AIRCRAFT SEAT WITH SPRING-ASSISTED ACTUATION

An aircraft seat may include an upper aircraft seat assembly (126), a lower aircraft seat assembly (128), and a frame actuation assembly (110) configured to actuate the upper aircraft seat assembly (126) relative to the lower aircraft seat assembly (128). The lower aircraft seat assembly (128) may i...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: JACOB, Twinkle V, PENCE, Tracy
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 JACOB, Twinkle V
PENCE, Tracy
description An aircraft seat may include an upper aircraft seat assembly (126), a lower aircraft seat assembly (128), and a frame actuation assembly (110) configured to actuate the upper aircraft seat assembly (126) relative to the lower aircraft seat assembly (128). The lower aircraft seat assembly (128) may include at least one spring (202) coupled to a foundation (108) with a sloped actuation surface configured to cause the upper aircraft seat assembly (126) to be at a decreased height when in a bed position. The compressing of the at least one spring (202) may be configured to counterbalance a load within the aircraft seat and generate a controlled actuation of the upper aircraft seat assembly (126) from an upright position to the bed position. A return force provided by the at least one spring (202) may assist the frame actuation assembly (110) during actuation of the upper aircraft seat assembly (126) from the decreased height of the bed position to the upright position.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3895991B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3895991B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3895991B13</originalsourceid><addsrcrecordid>eNrjZNBx9AxyDnJ0C1EIdnUMUQj3DPFQCA4I8vRz13UMDvYMDnF1UXB0Dgl1DPH09-NhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcYWlqaWloZOhsZEKAEAYdslEg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIRCRAFT SEAT WITH SPRING-ASSISTED ACTUATION</title><source>esp@cenet</source><creator>JACOB, Twinkle V ; PENCE, Tracy</creator><creatorcontrib>JACOB, Twinkle V ; PENCE, Tracy</creatorcontrib><description>An aircraft seat may include an upper aircraft seat assembly (126), a lower aircraft seat assembly (128), and a frame actuation assembly (110) configured to actuate the upper aircraft seat assembly (126) relative to the lower aircraft seat assembly (128). The lower aircraft seat assembly (128) may include at least one spring (202) coupled to a foundation (108) with a sloped actuation surface configured to cause the upper aircraft seat assembly (126) to be at a decreased height when in a bed position. The compressing of the at least one spring (202) may be configured to counterbalance a load within the aircraft seat and generate a controlled actuation of the upper aircraft seat assembly (126) from an upright position to the bed position. A return force provided by the at least one spring (202) may assist the frame actuation assembly (110) during actuation of the upper aircraft seat assembly (126) from the decreased height of the bed position to the upright 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 ; SEATS SPECIALLY ADAPTED FOR VEHICLES ; TRANSPORTING ; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR ; VEHICLES IN GENERAL</subject><creationdate>2023</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=20230823&amp;DB=EPODOC&amp;CC=EP&amp;NR=3895991B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20230823&amp;DB=EPODOC&amp;CC=EP&amp;NR=3895991B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JACOB, Twinkle V</creatorcontrib><creatorcontrib>PENCE, Tracy</creatorcontrib><title>AIRCRAFT SEAT WITH SPRING-ASSISTED ACTUATION</title><description>An aircraft seat may include an upper aircraft seat assembly (126), a lower aircraft seat assembly (128), and a frame actuation assembly (110) configured to actuate the upper aircraft seat assembly (126) relative to the lower aircraft seat assembly (128). The lower aircraft seat assembly (128) may include at least one spring (202) coupled to a foundation (108) with a sloped actuation surface configured to cause the upper aircraft seat assembly (126) to be at a decreased height when in a bed position. The compressing of the at least one spring (202) may be configured to counterbalance a load within the aircraft seat and generate a controlled actuation of the upper aircraft seat assembly (126) from an upright position to the bed position. A return force provided by the at least one spring (202) may assist the frame actuation assembly (110) during actuation of the upper aircraft seat assembly (126) from the decreased height of the bed position to the upright 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>SEATS SPECIALLY ADAPTED FOR VEHICLES</subject><subject>TRANSPORTING</subject><subject>VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR</subject><subject>VEHICLES IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBx9AxyDnJ0C1EIdnUMUQj3DPFQCA4I8vRz13UMDvYMDnF1UXB0Dgl1DPH09-NhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcYWlqaWloZOhsZEKAEAYdslEg</recordid><startdate>20230823</startdate><enddate>20230823</enddate><creator>JACOB, Twinkle V</creator><creator>PENCE, Tracy</creator><scope>EVB</scope></search><sort><creationdate>20230823</creationdate><title>AIRCRAFT SEAT WITH SPRING-ASSISTED ACTUATION</title><author>JACOB, Twinkle V ; PENCE, Tracy</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3895991B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</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>SEATS SPECIALLY ADAPTED FOR VEHICLES</topic><topic>TRANSPORTING</topic><topic>VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR</topic><topic>VEHICLES IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>JACOB, Twinkle V</creatorcontrib><creatorcontrib>PENCE, Tracy</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JACOB, Twinkle V</au><au>PENCE, Tracy</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT SEAT WITH SPRING-ASSISTED ACTUATION</title><date>2023-08-23</date><risdate>2023</risdate><abstract>An aircraft seat may include an upper aircraft seat assembly (126), a lower aircraft seat assembly (128), and a frame actuation assembly (110) configured to actuate the upper aircraft seat assembly (126) relative to the lower aircraft seat assembly (128). The lower aircraft seat assembly (128) may include at least one spring (202) coupled to a foundation (108) with a sloped actuation surface configured to cause the upper aircraft seat assembly (126) to be at a decreased height when in a bed position. The compressing of the at least one spring (202) may be configured to counterbalance a load within the aircraft seat and generate a controlled actuation of the upper aircraft seat assembly (126) from an upright position to the bed position. A return force provided by the at least one spring (202) may assist the frame actuation assembly (110) during actuation of the upper aircraft seat assembly (126) from the decreased height of the bed position to the upright position.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3895991B1
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
SEATS SPECIALLY ADAPTED FOR VEHICLES
TRANSPORTING
VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR
VEHICLES IN GENERAL
title AIRCRAFT SEAT WITH SPRING-ASSISTED ACTUATION
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-10T18%3A43%3A31IST&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=JACOB,%20Twinkle%20V&rft.date=2023-08-23&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3895991B1%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