SUPPLEMENTAL RECLINE PANEL FOR AIRCRAFT CABIN ATTENDANT SEAT
A retrofit seat back assembly (150, 250, 350, 450) includes a supplemental recline panel (152, 252, 352, 452) having an upper end (241) and a lower end (242); a pivot member (275, 375, 475) disposed proximate the upper end (241) and configured to pivotally engage a seat back frame (114, 314, 414) of...
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creator | HOOVER, Douglas E ACHARYA, Pradeep MAGLIA, Dominic J KOZHIPURAM, Akhil Rajagopal |
description | A retrofit seat back assembly (150, 250, 350, 450) includes a supplemental recline panel (152, 252, 352, 452) having an upper end (241) and a lower end (242); a pivot member (275, 375, 475) disposed proximate the upper end (241) and configured to pivotally engage a seat back frame (114, 314, 414) of a stowable seat (100); an actuator (254, 354, 454) disposed proximate the lower end (242) and configured to operably engage the seat back frame (114, 314, 414) and move the supplemental recline panel (152, 252, 352, 452) between a retracted position and a deployed position; and a bias element (260, 360, 460) disposed between the supplemental recline panel (152, 252, 352, 452) and the seat back frame (114, 314, 414) and configured to urge the supplemental recline panel (152, 252, 352, 452) toward the seat back frame (114, 314, 414). |
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a pivot member (275, 375, 475) disposed proximate the upper end (241) and configured to pivotally engage a seat back frame (114, 314, 414) of a stowable seat (100); an actuator (254, 354, 454) disposed proximate the lower end (242) and configured to operably engage the seat back frame (114, 314, 414) and move the supplemental recline panel (152, 252, 352, 452) between a retracted position and a deployed position; and a bias element (260, 360, 460) disposed between the supplemental recline panel (152, 252, 352, 452) and the seat back frame (114, 314, 414) and configured to urge the supplemental recline panel (152, 252, 352, 452) toward the seat back frame (114, 314, 414).</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>2020</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=20200422&DB=EPODOC&CC=EP&NR=3640136A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200422&DB=EPODOC&CC=EP&NR=3640136A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HOOVER, Douglas E</creatorcontrib><creatorcontrib>ACHARYA, Pradeep</creatorcontrib><creatorcontrib>MAGLIA, Dominic J</creatorcontrib><creatorcontrib>KOZHIPURAM, Akhil Rajagopal</creatorcontrib><title>SUPPLEMENTAL RECLINE PANEL FOR AIRCRAFT CABIN ATTENDANT SEAT</title><description>A retrofit seat back assembly (150, 250, 350, 450) includes a supplemental recline panel (152, 252, 352, 452) having an upper end (241) and a lower end (242); a pivot member (275, 375, 475) disposed proximate the upper end (241) and configured to pivotally engage a seat back frame (114, 314, 414) of a stowable seat (100); an actuator (254, 354, 454) disposed proximate the lower end (242) and configured to operably engage the seat back frame (114, 314, 414) and move the supplemental recline panel (152, 252, 352, 452) between a retracted position and a deployed position; and a bias element (260, 360, 460) disposed between the supplemental recline panel (152, 252, 352, 452) and the seat back frame (114, 314, 414) and configured to urge the supplemental recline panel (152, 252, 352, 452) toward the seat back frame (114, 314, 414).</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>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLAJDg0I8HH1dfULcfRRCHJ19vH0c1UIcPRz9VFw8w9ScPQMcg5ydAtRcHZ08vRTcAwJcfVzcfQLUQh2dQzhYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGZiYGhsZmjobGRCgBAK5TKQU</recordid><startdate>20200422</startdate><enddate>20200422</enddate><creator>HOOVER, Douglas E</creator><creator>ACHARYA, Pradeep</creator><creator>MAGLIA, Dominic J</creator><creator>KOZHIPURAM, Akhil Rajagopal</creator><scope>EVB</scope></search><sort><creationdate>20200422</creationdate><title>SUPPLEMENTAL RECLINE PANEL FOR AIRCRAFT CABIN ATTENDANT SEAT</title><author>HOOVER, Douglas E ; ACHARYA, Pradeep ; MAGLIA, Dominic J ; KOZHIPURAM, Akhil Rajagopal</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3640136A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2020</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>HOOVER, Douglas E</creatorcontrib><creatorcontrib>ACHARYA, Pradeep</creatorcontrib><creatorcontrib>MAGLIA, Dominic J</creatorcontrib><creatorcontrib>KOZHIPURAM, Akhil Rajagopal</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HOOVER, Douglas E</au><au>ACHARYA, Pradeep</au><au>MAGLIA, Dominic J</au><au>KOZHIPURAM, Akhil Rajagopal</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SUPPLEMENTAL RECLINE PANEL FOR AIRCRAFT CABIN ATTENDANT SEAT</title><date>2020-04-22</date><risdate>2020</risdate><abstract>A retrofit seat back assembly (150, 250, 350, 450) includes a supplemental recline panel (152, 252, 352, 452) having an upper end (241) and a lower end (242); a pivot member (275, 375, 475) disposed proximate the upper end (241) and configured to pivotally engage a seat back frame (114, 314, 414) of a stowable seat (100); an actuator (254, 354, 454) disposed proximate the lower end (242) and configured to operably engage the seat back frame (114, 314, 414) and move the supplemental recline panel (152, 252, 352, 452) between a retracted position and a deployed position; and a bias element (260, 360, 460) disposed between the supplemental recline panel (152, 252, 352, 452) and the seat back frame (114, 314, 414) and configured to urge the supplemental recline panel (152, 252, 352, 452) toward the seat back frame (114, 314, 414).</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 | SUPPLEMENTAL RECLINE PANEL FOR AIRCRAFT CABIN ATTENDANT SEAT |
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