"ROTOR BLADE DE-ICING SYSTEM"

An aircraft includes a heat absorbent material carried by an airfoil susceptible to ice buildup and a transmitter spaced apart from the heat absorbent material. A method includes the process of transmitting the heat energy from the transmitter to the heat absorbent material that in turn warms the ai...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	MCCOLLOUGH, JAMES, M, AUBERT, ROGER
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BORING COSMONAUTICS ELECTRIC HEATING ELECTRIC LIGHTING NOT OTHERWISE PROVIDED FOR ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS TRANSPORTING TURNING
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Beschreibung
Zusammenfassung:	An aircraft includes a heat absorbent material carried by an airfoil susceptible to ice buildup and a transmitter spaced apart from the heat absorbent material. A method includes the process of transmitting the heat energy from the transmitter to the heat absorbent material that in turn warms the airfoil to break apart ice buildup.