AVIONIC CONNECTOR INTERFACE DISTRIBUTION UNIT
An avionic connector interface distribution unit interfaces a central controller with a plurality of avionic devices. The distribution unit comprises a large avionic connector (16), a mother input/output (I/O) printed wiring board (18), first and second daughter I/O printed wiring boards (20, 22), f...
Gespeichert in:
| Hauptverfasser: | , , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| 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 | BASSETT, GREGORY, J BRYER, STEVEN, M LAYTON, RANDOLPH, M HAAS, DONNA, E HORNIG, JAMES, F SHEFFIELD, JAMES, W STEINMAN, JOSEPH, R BEATON, JEFFERY, D LYON, RICHARD, A |
| description | An avionic connector interface distribution unit interfaces a central controller with a plurality of avionic devices. The distribution unit comprises a large avionic connector (16), a mother input/output (I/O) printed wiring board (18), first and second daughter I/O printed wiring boards (20, 22), first and second parallel headers (28, 30) formed of matable connector pairs, and a plurality of miniature connectors (14). The mother board (18) includes first and second planar surfaces, and each of the daughter boards (20, 22) includes first and second planar surfaces. The first and second daughter boards (20, 22) are generally co-planar and adjacent to each other, and these daughter boards (20, 22) are parallel to the mother board (18). The second surface of the mother board (18) faces the first surfaces of the daughter boards (20, 22). The first header (28) is situated between and mounted to the second surface of the mother board (18) and the first surfaces of the first daughter board (20). Similarly, the second header (30) is situated between and mounted to the second surface of the mother board (18) and the first surface of the second daughter board (22). The large avionic connector (16) is mounted to the first surface of the mother board (18). The plurality of miniature connectors (14) are mounted to the second surfaces of the daughter boards (20, 22). |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP0791234A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP0791234A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP0791234A13</originalsourceid><addsrcrecordid>eNrjZNB1DPP09_N0VnD29_NzdQ7xD1Lw9AtxDXJzdHZVcPEMDgnydAoNASpRCPXzDOFhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAQbmloZGxiaOhsZEKAEAke8lVQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AVIONIC CONNECTOR INTERFACE DISTRIBUTION UNIT</title><source>esp@cenet</source><creator>BASSETT, GREGORY, J ; BRYER, STEVEN, M ; LAYTON, RANDOLPH, M ; HAAS, DONNA, E ; HORNIG, JAMES, F ; SHEFFIELD, JAMES, W ; STEINMAN, JOSEPH, R ; BEATON, JEFFERY, D ; LYON, RICHARD, A</creator><creatorcontrib>BASSETT, GREGORY, J ; BRYER, STEVEN, M ; LAYTON, RANDOLPH, M ; HAAS, DONNA, E ; HORNIG, JAMES, F ; SHEFFIELD, JAMES, W ; STEINMAN, JOSEPH, R ; BEATON, JEFFERY, D ; LYON, RICHARD, A</creatorcontrib><description>An avionic connector interface distribution unit interfaces a central controller with a plurality of avionic devices. The distribution unit comprises a large avionic connector (16), a mother input/output (I/O) printed wiring board (18), first and second daughter I/O printed wiring boards (20, 22), first and second parallel headers (28, 30) formed of matable connector pairs, and a plurality of miniature connectors (14). The mother board (18) includes first and second planar surfaces, and each of the daughter boards (20, 22) includes first and second planar surfaces. The first and second daughter boards (20, 22) are generally co-planar and adjacent to each other, and these daughter boards (20, 22) are parallel to the mother board (18). The second surface of the mother board (18) faces the first surfaces of the daughter boards (20, 22). The first header (28) is situated between and mounted to the second surface of the mother board (18) and the first surfaces of the first daughter board (20). Similarly, the second header (30) is situated between and mounted to the second surface of the mother board (18) and the first surface of the second daughter board (22). The large avionic connector (16) is mounted to the first surface of the mother board (18). The plurality of miniature connectors (14) are mounted to the second surfaces of the daughter boards (20, 22).</description><edition>6</edition><language>eng ; fre ; ger</language><subject>BASIC ELECTRIC ELEMENTS ; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ; CURRENT COLLECTORS ; ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ; ELECTRICITY ; LINE CONNECTORS ; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS ; PERFORMING OPERATIONS ; PRINTED CIRCUITS ; TRANSPORTING ; VEHICLES IN GENERAL ; VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR</subject><creationdate>1997</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=19970827&DB=EPODOC&CC=EP&NR=0791234A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19970827&DB=EPODOC&CC=EP&NR=0791234A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BASSETT, GREGORY, J</creatorcontrib><creatorcontrib>BRYER, STEVEN, M</creatorcontrib><creatorcontrib>LAYTON, RANDOLPH, M</creatorcontrib><creatorcontrib>HAAS, DONNA, E</creatorcontrib><creatorcontrib>HORNIG, JAMES, F</creatorcontrib><creatorcontrib>SHEFFIELD, JAMES, W</creatorcontrib><creatorcontrib>STEINMAN, JOSEPH, R</creatorcontrib><creatorcontrib>BEATON, JEFFERY, D</creatorcontrib><creatorcontrib>LYON, RICHARD, A</creatorcontrib><title>AVIONIC CONNECTOR INTERFACE DISTRIBUTION UNIT</title><description>An avionic connector interface distribution unit interfaces a central controller with a plurality of avionic devices. The distribution unit comprises a large avionic connector (16), a mother input/output (I/O) printed wiring board (18), first and second daughter I/O printed wiring boards (20, 22), first and second parallel headers (28, 30) formed of matable connector pairs, and a plurality of miniature connectors (14). The mother board (18) includes first and second planar surfaces, and each of the daughter boards (20, 22) includes first and second planar surfaces. The first and second daughter boards (20, 22) are generally co-planar and adjacent to each other, and these daughter boards (20, 22) are parallel to the mother board (18). The second surface of the mother board (18) faces the first surfaces of the daughter boards (20, 22). The first header (28) is situated between and mounted to the second surface of the mother board (18) and the first surfaces of the first daughter board (20). Similarly, the second header (30) is situated between and mounted to the second surface of the mother board (18) and the first surface of the second daughter board (22). The large avionic connector (16) is mounted to the first surface of the mother board (18). The plurality of miniature connectors (14) are mounted to the second surfaces of the daughter boards (20, 22).