AIRCRAFT CABIN APPARATUS INCLUDING PERSONAL ELECTRONIC DEVICE HOLDER

An apparatus for an aircraft cabin may include a body and a personal electronic device (PED) holder. The body may include a sloped surface between a top surface and a recess surface with a plurality of recess protrusions configured to support a PED. The body may be couplable to a surface within the...

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Hauptverfasser:	WANNER, Jackson R, RAMOS, Rafael Z, RICHARDSON, David A
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS SEATS SPECIALLY ADAPTED FOR VEHICLES STANDS OR SUPPORTS THERMAL INSULATION IN GENERAL TRANSPORTING VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR VEHICLES IN GENERAL VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR WEAPONS
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creator	WANNER, Jackson R RAMOS, Rafael Z RICHARDSON, David A
description	An apparatus for an aircraft cabin may include a body and a personal electronic device (PED) holder. The body may include a sloped surface between a top surface and a recess surface with a plurality of recess protrusions configured to support a PED. The body may be couplable to a surface within the aircraft cabin via one or more couplers. The PED holder may include a paddle and at least one hinge coupler. The paddle may be located opposite the sloped surface within the recess. The paddle may be dimensioned to fit within the recess when the PED holder is in a closed position. The paddle may be configured to support the PED when the PED holder is in an open position. The PED holder may be configured to rotate about an axis through the at least one hinge coupler between at least the open position and the closed position.
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The body may include a sloped surface between a top surface and a recess surface with a plurality of recess protrusions configured to support a PED. The body may be couplable to a surface within the aircraft cabin via one or more couplers. The PED holder may include a paddle and at least one hinge coupler. The paddle may be located opposite the sloped surface within the recess. The paddle may be dimensioned to fit within the recess when the PED holder is in a closed position. The paddle may be configured to support the PED when the PED holder is in an open position. The PED holder may be configured to rotate about an axis through the at least one hinge coupler between at least the open position and the closed position.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINEERING ELEMENTS AND UNITS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; SEATS SPECIALLY ADAPTED FOR VEHICLES ; STANDS OR SUPPORTS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR ; VEHICLES IN GENERAL ; VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR ; WEAPONS</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&date=20231011&DB=EPODOC&CC=EP&NR=3594067B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231011&DB=EPODOC&CC=EP&NR=3594067B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WANNER, Jackson R</creatorcontrib><creatorcontrib>RAMOS, Rafael Z</creatorcontrib><creatorcontrib>RICHARDSON, David A</creatorcontrib><title>AIRCRAFT CABIN APPARATUS INCLUDING PERSONAL ELECTRONIC DEVICE HOLDER</title><description>An apparatus for an aircraft cabin may include a body and a personal electronic device (PED) holder. The body may include a sloped surface between a top surface and a recess surface with a plurality of recess protrusions configured to support a PED. The body may be couplable to a surface within the aircraft cabin via one or more couplers. The PED holder may include a paddle and at least one hinge coupler. The paddle may be located opposite the sloped surface within the recess. The paddle may be dimensioned to fit within the recess when the PED holder is in a closed position. The paddle may be configured to support the PED when the PED holder is in an open position. The PED holder may be configured to rotate about an axis through the at least one hinge coupler between at least the open position and the closed position.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>SEATS SPECIALLY ADAPTED FOR VEHICLES</subject><subject>STANDS OR SUPPORTS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR</subject><subject>VEHICLES IN GENERAL</subject><subject>VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBx9AxyDnJ0C1FwdnTy9FNwDAhwDHIMCQ1W8PRz9gl18fRzVwhwDQr293P0UXD1cXUOCfL383RWcHEN83R2VfDw93FxDeJhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcamliYGZuZOhsZEKAEAA08rag</recordid><startdate>20231011</startdate><enddate>20231011</enddate><creator>WANNER, Jackson R</creator><creator>RAMOS, Rafael Z</creator><creator>RICHARDSON, David A</creator><scope>EVB</scope></search><sort><creationdate>20231011</creationdate><title>AIRCRAFT CABIN APPARATUS INCLUDING PERSONAL ELECTRONIC DEVICE HOLDER</title><author>WANNER, Jackson R ; RAMOS, Rafael Z ; RICHARDSON, David A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3594067B13</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>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>SEATS SPECIALLY ADAPTED FOR VEHICLES</topic><topic>STANDS OR SUPPORTS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR</topic><topic>VEHICLES IN GENERAL</topic><topic>VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WANNER, Jackson R</creatorcontrib><creatorcontrib>RAMOS, Rafael Z</creatorcontrib><creatorcontrib>RICHARDSON, David A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WANNER, Jackson R</au><au>RAMOS, Rafael Z</au><au>RICHARDSON, David A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT CABIN APPARATUS INCLUDING PERSONAL ELECTRONIC DEVICE HOLDER</title><date>2023-10-11</date><risdate>2023</risdate><abstract>An apparatus for an aircraft cabin may include a body and a personal electronic device (PED) holder. The body may include a sloped surface between a top surface and a recess surface with a plurality of recess protrusions configured to support a PED. The body may be couplable to a surface within the aircraft cabin via one or more couplers. The PED holder may include a paddle and at least one hinge coupler. The paddle may be located opposite the sloped surface within the recess. The paddle may be dimensioned to fit within the recess when the PED holder is in a closed position. The paddle may be configured to support the PED when the PED holder is in an open position. The PED holder may be configured to rotate about an axis through the at least one hinge coupler between at least the open position and the closed position.</abstract><oa>free_for_read</oa></addata></record>
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language	eng ; fre ; ger
recordid	cdi_epo_espacenet_EP3594067B1
source	esp@cenet
subjects	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS SEATS SPECIALLY ADAPTED FOR VEHICLES STANDS OR SUPPORTS THERMAL INSULATION IN GENERAL TRANSPORTING VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR VEHICLES IN GENERAL VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR WEAPONS
title	AIRCRAFT CABIN APPARATUS INCLUDING PERSONAL ELECTRONIC DEVICE HOLDER
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