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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Hauptverfasser: Dopker, Bernhard, Diep, Paul
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Sprache:eng ; fre ; ger
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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.
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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
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subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Circumference splice for joining shell structures
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