</description><subject>BASIC ELECTRIC ELEMENTS</subject><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</subject><subject>CURRENT COLLECTORS</subject><subject>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</subject><subject>ELECTRICITY</subject><subject>LINE CONNECTORS</subject><subject>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</subject><subject>PERFORMING OPERATIONS</subject><subject>PRINTED CIRCUITS</subject><subject>TRANSPORTING</subject><subject>VEHICLES IN GENERAL</subject><subject>VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1997</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB1DPP09_N0VnD29_NzdQ7xD1Lw9AtxDXJzdHZVcPEMDgnydAoNASpRCPXzDOFhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAQbmloZGxiaOhsZEKAEAke8lVQ</recordid><startdate>19970827</startdate><enddate>19970827</enddate><creator>BASSETT, GREGORY, J</creator><creator>BRYER, STEVEN, M</creator><creator>LAYTON, RANDOLPH, M</creator><creator>HAAS, DONNA, E</creator><creator>HORNIG, JAMES, F</creator><creator>SHEFFIELD, JAMES, W</creator><creator>STEINMAN, JOSEPH, R</creator><creator>BEATON, JEFFERY, D</creator><creator>LYON, RICHARD, A</creator><scope>EVB</scope></search><sort><creationdate>19970827</creationdate><title>AVIONIC CONNECTOR INTERFACE DISTRIBUTION UNIT</title><author>BASSETT, GREGORY, J ; BRYER, STEVEN, M ; LAYTON, RANDOLPH, M ; HAAS, DONNA, E ; HORNIG, JAMES, F ; SHEFFIELD, JAMES, W ; STEINMAN, JOSEPH, R ; BEATON, JEFFERY, D ; LYON, RICHARD, A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP0791234A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>1997</creationdate><topic>BASIC ELECTRIC ELEMENTS</topic><topic>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</topic><topic>CURRENT COLLECTORS</topic><topic>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</topic><topic>ELECTRICITY</topic><topic>LINE CONNECTORS</topic><topic>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</topic><topic>PERFORMING OPERATIONS</topic><topic>PRINTED CIRCUITS</topic><topic>TRANSPORTING</topic><topic>VEHICLES IN GENERAL</topic><topic>VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR</topic><toplevel>online_resources</toplevel><creatorcontrib>BASSETT, GREGORY, J</creatorcontrib><creatorcontrib>BRYER, STEVEN, M</creatorcontrib><creatorcontrib>LAYTON, RANDOLPH, M</creatorcontrib><creatorcontrib>HAAS, DONNA, E</creatorcontrib><creatorcontrib>HORNIG, JAMES, F</creatorcontrib><creatorcontrib>SHEFFIELD, JAMES, W</creatorcontrib><creatorcontrib>STEINMAN, JOSEPH, R</creatorcontrib><creatorcontrib>BEATON, JEFFERY, D</creatorcontrib><creatorcontrib>LYON, RICHARD, A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BASSETT, GREGORY, J</au><au>BRYER, STEVEN, M</au><au>LAYTON, RANDOLPH, M</au><au>HAAS, DONNA, E</au><au>HORNIG, JAMES, F</au><au>SHEFFIELD, JAMES, W</au><au>STEINMAN, JOSEPH, R</au><au>BEATON, JEFFERY, D</au><au>LYON, RICHARD, A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AVIONIC CONNECTOR INTERFACE DISTRIBUTION UNIT</title><date>1997-08-27</date><risdate>1997</risdate><abstract>An avionic connector interface distribution unit interfaces a central controller with a plurality of avionic devices. The distribution unit comprises a large avionic connector (16), a mother input/output (I/O) printed wiring board (18), first and second daughter I/O printed wiring boards (20, 22), first and second parallel headers (28, 30) formed of matable connector pairs, and a plurality of miniature connectors (14). The mother board (18) includes first and second planar surfaces, and each of the daughter boards (20, 22) includes first and second planar surfaces. The first and second daughter boards (20, 22) are generally co-planar and adjacent to each other, and these daughter boards (20, 22) are parallel to the mother board (18). The second surface of the mother board (18) faces the first surfaces of the daughter boards (20, 22). The first header (28) is situated between and mounted to the second surface of the mother board (18) and the first surfaces of the first daughter board (20). Similarly, the second header (30) is situated between and mounted to the second surface of the mother board (18) and the first surface of the second daughter board (22). The large avionic connector (16) is mounted to the first surface of the mother board (18). The plurality of miniature connectors (14) are mounted to the second surfaces of the daughter boards (20, 22).</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP0791234A1 |
| source | esp@cenet |
| subjects | BASIC ELECTRIC ELEMENTS CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS CURRENT COLLECTORS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY LINE CONNECTORS MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PERFORMING OPERATIONS PRINTED CIRCUITS TRANSPORTING VEHICLES IN GENERAL VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR |
| title | AVIONIC CONNECTOR INTERFACE DISTRIBUTION UNIT |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-23T01%3A09%3A04IST&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=BASSETT,%20GREGORY,%20J&rft.date=1997-08-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP0791234A1%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 |