AIRCRAFT TRAY TABLE RETENTION ASSEMBLY

An aircraft tray table retention assembly may include a seat magnetic component (114) installed within a rear bezel (104) of an aircraft seat (100), and a tray table magnetic component (202) installed within an aircraft tray table (200). The aircraft tray table may be coupled to the aircraft seat vi...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: HUIJSING, Hans, WANNER, Jackson R, RAMAN, Varun, SPENCER, Gregory S
Format: Patent
Sprache:eng ; fre ; ger
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 HUIJSING, Hans
WANNER, Jackson R
RAMAN, Varun
SPENCER, Gregory S
description An aircraft tray table retention assembly may include a seat magnetic component (114) installed within a rear bezel (104) of an aircraft seat (100), and a tray table magnetic component (202) installed within an aircraft tray table (200). The aircraft tray table may be coupled to the aircraft seat via at least one of one or more hinges (326) or a set of rails, and may be configured to actuate between a stowed position and a deployed position via the at least one of one or more hinges or a set of rails. The tray table magnetic component may be configured to engage the seat magnetic component when the aircraft tray table is in the stowed position. The aircraft tray table retention assembly may include a tray magnetic component configured to engage the tray table magnetic component when the aircraft tray table is in the deployed position.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3992080A2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3992080A2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3992080A23</originalsourceid><addsrcrecordid>eNrjZFBz9AxyDnJ0C1EICXKMVAhxdPJxVQhyDXH1C_H091NwDA529XXyieRhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcaWlkYGFgaORsZEKAEAhLkjQQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIRCRAFT TRAY TABLE RETENTION ASSEMBLY</title><source>esp@cenet</source><creator>HUIJSING, Hans ; WANNER, Jackson R ; RAMAN, Varun ; SPENCER, Gregory S</creator><creatorcontrib>HUIJSING, Hans ; WANNER, Jackson R ; RAMAN, Varun ; SPENCER, Gregory S</creatorcontrib><description>An aircraft tray table retention assembly may include a seat magnetic component (114) installed within a rear bezel (104) of an aircraft seat (100), and a tray table magnetic component (202) installed within an aircraft tray table (200). The aircraft tray table may be coupled to the aircraft seat via at least one of one or more hinges (326) or a set of rails, and may be configured to actuate between a stowed position and a deployed position via the at least one of one or more hinges or a set of rails. The tray table magnetic component may be configured to engage the seat magnetic component when the aircraft tray table is in the stowed position. The aircraft tray table retention assembly may include a tray magnetic component configured to engage the tray table magnetic component when the aircraft tray table is in the deployed position.</description><language>eng ; fre ; ger</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>2022</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=20220504&amp;DB=EPODOC&amp;CC=EP&amp;NR=3992080A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220504&amp;DB=EPODOC&amp;CC=EP&amp;NR=3992080A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUIJSING, Hans</creatorcontrib><creatorcontrib>WANNER, Jackson R</creatorcontrib><creatorcontrib>RAMAN, Varun</creatorcontrib><creatorcontrib>SPENCER, Gregory S</creatorcontrib><title>AIRCRAFT TRAY TABLE RETENTION ASSEMBLY</title><description>An aircraft tray table retention assembly may include a seat magnetic component (114) installed within a rear bezel (104) of an aircraft seat (100), and a tray table magnetic component (202) installed within an aircraft tray table (200). The aircraft tray table may be coupled to the aircraft seat via at least one of one or more hinges (326) or a set of rails, and may be configured to actuate between a stowed position and a deployed position via the at least one of one or more hinges or a set of rails. The tray table magnetic component may be configured to engage the seat magnetic component when the aircraft tray table is in the stowed position. The aircraft tray table retention assembly may include a tray magnetic component configured to engage the tray table magnetic component when the aircraft tray table is in the deployed position.</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBz9AxyDnJ0C1EICXKMVAhxdPJxVQhyDXH1C_H091NwDA529XXyieRhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcaWlkYGFgaORsZEKAEAhLkjQQ</recordid><startdate>20220504</startdate><enddate>20220504</enddate><creator>HUIJSING, Hans</creator><creator>WANNER, Jackson R</creator><creator>RAMAN, Varun</creator><creator>SPENCER, Gregory S</creator><scope>EVB</scope></search><sort><creationdate>20220504</creationdate><title>AIRCRAFT TRAY TABLE RETENTION ASSEMBLY</title><author>HUIJSING, Hans ; WANNER, Jackson R ; RAMAN, Varun ; SPENCER, Gregory S</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3992080A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</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>HUIJSING, Hans</creatorcontrib><creatorcontrib>WANNER, Jackson R</creatorcontrib><creatorcontrib>RAMAN, Varun</creatorcontrib><creatorcontrib>SPENCER, Gregory S</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUIJSING, Hans</au><au>WANNER, Jackson R</au><au>RAMAN, Varun</au><au>SPENCER, Gregory S</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT TRAY TABLE RETENTION ASSEMBLY</title><date>2022-05-04</date><risdate>2022</risdate><abstract>An aircraft tray table retention assembly may include a seat magnetic component (114) installed within a rear bezel (104) of an aircraft seat (100), and a tray table magnetic component (202) installed within an aircraft tray table (200). The aircraft tray table may be coupled to the aircraft seat via at least one of one or more hinges (326) or a set of rails, and may be configured to actuate between a stowed position and a deployed position via the at least one of one or more hinges or a set of rails. The tray table magnetic component may be configured to engage the seat magnetic component when the aircraft tray table is in the stowed position. The aircraft tray table retention assembly may include a tray magnetic component configured to engage the tray table magnetic component when the aircraft tray table is in the deployed position.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3992080A2
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 AIRCRAFT TRAY TABLE RETENTION ASSEMBLY
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-24T22%3A54%3A49IST&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=HUIJSING,%20Hans&rft.date=2022-05-04&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3992080A2%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