HEATED AIRCRAFT FLOOR PANELS

An aircraft heated floor panel includes a first face sheet (106), a second face sheet (108) opposite the first face sheet, and core (110) with an electrically conductive core portion (112). The electrically conductive core portion supports the first face sheet and the second face sheet, and is elect...

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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 includes a first face sheet (106), a second face sheet (108) opposite the first face sheet, and core (110) with an electrically conductive core portion (112). The electrically conductive core portion supports the first face sheet and the second face sheet, and is electrically insulated from the external environment to receive electrical power, resistively generate heat, and communicate heat to the first face sheet.