Electromagnetic shielding systems and methods for aircraft
An electromagnetic shielding system is configured to shield one or more electrical connections between one or more first electrical cables and one or more second electrical cables. The electromagnetic shielding system includes a base. A first cable coupler is frangibly coupled to the base. The first...
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | Klein, Steven E Fraser, Jason A Robb, Andrew M Gilbert, Eric B |
description | An electromagnetic shielding system is configured to shield one or more electrical connections between one or more first electrical cables and one or more second electrical cables. The electromagnetic shielding system includes a base. A first cable coupler is frangibly coupled to the base. The first cable coupler is configured to electrically couple to the first electrical cable(s). A second cable coupler is frangibly coupled to the base. The second cable coupler is configured to electrically couple to the second electrical cable(s). A covering lid is frangibly coupled to the first cable coupler, the second cable coupler, and the base. An electrical connection chamber is defined between the base, the first cable coupler, the second cable coupler, and the covering lid. The first electrical cable(s) are configured to electrically connect to the second electrical cable(s) within the electrical connection chamber. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US10826247B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US10826247B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US10826247B13</originalsourceid><addsrcrecordid>eNrjZLByzUlNLinKz01Mz0styUxWKM7ITM1JycxLVyiuLC5JzS1WSMxLUchNLcnITylWSMsvUkjMLEouSkwr4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpQCPjQ4MNDSyMzIxMzJ0MjYlRAwC6Ky-u</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Electromagnetic shielding systems and methods for aircraft</title><source>esp@cenet</source><creator>Klein, Steven E ; Fraser, Jason A ; Robb, Andrew M ; Gilbert, Eric B</creator><creatorcontrib>Klein, Steven E ; Fraser, Jason A ; Robb, Andrew M ; Gilbert, Eric B</creatorcontrib><description>An electromagnetic shielding system is configured to shield one or more electrical connections between one or more first electrical cables and one or more second electrical cables. The electromagnetic shielding system includes a base. A first cable coupler is frangibly coupled to the base. The first cable coupler is configured to electrically couple to the first electrical cable(s). A second cable coupler is frangibly coupled to the base. The second cable coupler is configured to electrically couple to the second electrical cable(s). A covering lid is frangibly coupled to the first cable coupler, the second cable coupler, and the base. An electrical connection chamber is defined between the base, the first cable coupler, the second cable coupler, and the covering lid. The first electrical cable(s) are configured to electrically connect to the second electrical cable(s) within the electrical connection chamber.</description><language>eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BASIC ELECTRIC ELEMENTS ; CABLES ; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ; CONDUCTORS ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; CURRENT COLLECTORS ; ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ; ELECTRICITY ; EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERATION ; INSULATORS ; LINE CONNECTORS ; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS ; PARACHUTES ; PERFORMING OPERATIONS ; PRINTED CIRCUITS ; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES ; TRANSPORTING</subject><creationdate>2020</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=20201103&DB=EPODOC&CC=US&NR=10826247B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201103&DB=EPODOC&CC=US&NR=10826247B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Klein, Steven E</creatorcontrib><creatorcontrib>Fraser, Jason A</creatorcontrib><creatorcontrib>Robb, Andrew M</creatorcontrib><creatorcontrib>Gilbert, Eric B</creatorcontrib><title>Electromagnetic shielding systems and methods for aircraft</title><description>An electromagnetic shielding system is configured to shield one or more electrical connections between one or more first electrical cables and one or more second electrical cables. The electromagnetic shielding system includes a base. A first cable coupler is frangibly coupled to the base. The first cable coupler is configured to electrically couple to the first electrical cable(s). A second cable coupler is frangibly coupled to the base. The second cable coupler is configured to electrically couple to the second electrical cable(s). A covering lid is frangibly coupled to the first cable coupler, the second cable coupler, and the base. An electrical connection chamber is defined between the base, the first cable coupler, the second cable coupler, and the covering lid. The first electrical cable(s) are configured to electrically connect to the second electrical cable(s) within the electrical connection chamber.</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>CABLES</subject><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</subject><subject>CONDUCTORS</subject><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>COSMONAUTICS</subject><subject>CURRENT COLLECTORS</subject><subject>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</subject><subject>ELECTRICITY</subject><subject>EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERATION</subject><subject>INSULATORS</subject><subject>LINE CONNECTORS</subject><subject>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PRINTED CIRCUITS</subject><subject>SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLByzUlNLinKz01Mz0styUxWKM7ITM1JycxLVyiuLC5JzS1WSMxLUchNLcnITylWSMsvUkjMLEouSkwr4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpQCPjQ4MNDSyMzIxMzJ0MjYlRAwC6Ky-u</recordid><startdate>20201103</startdate><enddate>20201103</enddate><creator>Klein, Steven E</creator><creator>Fraser, Jason A</creator><creator>Robb, Andrew M</creator><creator>Gilbert, Eric B</creator><scope>EVB</scope></search><sort><creationdate>20201103</creationdate><title>Electromagnetic shielding systems and methods for aircraft</title><author>Klein, Steven E ; Fraser, Jason A ; Robb, Andrew M ; Gilbert, Eric B</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US10826247B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2020</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>CABLES</topic><topic>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</topic><topic>CONDUCTORS</topic><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>COSMONAUTICS</topic><topic>CURRENT COLLECTORS</topic><topic>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</topic><topic>ELECTRICITY</topic><topic>EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERATION</topic><topic>INSULATORS</topic><topic>LINE CONNECTORS</topic><topic>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PRINTED CIRCUITS</topic><topic>SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Klein, Steven E</creatorcontrib><creatorcontrib>Fraser, Jason A</creatorcontrib><creatorcontrib>Robb, Andrew M</creatorcontrib><creatorcontrib>Gilbert, Eric B</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Klein, Steven E</au><au>Fraser, Jason A</au><au>Robb, Andrew M</au><au>Gilbert, Eric B</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Electromagnetic shielding systems and methods for aircraft</title><date>2020-11-03</date><risdate>2020</risdate><abstract>An electromagnetic shielding system is configured to shield one or more electrical connections between one or more first electrical cables and one or more second electrical cables. The electromagnetic shielding system includes a base. A first cable coupler is frangibly coupled to the base. The first cable coupler is configured to electrically couple to the first electrical cable(s). A second cable coupler is frangibly coupled to the base. The second cable coupler is configured to electrically couple to the second electrical cable(s). A covering lid is frangibly coupled to the first cable coupler, the second cable coupler, and the base. An electrical connection chamber is defined between the base, the first cable coupler, the second cable coupler, and the covering lid. The first electrical cable(s) are configured to electrically connect to the second electrical cable(s) within the electrical connection chamber.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_US10826247B1 |
source | esp@cenet |
subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS CABLES CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS CONDUCTORS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS CURRENT COLLECTORS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION INSULATORS LINE CONNECTORS MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PARACHUTES PERFORMING OPERATIONS PRINTED CIRCUITS SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING ORDIELECTRIC PROPERTIES TRANSPORTING |
title | Electromagnetic shielding systems and methods for aircraft |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-20T19%3A16%3A32IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Klein,%20Steven%20E&rft.date=2020-11-03&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS10826247B1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |