HEATED AIRCRAFT FLOOR PANELS

An aircraft heated floor panel, comprising a first face sheet (106), a second face sheet (108) opposite the first face sheet, a core (110) with an insulating core portion (124, 126) and a conductive core portion (112), and a lead (102, 104) electrically connected to the conductive core portion, wher...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ROACH, Kevin E, MULLEN, James, WILSON, Tom, VERONESI, William A, BRITTINGHAM, David L, GIAMATI, Michael J, GESNER, Jason, WINESDOERFFER, Joseph, OWENS, George, TWISK, James V, GURVICH, Mark R, HU, Jin, SHEARER, Jon
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 ROACH, Kevin E
MULLEN, James
WILSON, Tom
VERONESI, William A
BRITTINGHAM, David L
GIAMATI, Michael J
GESNER, Jason
WINESDOERFFER, Joseph
OWENS, George
TWISK, James V
GURVICH, Mark R
HU, Jin
SHEARER, Jon
description An aircraft heated floor panel, comprising a first face sheet (106), a second face sheet (108) opposite the first face sheet, a core (110) with an insulating core portion (124, 126) and a conductive core portion (112), and a lead (102, 104) electrically connected to the conductive core portion, wherein the insulating core portion separates the conductive core portion from the first face sheet, wherein the insulating core portion and the conductive core portion both supporting the first face sheet and the second face sheet, and wherein the conductive core portion is electrically insulated from the external environment by the first and second faces to resistively heat the first face sheet.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3210881B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3210881B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3210881B13</originalsourceid><addsrcrecordid>eNrjZJDxcHUMcXVRcPQMcg5ydAtRcPPx9w9SCHD0c_UJ5mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxkaGBhYWhk6GxkQoAQAhYSA3</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>HEATED AIRCRAFT FLOOR PANELS</title><source>esp@cenet</source><creator>ROACH, Kevin E ; MULLEN, James ; WILSON, Tom ; VERONESI, William A ; BRITTINGHAM, David L ; GIAMATI, Michael J ; GESNER, Jason ; WINESDOERFFER, Joseph ; OWENS, George ; TWISK, James V ; GURVICH, Mark R ; HU, Jin ; SHEARER, Jon</creator><creatorcontrib>ROACH, Kevin E ; MULLEN, James ; WILSON, Tom ; VERONESI, William A ; BRITTINGHAM, David L ; GIAMATI, Michael J ; GESNER, Jason ; WINESDOERFFER, Joseph ; OWENS, George ; TWISK, James V ; GURVICH, Mark R ; HU, Jin ; SHEARER, Jon</creatorcontrib><description>An aircraft heated floor panel, comprising a first face sheet (106), a second face sheet (108) opposite the first face sheet, a core (110) with an insulating core portion (124, 126) and a conductive core portion (112), and a lead (102, 104) electrically connected to the conductive core portion, wherein the insulating core portion separates the conductive core portion from the first face sheet, wherein the insulating core portion and the conductive core portion both supporting the first face sheet and the second face sheet, and wherein the conductive core portion is electrically insulated from the external environment by the first and second faces to resistively heat the first face sheet.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; DOMESTIC HOT-WATER SUPPLY SYSTEMS ; DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATINGSYSTEMS ; ELEMENTS OR COMPONENTS THEREFOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; RANGES ; TRANSPORTING ; VENTILATING ; WEAPONS</subject><creationdate>2019</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=20190807&amp;DB=EPODOC&amp;CC=EP&amp;NR=3210881B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20190807&amp;DB=EPODOC&amp;CC=EP&amp;NR=3210881B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ROACH, Kevin E</creatorcontrib><creatorcontrib>MULLEN, James</creatorcontrib><creatorcontrib>WILSON, Tom</creatorcontrib><creatorcontrib>VERONESI, William A</creatorcontrib><creatorcontrib>BRITTINGHAM, David L</creatorcontrib><creatorcontrib>GIAMATI, Michael J</creatorcontrib><creatorcontrib>GESNER, Jason</creatorcontrib><creatorcontrib>WINESDOERFFER, Joseph</creatorcontrib><creatorcontrib>OWENS, George</creatorcontrib><creatorcontrib>TWISK, James V</creatorcontrib><creatorcontrib>GURVICH, Mark R</creatorcontrib><creatorcontrib>HU, Jin</creatorcontrib><creatorcontrib>SHEARER, Jon</creatorcontrib><title>HEATED AIRCRAFT FLOOR PANELS</title><description>An aircraft heated floor panel, comprising a first face sheet (106), a second face sheet (108) opposite the first face sheet, a core (110) with an insulating core portion (124, 126) and a conductive core portion (112), and a lead (102, 104) electrically connected to the conductive core portion, wherein the insulating core portion separates the conductive core portion from the first face sheet, wherein the insulating core portion and the conductive core portion both supporting the first face sheet and the second face sheet, and wherein the conductive core portion is electrically insulated from the external environment by the first and second faces to resistively heat the first face sheet.