Communication system for turbine engine
A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wir...
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creator | HART ANDREW CLIFFORD PAK JONG YOUN CUMMINS JOSEF SCOTT SCHLEIF KURT KRAMER BROWN GREGORY QUENTIN CASANOVA FERNANDO JORGE JONES ROBERT DAVID CHOI SEUNG-WOO CARUSO PHILIP MICHAEL FERSLEW MATTHEW RYAN SORANNA FRANCESCO |
description | A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal. |
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INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MEASURING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PHYSICS ; STEAM ENGINES ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR ; WEAPONS</subject><creationdate>2012</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=20120717&DB=EPODOC&CC=US&NR=8220319B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120717&DB=EPODOC&CC=US&NR=8220319B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HART ANDREW CLIFFORD</creatorcontrib><creatorcontrib>PAK JONG YOUN</creatorcontrib><creatorcontrib>CUMMINS JOSEF SCOTT</creatorcontrib><creatorcontrib>SCHLEIF KURT KRAMER</creatorcontrib><creatorcontrib>BROWN GREGORY QUENTIN</creatorcontrib><creatorcontrib>CASANOVA FERNANDO JORGE</creatorcontrib><creatorcontrib>JONES ROBERT DAVID</creatorcontrib><creatorcontrib>CHOI SEUNG-WOO</creatorcontrib><creatorcontrib>CARUSO PHILIP MICHAEL</creatorcontrib><creatorcontrib>FERSLEW MATTHEW RYAN</creatorcontrib><creatorcontrib>SORANNA FRANCESCO</creatorcontrib><title>Communication system for turbine engine</title><description>A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MEASURING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PHYSICS</subject><subject>STEAM ENGINES</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>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB3zs_NLc3LTE4syczPUyiuLC5JzVVIyy9SKCktSsrMS1VIzUsHUjwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JD402MLIyMDY0NLJyJgIJQB_TSgD</recordid><startdate>20120717</startdate><enddate>20120717</enddate><creator>HART ANDREW CLIFFORD</creator><creator>PAK JONG YOUN</creator><creator>CUMMINS JOSEF SCOTT</creator><creator>SCHLEIF KURT KRAMER</creator><creator>BROWN GREGORY QUENTIN</creator><creator>CASANOVA FERNANDO JORGE</creator><creator>JONES ROBERT DAVID</creator><creator>CHOI SEUNG-WOO</creator><creator>CARUSO PHILIP MICHAEL</creator><creator>FERSLEW MATTHEW RYAN</creator><creator>SORANNA FRANCESCO</creator><scope>EVB</scope></search><sort><creationdate>20120717</creationdate><title>Communication system for turbine engine</title><author>HART ANDREW CLIFFORD ; PAK JONG YOUN ; CUMMINS JOSEF SCOTT ; SCHLEIF KURT KRAMER ; BROWN GREGORY QUENTIN ; CASANOVA FERNANDO JORGE ; JONES ROBERT DAVID ; CHOI SEUNG-WOO ; CARUSO PHILIP MICHAEL ; FERSLEW MATTHEW RYAN ; SORANNA FRANCESCO</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US8220319B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2012</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MEASURING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PHYSICS</topic><topic>STEAM ENGINES</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>HART ANDREW CLIFFORD</creatorcontrib><creatorcontrib>PAK JONG YOUN</creatorcontrib><creatorcontrib>CUMMINS JOSEF SCOTT</creatorcontrib><creatorcontrib>SCHLEIF KURT KRAMER</creatorcontrib><creatorcontrib>BROWN GREGORY QUENTIN</creatorcontrib><creatorcontrib>CASANOVA FERNANDO JORGE</creatorcontrib><creatorcontrib>JONES ROBERT DAVID</creatorcontrib><creatorcontrib>CHOI SEUNG-WOO</creatorcontrib><creatorcontrib>CARUSO PHILIP MICHAEL</creatorcontrib><creatorcontrib>FERSLEW MATTHEW RYAN</creatorcontrib><creatorcontrib>SORANNA FRANCESCO</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HART ANDREW CLIFFORD</au><au>PAK JONG YOUN</au><au>CUMMINS JOSEF SCOTT</au><au>SCHLEIF KURT KRAMER</au><au>BROWN GREGORY QUENTIN</au><au>CASANOVA FERNANDO JORGE</au><au>JONES ROBERT DAVID</au><au>CHOI SEUNG-WOO</au><au>CARUSO PHILIP MICHAEL</au><au>FERSLEW MATTHEW RYAN</au><au>SORANNA FRANCESCO</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Communication system for turbine engine</title><date>2012-07-17</date><risdate>2012</risdate><abstract>A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MEASURING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS |
title | Communication system for turbine engine |
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