COMPOSITE SEATING COMPONENTS
Composite components (22, 32) are described herein. An example composite component (22, 32) includes a fill material sandwiched between a first shell and a second shell. The first shell can include a cavity for receiving the fill material. The second shell can include a recessed portion extending in...
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creator | SMITH, Joshua T KINARD, Marc W |
description | Composite components (22, 32) are described herein. An example composite component (22, 32) includes a fill material sandwiched between a first shell and a second shell. The first shell can include a cavity for receiving the fill material. The second shell can include a recessed portion extending into the cavity. The recessed portion can be configured to receive a separate component (16a, 30) of a passenger seat (12).
Cette invention concerne des composants composites (22, 32). Un composant composite (22, 32) donné à titre d'exemple comprend un matériau de remplissage pris en sandwich entre une première coque et une seconde coque. La première coque peut comprendre une cavité destinée à recevoir le matériau de remplissage. La seconde coque peut comprendre une partie en retrait s'étendant dans la cavité. La partie en retrait peut être configurée pour recevoir un composant distinct (16a, 30) d'un siège passager (12). |
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Cette invention concerne des composants composites (22, 32). Un composant composite (22, 32) donné à titre d'exemple comprend un matériau de remplissage pris en sandwich entre une première coque et une seconde coque. La première coque peut comprendre une cavité destinée à recevoir le matériau de remplissage. La seconde coque peut comprendre une partie en retrait s'étendant dans la cavité. La partie en retrait peut être configurée pour recevoir un composant distinct (16a, 30) d'un siège passager (12).</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2018</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=20180111&DB=EPODOC&CC=WO&NR=2018009201A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180111&DB=EPODOC&CC=WO&NR=2018009201A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SMITH, Joshua T</creatorcontrib><creatorcontrib>KINARD, Marc W</creatorcontrib><title>COMPOSITE SEATING COMPONENTS</title><description>Composite components (22, 32) are described herein. An example composite component (22, 32) includes a fill material sandwiched between a first shell and a second shell. The first shell can include a cavity for receiving the fill material. The second shell can include a recessed portion extending into the cavity. The recessed portion can be configured to receive a separate component (16a, 30) of a passenger seat (12).
Cette invention concerne des composants composites (22, 32). Un composant composite (22, 32) donné à titre d'exemple comprend un matériau de remplissage pris en sandwich entre une première coque et une seconde coque. La première coque peut comprendre une cavité destinée à recevoir le matériau de remplissage. La seconde coque peut comprendre une partie en retrait s'étendant dans la cavité. La partie en retrait peut être configurée pour recevoir un composant distinct (16a, 30) d'un siège passager (12).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBx9vcN8A_2DHFVCHZ1DPH0c1cAi_i5-oUE8zCwpiXmFKfyQmluBmU31xBnD93Ugvz41OKCxOTUvNSS-HB_IwNDCwMDSyDlaGhMnCoADO8h5Q</recordid><startdate>20180111</startdate><enddate>20180111</enddate><creator>SMITH, Joshua T</creator><creator>KINARD, Marc W</creator><scope>EVB</scope></search><sort><creationdate>20180111</creationdate><title>COMPOSITE SEATING COMPONENTS</title><author>SMITH, Joshua T ; KINARD, Marc W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2018009201A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2018</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>SMITH, Joshua T</creatorcontrib><creatorcontrib>KINARD, Marc W</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SMITH, Joshua T</au><au>KINARD, Marc W</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPOSITE SEATING COMPONENTS</title><date>2018-01-11</date><risdate>2018</risdate><abstract>Composite components (22, 32) are described herein. An example composite component (22, 32) includes a fill material sandwiched between a first shell and a second shell. The first shell can include a cavity for receiving the fill material. The second shell can include a recessed portion extending into the cavity. The recessed portion can be configured to receive a separate component (16a, 30) of a passenger seat (12).
Cette invention concerne des composants composites (22, 32). Un composant composite (22, 32) donné à titre d'exemple comprend un matériau de remplissage pris en sandwich entre une première coque et une seconde coque. La première coque peut comprendre une cavité destinée à recevoir le matériau de remplissage. La seconde coque peut comprendre une partie en retrait s'étendant dans la cavité. La partie en retrait peut être configurée pour recevoir un composant distinct (16a, 30) d'un siège passager (12).</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | COMPOSITE SEATING COMPONENTS |
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