ELECTRICAL POWER RETURN DEVICE FOR AVIONICS EQUIPMENT
The invention involves an electrical power supply return device for onboard avionic devices (1a, 1b) arranged on an aircraft's conducting composite structure, comprising at least one conducting metal bar (3) solidly fixed to the conducting composite structure using insulated fixings (4), the ba...
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| creator | MONTEGUT, FRANCOIS BERRADA, HICHAM |
| description | The invention involves an electrical power supply return device for onboard avionic devices (1a, 1b) arranged on an aircraft's conducting composite structure, comprising at least one conducting metal bar (3) solidly fixed to the conducting composite structure using insulated fixings (4), the bar (3) comprising at least one electrical connection component (5a, 5b) for at least one of the said onboard devices (1a, 1b) and an electrical connection element (6) to a primary electrical structure (7) of the said aircraft.
L'objet de l'invention est un dispositif de retour d'alimentation électrique pour dispositifs embarqués avioniques (1a, 1b) disposés sur une structure composite conductrice (2) d'un aéronef, comportant au moins une barre métallique conductrice (3) solidarisée à la structure composite conductrice au travers de moyens de fixation isolants (4), la barre (3) comportant d'une part au moins un organe de raccordement électrique (5a, 5b) pour au moins un desdits dispositifs embarqués (1a, 1b) et, d'autre part, un élément de raccordement électrique (6) à une structure électrique primaire (7) dudit aéronef. |
| format | Patent |
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L'objet de l'invention est un dispositif de retour d'alimentation électrique pour dispositifs embarqués avioniques (1a, 1b) disposés sur une structure composite conductrice (2) d'un aéronef, comportant au moins une barre métallique conductrice (3) solidarisée à la structure composite conductrice au travers de moyens de fixation isolants (4), la barre (3) comportant d'une part au moins un organe de raccordement électrique (5a, 5b) pour au moins un desdits dispositifs embarqués (1a, 1b) et, d'autre part, un élément de raccordement électrique (6) à une structure électrique primaire (7) dudit aéronef.</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BASIC ELECTRIC ELEMENTS ; COSMONAUTICS ; CURRENT COLLECTORS ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; LINE CONNECTORS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</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=20121218&DB=EPODOC&CC=CA&NR=2495987C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20121218&DB=EPODOC&CC=CA&NR=2495987C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MONTEGUT, FRANCOIS</creatorcontrib><creatorcontrib>BERRADA, HICHAM</creatorcontrib><title>ELECTRICAL POWER RETURN DEVICE FOR AVIONICS EQUIPMENT</title><description>The invention involves an electrical power supply return device for onboard avionic devices (1a, 1b) arranged on an aircraft's conducting composite structure, comprising at least one conducting metal bar (3) solidly fixed to the conducting composite structure using insulated fixings (4), the bar (3) comprising at least one electrical connection component (5a, 5b) for at least one of the said onboard devices (1a, 1b) and an electrical connection element (6) to a primary electrical structure (7) of the said aircraft.
L'objet de l'invention est un dispositif de retour d'alimentation électrique pour dispositifs embarqués avioniques (1a, 1b) disposés sur une structure composite conductrice (2) d'un aéronef, comportant au moins une barre métallique conductrice (3) solidarisée à la structure composite conductrice au travers de moyens de fixation isolants (4), la barre (3) comportant d'une part au moins un organe de raccordement électrique (5a, 5b) pour au moins un desdits dispositifs embarqués (1a, 1b) et, d'autre part, un élément de raccordement électrique (6) à une structure électrique primaire (7) dudit aéronef.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>COSMONAUTICS</subject><subject>CURRENT COLLECTORS</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>LINE CONNECTORS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB19XF1DgnydHb0UQjwD3cNUghyDQkN8lNwcQ3zdHZVcPMPUnAM8_T383QOVnANDPUM8HX1C-FhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfHOjkYmlqaWFubOxoRVAABlzCcK</recordid><startdate>20121218</startdate><enddate>20121218</enddate><creator>MONTEGUT, FRANCOIS</creator><creator>BERRADA, HICHAM</creator><scope>EVB</scope></search><sort><creationdate>20121218</creationdate><title>ELECTRICAL POWER RETURN DEVICE FOR AVIONICS EQUIPMENT</title><author>MONTEGUT, FRANCOIS ; BERRADA, HICHAM</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2495987C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2012</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>COSMONAUTICS</topic><topic>CURRENT COLLECTORS</topic><topic>ELECTRICITY</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>LINE CONNECTORS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>MONTEGUT, FRANCOIS</creatorcontrib><creatorcontrib>BERRADA, HICHAM</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MONTEGUT, FRANCOIS</au><au>BERRADA, HICHAM</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ELECTRICAL POWER RETURN DEVICE FOR AVIONICS EQUIPMENT</title><date>2012-12-18</date><risdate>2012</risdate><abstract>The invention involves an electrical power supply return device for onboard avionic devices (1a, 1b) arranged on an aircraft's conducting composite structure, comprising at least one conducting metal bar (3) solidly fixed to the conducting composite structure using insulated fixings (4), the bar (3) comprising at least one electrical connection component (5a, 5b) for at least one of the said onboard devices (1a, 1b) and an electrical connection element (6) to a primary electrical structure (7) of the said aircraft.
L'objet de l'invention est un dispositif de retour d'alimentation électrique pour dispositifs embarqués avioniques (1a, 1b) disposés sur une structure composite conductrice (2) d'un aéronef, comportant au moins une barre métallique conductrice (3) solidarisée à la structure composite conductrice au travers de moyens de fixation isolants (4), la barre (3) comportant d'une part au moins un organe de raccordement électrique (5a, 5b) pour au moins un desdits dispositifs embarqués (1a, 1b) et, d'autre part, un élément de raccordement électrique (6) à une structure électrique primaire (7) dudit aéronef.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS CURRENT COLLECTORS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS LINE CONNECTORS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | ELECTRICAL POWER RETURN DEVICE FOR AVIONICS EQUIPMENT |
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