Circumference splice for joining shell structures
The disclosed shell structure splice (10) and method includes a first panel (108) having a first edge, a second panel having a second edge, the second edge being positioned in edgewise alignment with the first edge to form a splice joint, a strap (12) bridging the splice joint and attached to the fi...
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creator | Dopker, Bernhard Diep, Paul |
description | The disclosed shell structure splice (10) and method includes a first panel (108) having a first edge, a second panel having a second edge, the second edge being positioned in edgewise alignment with the first edge to form a splice joint, a strap (12) bridging the splice joint and attached to the first panel and the second panel, the strap having a first tapered region (22a) and a second tapered region (22b), a first fitting (24a) having a tapered section (34)and a flat section (36), the tapered section being attached to the first tapered region of the strap, and a second fitting (24b) having a tapered section and a flat section, the tapered section being attached to the second tapered region of the strap. |
format | Patent |
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fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; 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=20170329&DB=EPODOC&CC=EP&NR=2727821B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170329&DB=EPODOC&CC=EP&NR=2727821B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Dopker, Bernhard</creatorcontrib><creatorcontrib>Diep, Paul</creatorcontrib><title>Circumference splice for joining shell structures</title><description>The disclosed shell structure splice (10) and method includes a first panel (108) having a first edge, a second panel having a second edge, the second edge being positioned in edgewise alignment with the first edge to form a splice joint, a strap (12) bridging the splice joint and attached to the first panel and the second panel, the strap having a first tapered region (22a) and a second tapered region (22b), a first fitting (24a) having a tapered section (34)and a flat section (36), the tapered section being attached to the first tapered region of the strap, and a second fitting (24b) having a tapered section and a flat section, the tapered section being attached to the second tapered region of the strap.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB0zixKLs1NSy1KzUtOVSguyMkEUmn5RQpZ-Zl5mXnpCsUZqTk5CsUlRaXJJaVFqcU8DKxpiTnFqbxQmptBwc01xNlDN7UgPz61uCAxOTUvtSTeNcDI3MjcwsjQydCYCCUAcjcryA</recordid><startdate>20170329</startdate><enddate>20170329</enddate><creator>Dopker, Bernhard</creator><creator>Diep, Paul</creator><scope>EVB</scope></search><sort><creationdate>20170329</creationdate><title>Circumference splice for joining shell structures</title><author>Dopker, Bernhard ; Diep, Paul</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2727821B13</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>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Dopker, Bernhard</creatorcontrib><creatorcontrib>Diep, Paul</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Dopker, Bernhard</au><au>Diep, Paul</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Circumference splice for joining shell structures</title><date>2017-03-29</date><risdate>2017</risdate><abstract>The disclosed shell structure splice (10) and method includes a first panel (108) having a first edge, a second panel having a second edge, the second edge being positioned in edgewise alignment with the first edge to form a splice joint, a strap (12) bridging the splice joint and attached to the first panel and the second panel, the strap having a first tapered region (22a) and a second tapered region (22b), a first fitting (24a) having a tapered section (34)and a flat section (36), the tapered section being attached to the first tapered region of the strap, and a second fitting (24b) having a tapered section and a flat section, the tapered section being attached to the second tapered region of the strap.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
recordid | cdi_epo_espacenet_EP2727821B1 |
source | esp@cenet |
subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | Circumference splice for joining shell structures |
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