Composite stringer end trim
A stringer (2) having a stringer end trim (7) that reduces pull-off forces in a stringer connection structure, includes a stringer body (9); a stringer free edge (8) provided on said stringer body (9); and a stringer end trim (7) having at least one curvature (10, 12, 14) provided in the stringer fr...
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creator | LEE HANGKI DOPKER BERNHARD LIN CHUN-LIANG BARNARD JOSHUA D PAEZ CARLOS ALBERTO ARENT BRIAN W |
description | A stringer (2) having a stringer end trim (7) that reduces pull-off forces in a stringer connection structure, includes a stringer body (9); a stringer free edge (8) provided on said stringer body (9); and a stringer end trim (7) having at least one curvature (10, 12, 14) provided in the stringer free edge (8) to form the stringer connection structure. |
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a stringer free edge (8) provided on said stringer body (9); and a stringer end trim (7) having at least one curvature (10, 12, 14) provided in the stringer free edge (8) to form the stringer connection structure.</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2013</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=20130123&DB=EPODOC&CC=CN&NR=102892670A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130123&DB=EPODOC&CC=CN&NR=102892670A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEE HANGKI</creatorcontrib><creatorcontrib>DOPKER BERNHARD</creatorcontrib><creatorcontrib>LIN CHUN-LIANG</creatorcontrib><creatorcontrib>BARNARD JOSHUA D</creatorcontrib><creatorcontrib>PAEZ CARLOS ALBERTO</creatorcontrib><creatorcontrib>ARENT BRIAN W</creatorcontrib><title>Composite stringer end trim</title><description>A stringer (2) having a stringer end trim (7) that reduces pull-off forces in a stringer connection structure, includes a stringer body (9); a stringer free edge (8) provided on said stringer body (9); and a stringer end trim (7) having at least one curvature (10, 12, 14) provided in the stringer free edge (8) to form the stringer connection structure.</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>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB2zs8tyC_OLElVKC4pysxLTy1SSM1LUQCyc3kYWNMSc4pTeaE0N4Oim2uIs4duakF-fGpxQWJyal5qSbyzn6GBkYWlkZm5gaMxMWoAgIQjfA</recordid><startdate>20130123</startdate><enddate>20130123</enddate><creator>LEE HANGKI</creator><creator>DOPKER BERNHARD</creator><creator>LIN CHUN-LIANG</creator><creator>BARNARD JOSHUA D</creator><creator>PAEZ CARLOS ALBERTO</creator><creator>ARENT BRIAN W</creator><scope>EVB</scope></search><sort><creationdate>20130123</creationdate><title>Composite stringer end trim</title><author>LEE HANGKI ; DOPKER BERNHARD ; LIN CHUN-LIANG ; BARNARD JOSHUA D ; PAEZ CARLOS ALBERTO ; ARENT BRIAN W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN102892670A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2013</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>LEE HANGKI</creatorcontrib><creatorcontrib>DOPKER BERNHARD</creatorcontrib><creatorcontrib>LIN CHUN-LIANG</creatorcontrib><creatorcontrib>BARNARD JOSHUA D</creatorcontrib><creatorcontrib>PAEZ CARLOS ALBERTO</creatorcontrib><creatorcontrib>ARENT BRIAN W</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEE HANGKI</au><au>DOPKER BERNHARD</au><au>LIN CHUN-LIANG</au><au>BARNARD JOSHUA D</au><au>PAEZ CARLOS ALBERTO</au><au>ARENT BRIAN W</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Composite stringer end trim</title><date>2013-01-23</date><risdate>2013</risdate><abstract>A stringer (2) having a stringer end trim (7) that reduces pull-off forces in a stringer connection structure, includes a stringer body (9); a stringer free edge (8) provided on said stringer body (9); and a stringer end trim (7) having at least one curvature (10, 12, 14) provided in the stringer free edge (8) to form the stringer connection structure.</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | Composite stringer end trim |
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