5E</recordid><startdate>20051229</startdate><enddate>20051229</enddate><creator>SUBRAMANIAN RAMESH</creator><creator>SABOL STEPHEN M</creator><scope>EVB</scope></search><sort><creationdate>20051229</creationdate><title>Method of instrumenting a component</title><author>SUBRAMANIAN RAMESH ; SABOL STEPHEN M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2005287386A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2005</creationdate><topic>BLASTING</topic><topic>ELECTRICITY</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LAYERED PRODUCTS</topic><topic>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</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>PERFORMING OPERATIONS</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>SUBRAMANIAN RAMESH</creatorcontrib><creatorcontrib>SABOL STEPHEN M</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SUBRAMANIAN RAMESH</au><au>SABOL STEPHEN M</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method of instrumenting a component</title><date>2005-12-29</date><risdate>2005</risdate><abstract>A method of instrumenting a first component ( 210 ) for use in a combustion turbine engine ( 10 ) wherein the first component ( 210 ) has a surface contacted by a second component during operation of the combustion turbine engine ( 10 ). The method may include depositing an insulating layer ( 260 ) on the surface of the first component ( 210 ) and depositing a first conductive lead ( 232, 254 ) on the insulating layer ( 260 ). A piezoelectric material ( 230 ) may be deposited in electrical communication with the first conductive lead ( 232, 254 ) and a second conductive lead ( 236, 256 ) may be deposited in electrical communication with the piezoelectric material ( 230 ) and be insulated from the first conductive lead ( 232, 254 ) to form a sensor ( 50 ) for detecting pressure exerted on the surface of the first component ( 210 ) during operation of the combustion turbine engine ( 10 ).</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING ELECTRICITY ENGINE PLANTS IN GENERAL HEATING LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS |
title | Method of instrumenting a component |
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