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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: SMITH, Joshua T, KINARD, Marc W
Format: Patent
Sprache:eng ; fre
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
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).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_WO2018009201A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>WO2018009201A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_WO2018009201A13</originalsourceid><addsrcrecordid>eNrjZJBx9vcN8A_2DHFVCHZ1DPH0c1cAi_i5-oUE8zCwpiXmFKfyQmluBmU31xBnD93Ugvz41OKCxOTUvNSS-HB_IwNDCwMDSyDlaGhMnCoADO8h5Q</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COMPOSITE SEATING COMPONENTS</title><source>esp@cenet</source><creator>SMITH, Joshua T ; KINARD, Marc W</creator><creatorcontrib>SMITH, Joshua T ; KINARD, Marc W</creatorcontrib><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><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&amp;date=20180111&amp;DB=EPODOC&amp;CC=WO&amp;NR=2018009201A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20180111&amp;DB=EPODOC&amp;CC=WO&amp;NR=2018009201A1$$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>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre
recordid cdi_epo_espacenet_WO2018009201A1
source esp@cenet
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
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T11%3A03%3A55IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=SMITH,%20Joshua%20T&rft.date=2018-01-11&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EWO2018009201A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true