Current retour network element for aircraft
The element (1) has a set of electrically conducting strips (2) formed from a single piece and separated from each other so as to form a set of openings (4) between the strips. The strips are intersected in a perpendicular manner to form a mesh, where intersections of the strips form a mesh node. Th...
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creator | Charon, Pierre Gallant, Guillaume |
description | The element (1) has a set of electrically conducting strips (2) formed from a single piece and separated from each other so as to form a set of openings (4) between the strips. The strips are intersected in a perpendicular manner to form a mesh, where intersections of the strips form a mesh node. Thickness of the strips ranges between 1 mm and 5 mm, and is equal to or less than width of the strips, where the network element is supported against an upper surface or lower surface of crosspieces (8). An independent claim is also included for a portion of aircraft, comprising a current return network element. |
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The strips are intersected in a perpendicular manner to form a mesh, where intersections of the strips form a mesh node. Thickness of the strips ranges between 1 mm and 5 mm, and is equal to or less than width of the strips, where the network element is supported against an upper surface or lower surface of crosspieces (8). An independent claim is also included for a portion of aircraft, comprising a current return network element.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BASIC ELECTRIC ELEMENTS ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; CURRENT COLLECTORS ; ELECTRICITY ; GENERATION ; HELICOPTERS ; INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINEDOPTICAL AND ELECTRIC CABLES OR LINES ; LINE CONNECTORS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2017</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=20171122&DB=EPODOC&CC=EP&NR=2218641B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20171122&DB=EPODOC&CC=EP&NR=2218641B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Charon, Pierre</creatorcontrib><creatorcontrib>Gallant, Guillaume</creatorcontrib><title>Current retour network element for aircraft</title><description>The element (1) has a set of electrically conducting strips (2) formed from a single piece and separated from each other so as to form a set of openings (4) between the strips. The strips are intersected in a perpendicular manner to form a mesh, where intersections of the strips form a mesh node. Thickness of the strips ranges between 1 mm and 5 mm, and is equal to or less than width of the strips, where the network element is supported against an upper surface or lower surface of crosspieces (8). An independent claim is also included for a portion of aircraft, comprising a current return network element.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>COSMONAUTICS</subject><subject>CURRENT COLLECTORS</subject><subject>ELECTRICITY</subject><subject>GENERATION</subject><subject>HELICOPTERS</subject><subject>INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINEDOPTICAL AND ELECTRIC CABLES OR LINES</subject><subject>LINE CONNECTORS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB2Li0qSs0rUShKLckvLVLISy0pzy_KVkjNSc0FCaflFykkZhYlFyWmlfAwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTkVKD2eNcAIyNDCzMTQydDYyKUAAA5rClX</recordid><startdate>20171122</startdate><enddate>20171122</enddate><creator>Charon, Pierre</creator><creator>Gallant, Guillaume</creator><scope>EVB</scope></search><sort><creationdate>20171122</creationdate><title>Current retour network element for aircraft</title><author>Charon, Pierre ; Gallant, Guillaume</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2218641B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>COSMONAUTICS</topic><topic>CURRENT COLLECTORS</topic><topic>ELECTRICITY</topic><topic>GENERATION</topic><topic>HELICOPTERS</topic><topic>INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINEDOPTICAL AND ELECTRIC CABLES OR LINES</topic><topic>LINE CONNECTORS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Charon, Pierre</creatorcontrib><creatorcontrib>Gallant, Guillaume</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Charon, Pierre</au><au>Gallant, Guillaume</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Current retour network element for aircraft</title><date>2017-11-22</date><risdate>2017</risdate><abstract>The element (1) has a set of electrically conducting strips (2) formed from a single piece and separated from each other so as to form a set of openings (4) between the strips. The strips are intersected in a perpendicular manner to form a mesh, where intersections of the strips form a mesh node. Thickness of the strips ranges between 1 mm and 5 mm, and is equal to or less than width of the strips, where the network element is supported against an upper surface or lower surface of crosspieces (8). An independent claim is also included for a portion of aircraft, comprising a current return network element.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | AEROPLANES AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS CURRENT COLLECTORS ELECTRICITY GENERATION HELICOPTERS INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINEDOPTICAL AND ELECTRIC CABLES OR LINES LINE CONNECTORS PERFORMING OPERATIONS TRANSPORTING |
title | Current retour network element for aircraft |
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