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...

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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:	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
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Beschreibung
Zusammenfassung:	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.