Heating elements for aircraft heated floor panels

A method for providing an electrical connection (107; 207; 307) for conductive ink (102; 202; 302) includes direct writing a bus bar (104; 204; 304) onto areas of a desired electrical connection of the conductive ink. The conductive ink is screen printed onto a dielectric film (106; 206; 306) to cre...

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Bibliographische Detailangaben
Hauptverfasser:	HAMM, RICHARD R, HU, JIN, ROACH, KEVIN E
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ELECTRIC HEATING ELECTRIC LIGHTING NOT OTHERWISE PROVIDED FOR ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PRINTED CIRCUITS
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Beschreibung
Zusammenfassung:	A method for providing an electrical connection (107; 207; 307) for conductive ink (102; 202; 302) includes direct writing a bus bar (104; 204; 304) onto areas of a desired electrical connection of the conductive ink. The conductive ink is screen printed onto a dielectric film (106; 206; 306) to create a conductive circuit. An aircraft heated floor panel (200) includes at least one floor panel (203) of an aircraft. The one floor panel includes a conductive circuit (201) having a conductive ink (202) including a bus bar (204) directly written onto areas of a desired electrical connection (207) of the conductive ink. The conductive ink is screen printed onto a dielectric film (206) to create a conductive circuit.