Composite structural part
The part has multiple fiber layers oriented with respect to longitudinal direction (2) of the part. One of the fiber layers is constituted of continuous fibers extending from one edge to another edge of the part on a surface of the part, where thickness of the part is constant. The fiber layers are...
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| creator | GUILLEMAUT, JULIEN SOULA, DENIS |
| description | The part has multiple fiber layers oriented with respect to longitudinal direction (2) of the part. One of the fiber layers is constituted of continuous fibers extending from one edge to another edge of the part on a surface of the part, where thickness of the part is constant. The fiber layers are formed as a lay-up with multi-axes (110, 140, 150), where the multi-axes are arranged in a central part of the structural part. An independent claim is also included for a center wing box of an aircraft comprising a spar. |
| format | Patent |
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One of the fiber layers is constituted of continuous fibers extending from one edge to another edge of the part on a surface of the part, where thickness of the part is constant. The fiber layers are formed as a lay-up with multi-axes (110, 140, 150), where the multi-axes are arranged in a central part of the structural part. An independent claim is also included for a center wing box of an aircraft comprising a spar.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2015</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=20150701&DB=EPODOC&CC=EP&NR=2388130B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150701&DB=EPODOC&CC=EP&NR=2388130B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GUILLEMAUT, JULIEN</creatorcontrib><creatorcontrib>SOULA, DENIS</creatorcontrib><title>Composite structural part</title><description>The part has multiple fiber layers oriented with respect to longitudinal direction (2) of the part. One of the fiber layers is constituted of continuous fibers extending from one edge to another edge of the part on a surface of the part, where thickness of the part is constant. The fiber layers are formed as a lay-up with multi-axes (110, 140, 150), where the multi-axes are arranged in a central part of the structural part. An independent claim is also included for a center wing box of an aircraft comprising a spar.</description><subject>AEROPLANES</subject><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>TRANSPORTING</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB0zs8tyC_OLElVKC4pKk0uKS1KzFEoSCwq4WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRsYWFobGBk6GxkQoAQAD9CKf</recordid><startdate>20150701</startdate><enddate>20150701</enddate><creator>GUILLEMAUT, JULIEN</creator><creator>SOULA, DENIS</creator><scope>EVB</scope></search><sort><creationdate>20150701</creationdate><title>Composite structural part</title><author>GUILLEMAUT, JULIEN ; SOULA, DENIS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2388130B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2015</creationdate><topic>AEROPLANES</topic><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>TRANSPORTING</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>GUILLEMAUT, JULIEN</creatorcontrib><creatorcontrib>SOULA, DENIS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GUILLEMAUT, JULIEN</au><au>SOULA, DENIS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Composite structural part</title><date>2015-07-01</date><risdate>2015</risdate><abstract>The part has multiple fiber layers oriented with respect to longitudinal direction (2) of the part. One of the fiber layers is constituted of continuous fibers extending from one edge to another edge of the part on a surface of the part, where thickness of the part is constant. The fiber layers are formed as a lay-up with multi-axes (110, 140, 150), where the multi-axes are arranged in a central part of the structural part. An independent claim is also included for a center wing box of an aircraft comprising a spar.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | Composite structural part |
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