Protection method and device of an electrical network for aircraft
A method for protecting a bipolar power distribution network supplied with power by an electric power source isolated from an electrical ground of an aircraft. The network includes a resistive protection device configured to be connected to the electrical ground and to the two phases of the network....
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creator | ALEJO DOMINIQUE PRISSE LUCIEN PAUVERT VINCENT LAM SHANG LEEN LUDOVIC |
description | A method for protecting a bipolar power distribution network supplied with power by an electric power source isolated from an electrical ground of an aircraft. The network includes a resistive protection device configured to be connected to the electrical ground and to the two phases of the network. The method includes the steps of receiving at least one voltage value on at least one of the two phases and/or at least one current value in the electrical ground, comparing the at least one voltage value with a first predetermined threshold value and/or the at least one current value with a second predetermined threshold value and controlling the protection device by changing its resistivity according to the comparison. |
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The network includes a resistive protection device configured to be connected to the electrical ground and to the two phases of the network. The method includes the steps of receiving at least one voltage value on at least one of the two phases and/or at least one current value in the electrical ground, comparing the at least one voltage value with a first predetermined threshold value and/or the at least one current value with a second predetermined threshold value and controlling the protection device by changing its resistivity according to the comparison.</description><language>eng</language><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; ELECTRICITY ; EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS ; GENERATION ; MEASURING ; MEASURING ELECTRIC VARIABLES ; MEASURING MAGNETIC VARIABLES ; PHYSICS ; TESTING</subject><creationdate>2014</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=20140417&DB=EPODOC&CC=US&NR=2014104734A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140417&DB=EPODOC&CC=US&NR=2014104734A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ALEJO DOMINIQUE</creatorcontrib><creatorcontrib>PRISSE LUCIEN</creatorcontrib><creatorcontrib>PAUVERT VINCENT</creatorcontrib><creatorcontrib>LAM SHANG LEEN LUDOVIC</creatorcontrib><title>Protection method and device of an electrical network for aircraft</title><description>A method for protecting a bipolar power distribution network supplied with power by an electric power source isolated from an electrical ground of an aircraft. 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The method includes the steps of receiving at least one voltage value on at least one of the two phases and/or at least one current value in the electrical ground, comparing the at least one voltage value with a first predetermined threshold value and/or the at least one current value with a second predetermined threshold value and controlling the protection device by changing its resistivity according to the comparison.</description><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>ELECTRICITY</subject><subject>EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS</subject><subject>GENERATION</subject><subject>MEASURING</subject><subject>MEASURING ELECTRIC VARIABLES</subject><subject>MEASURING MAGNETIC VARIABLES</subject><subject>PHYSICS</subject><subject>TESTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAKKMovSU0uyczPU8hNLcnIT1FIzEtRSEkty0xOVchPA_IUUnOACooykxNzFPJSS8rzi7IV0vKLFBIzi5KLEtNKeBhY0xJzilN5oTQ3g7Kba4izh25qQX58anFBYnIqUFt8aLCRgaGJoYGJubGJo6ExcaoA-IYy1Q</recordid><startdate>20140417</startdate><enddate>20140417</enddate><creator>ALEJO DOMINIQUE</creator><creator>PRISSE LUCIEN</creator><creator>PAUVERT VINCENT</creator><creator>LAM SHANG LEEN LUDOVIC</creator><scope>EVB</scope></search><sort><creationdate>20140417</creationdate><title>Protection method and device of an electrical network for aircraft</title><author>ALEJO DOMINIQUE ; PRISSE LUCIEN ; PAUVERT VINCENT ; LAM SHANG LEEN LUDOVIC</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2014104734A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2014</creationdate><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>ELECTRICITY</topic><topic>EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS</topic><topic>GENERATION</topic><topic>MEASURING</topic><topic>MEASURING ELECTRIC VARIABLES</topic><topic>MEASURING MAGNETIC VARIABLES</topic><topic>PHYSICS</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ALEJO DOMINIQUE</creatorcontrib><creatorcontrib>PRISSE LUCIEN</creatorcontrib><creatorcontrib>PAUVERT VINCENT</creatorcontrib><creatorcontrib>LAM SHANG LEEN LUDOVIC</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ALEJO DOMINIQUE</au><au>PRISSE LUCIEN</au><au>PAUVERT VINCENT</au><au>LAM SHANG LEEN LUDOVIC</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Protection method and device of an electrical network for aircraft</title><date>2014-04-17</date><risdate>2014</risdate><abstract>A method for protecting a bipolar power distribution network supplied with power by an electric power source isolated from an electrical ground of an aircraft. The network includes a resistive protection device configured to be connected to the electrical ground and to the two phases of the network. The method includes the steps of receiving at least one voltage value on at least one of the two phases and/or at least one current value in the electrical ground, comparing the at least one voltage value with a first predetermined threshold value and/or the at least one current value with a second predetermined threshold value and controlling the protection device by changing its resistivity according to the comparison.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS GENERATION MEASURING MEASURING ELECTRIC VARIABLES MEASURING MAGNETIC VARIABLES PHYSICS TESTING |
title | Protection method and device of an electrical network for aircraft |
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