Method and Apparatus for Providing a Current Return Network in an Aircraft Structure
According to an embodiment a current return network assembly, for an aircraft having a predetermined potential lightning strike zone, is mounted within the predetermined potential lightning strike zone. The current return network assembly includes an electrically conductive honeycomb central core th...
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| creator | DAY ARTHUR C PIEHL MARC J KAJITA KIRK B FOLTZ GREGORY ALAN GREGG PAUL S |
| description | According to an embodiment a current return network assembly, for an aircraft having a predetermined potential lightning strike zone, is mounted within the predetermined potential lightning strike zone. The current return network assembly includes an electrically conductive honeycomb central core that conducts electrical current both through the assembly and through the predetermined potential lightning strike zone. The electrical current is caused by a lightning strike on the aircraft at the predetermined potential lightning strike zone. According to an embodiment, an aircraft has a predetermined potential lightning strike zone. A current return network assembly is within the zone. An electrically conductive honeycomb central core is provided for conducting electrical current through the assembly and through the zone wherein the electrical current has been caused by a lightning strike on the aircraft at the zone. |
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The current return network assembly includes an electrically conductive honeycomb central core that conducts electrical current both through the assembly and through the predetermined potential lightning strike zone. The electrical current is caused by a lightning strike on the aircraft at the predetermined potential lightning strike zone. According to an embodiment, an aircraft has a predetermined potential lightning strike zone. A current return network assembly is within the zone. An electrically conductive honeycomb central core is provided for conducting electrical current through the assembly and through the zone wherein the electrical current has been caused by a lightning strike on the aircraft at the zone.</description><language>eng</language><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ; ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ; ELECTRICITY ; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS ; NATURALLY-OCCURRING ELECTRICITY ; PRINTED CIRCUITS ; STATIC ELECTRICITY</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=20141002&DB=EPODOC&CC=US&NR=2014293497A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20141002&DB=EPODOC&CC=US&NR=2014293497A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DAY ARTHUR C</creatorcontrib><creatorcontrib>PIEHL MARC J</creatorcontrib><creatorcontrib>KAJITA KIRK B</creatorcontrib><creatorcontrib>FOLTZ GREGORY ALAN</creatorcontrib><creatorcontrib>GREGG PAUL S</creatorcontrib><title>Method and Apparatus for Providing a Current Return Network in an Aircraft Structure</title><description>According to an embodiment a current return network assembly, for an aircraft having a predetermined potential lightning strike zone, is mounted within the predetermined potential lightning strike zone. The current return network assembly includes an electrically conductive honeycomb central core that conducts electrical current both through the assembly and through the predetermined potential lightning strike zone. The electrical current is caused by a lightning strike on the aircraft at the predetermined potential lightning strike zone. According to an embodiment, an aircraft has a predetermined potential lightning strike zone. A current return network assembly is within the zone. An electrically conductive honeycomb central core is provided for conducting electrical current through the assembly and through the zone wherein the electrical current has been caused by a lightning strike on the aircraft at the zone.</description><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</subject><subject>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</subject><subject>ELECTRICITY</subject><subject>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</subject><subject>NATURALLY-OCCURRING ELECTRICITY</subject><subject>PRINTED CIRCUITS</subject><subject>STATIC ELECTRICITY</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy78KwjAQgPEsDqK-w4GzYP-AdAxFcVHE1rkczUWDkoTLRV_fDj6A07f8vrnqTySPYAC9AR0jMkpOYAPDhcPbGefvgNBmZvICV5LMHs4kn8BPcH76QDseGa1AJ5zHCdBSzSy-Eq1-Xaj1Yd-3xw3FMFCKOJInGW5duS3qsqnqZqeL6j_1BS_MOVA</recordid><startdate>20141002</startdate><enddate>20141002</enddate><creator>DAY ARTHUR C</creator><creator>PIEHL MARC J</creator><creator>KAJITA KIRK B</creator><creator>FOLTZ GREGORY ALAN</creator><creator>GREGG PAUL S</creator><scope>EVB</scope></search><sort><creationdate>20141002</creationdate><title>Method and Apparatus for Providing a Current Return Network in an Aircraft Structure</title><author>DAY ARTHUR C ; PIEHL MARC J ; KAJITA KIRK B ; FOLTZ GREGORY ALAN ; GREGG PAUL S</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2014293497A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2014</creationdate><topic>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</topic><topic>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</topic><topic>ELECTRICITY</topic><topic>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</topic><topic>NATURALLY-OCCURRING ELECTRICITY</topic><topic>PRINTED CIRCUITS</topic><topic>STATIC ELECTRICITY</topic><toplevel>online_resources</toplevel><creatorcontrib>DAY ARTHUR C</creatorcontrib><creatorcontrib>PIEHL MARC J</creatorcontrib><creatorcontrib>KAJITA KIRK B</creatorcontrib><creatorcontrib>FOLTZ GREGORY ALAN</creatorcontrib><creatorcontrib>GREGG PAUL S</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DAY ARTHUR C</au><au>PIEHL MARC J</au><au>KAJITA KIRK B</au><au>FOLTZ GREGORY ALAN</au><au>GREGG PAUL S</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method and Apparatus for Providing a Current Return Network in an Aircraft Structure</title><date>2014-10-02</date><risdate>2014</risdate><abstract>According to an embodiment a current return network assembly, for an aircraft having a predetermined potential lightning strike zone, is mounted within the predetermined potential lightning strike zone. The current return network assembly includes an electrically conductive honeycomb central core that conducts electrical current both through the assembly and through the predetermined potential lightning strike zone. The electrical current is caused by a lightning strike on the aircraft at the predetermined potential lightning strike zone. According to an embodiment, an aircraft has a predetermined potential lightning strike zone. A current return network assembly is within the zone. An electrically conductive honeycomb central core is provided for conducting electrical current through the assembly and through the zone wherein the electrical current has been caused by a lightning strike on the aircraft at the zone.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS NATURALLY-OCCURRING ELECTRICITY PRINTED CIRCUITS STATIC ELECTRICITY |
| title | Method and Apparatus for Providing a Current Return Network in an Aircraft Structure |
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