</description><subject>AEROPLANES</subject><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>DOMESTIC HOT-WATER SUPPLY SYSTEMS</subject><subject>DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATINGSYSTEMS</subject><subject>ELEMENTS OR COMPONENTS THEREFOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>RANGES</subject><subject>TRANSPORTING</subject><subject>VENTILATING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJDxcHUMcXVRcPQMcg5ydAtRcPPx9w9SCHD0c_UJ5mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxkaGBhYWhk6GxkQoAQAhYSA3</recordid><startdate>20190807</startdate><enddate>20190807</enddate><creator>ROACH, Kevin E</creator><creator>MULLEN, James</creator><creator>WILSON, Tom</creator><creator>VERONESI, William A</creator><creator>BRITTINGHAM, David L</creator><creator>GIAMATI, Michael J</creator><creator>GESNER, Jason</creator><creator>WINESDOERFFER, Joseph</creator><creator>OWENS, George</creator><creator>TWISK, James V</creator><creator>GURVICH, Mark R</creator><creator>HU, Jin</creator><creator>SHEARER, Jon</creator><scope>EVB</scope></search><sort><creationdate>20190807</creationdate><title>HEATED AIRCRAFT FLOOR PANELS</title><author>ROACH, Kevin E ; MULLEN, James ; WILSON, Tom ; VERONESI, William A ; BRITTINGHAM, David L ; GIAMATI, Michael J ; GESNER, Jason ; WINESDOERFFER, Joseph ; OWENS, George ; TWISK, James V ; GURVICH, Mark R ; HU, Jin ; SHEARER, Jon</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3210881B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</creationdate><topic>AEROPLANES</topic><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>DOMESTIC HOT-WATER SUPPLY SYSTEMS</topic><topic>DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATINGSYSTEMS</topic><topic>ELEMENTS OR COMPONENTS THEREFOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>RANGES</topic><topic>TRANSPORTING</topic><topic>VENTILATING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ROACH, Kevin E</creatorcontrib><creatorcontrib>MULLEN, James</creatorcontrib><creatorcontrib>WILSON, Tom</creatorcontrib><creatorcontrib>VERONESI, William A</creatorcontrib><creatorcontrib>BRITTINGHAM, David L</creatorcontrib><creatorcontrib>GIAMATI, Michael J</creatorcontrib><creatorcontrib>GESNER, Jason</creatorcontrib><creatorcontrib>WINESDOERFFER, Joseph</creatorcontrib><creatorcontrib>OWENS, George</creatorcontrib><creatorcontrib>TWISK, James V</creatorcontrib><creatorcontrib>GURVICH, Mark R</creatorcontrib><creatorcontrib>HU, Jin</creatorcontrib><creatorcontrib>SHEARER, Jon</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ROACH, Kevin E</au><au>MULLEN, James</au><au>WILSON, Tom</au><au>VERONESI, William A</au><au>BRITTINGHAM, David L</au><au>GIAMATI, Michael J</au><au>GESNER, Jason</au><au>WINESDOERFFER, Joseph</au><au>OWENS, George</au><au>TWISK, James V</au><au>GURVICH, Mark R</au><au>HU, Jin</au><au>SHEARER, Jon</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>HEATED AIRCRAFT FLOOR PANELS</title><date>2019-08-07</date><risdate>2019</risdate><abstract>An aircraft heated floor panel, comprising a first face sheet (106), a second face sheet (108) opposite the first face sheet, a core (110) with an insulating core portion (124, 126) and a conductive core portion (112), and a lead (102, 104) electrically connected to the conductive core portion, wherein the insulating core portion separates the conductive core portion from the first face sheet, wherein the insulating core portion and the conductive core portion both supporting the first face sheet and the second face sheet, and wherein the conductive core portion is electrically insulated from the external environment by the first and second faces to resistively heat the first face sheet.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3210881B1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
DOMESTIC HOT-WATER SUPPLY SYSTEMS
DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATINGSYSTEMS
ELEMENTS OR COMPONENTS THEREFOR
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HEATING
HELICOPTERS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
RANGES
TRANSPORTING
VENTILATING
WEAPONS
title HEATED AIRCRAFT FLOOR PANELS
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T23%3A26%3A05IST&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=ROACH,%20Kevin%20E&rft.date=2019-08-07&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3210881B1%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