Aircraft propeller with improved electrically de-icer leads
AssigneeHartzell Propeller Inc.
InventorsDavid E. Ziegler, Arthur J. Bowser
Life of this patent
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Abstract
A multiple blade aircraft propeller hub has a bulkhead supporting concentric slip rings connected by slide blocks to the aircraft electrical system. Electrical conducting flexible leads connect the slip rings to electrical heating elements or de-icing boots carried by the propeller blades. Each of the leads includes an elongated flexible braided copper tube for conducting electricity and which loosely surrounds a flexible multiple strand stainless steel cable, and an extruded flexible vinyl insulating tube loosely surrounds the braided tube. The leads provide for minimizing stresses and metal fatigue in the electrical conducting braided tube with changes in blade pitch and thereby provide for a substantially extended service life.
Claims15
A propeller assembly for use on an aircraft having an electrical power supply system, said assembly comprising a propeller hub, a plurality of angularly disposed adjustable pitch propeller blades supported by said hub, an electrical heating element carried by each said blade for de-icing said blade, means for conducting electricity from the aircraft power supply system to said heating elements, said conducting means including a plurality of elongated flexible leads, each of said leads having an intermediate portion connecting opposite end portions and including an elongated flexible element, a flexible braided tube of electrical conducting material surrounding said flexible element, said braided tube having sufficient clearance with said flexible element to provide for free axial movement of said braided tube on said flexible element along said intermediate portion of said lead in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and electrical connecting means for said opposite end portions of said leads and connected to said flexible element and said braided tube.
A propeller assembly for use on an aircraft having an electrical power supply system, said assembly comprising a propeller hub, a plurality of angularly disposed adjustable pitch propeller blades supported by said hub, an electrical heating element carried by each said blade for de-icing said blade, means for conducting electricity from the aircraft power supply system to said heating elements, said conducting means including a plurality of elongated flexible leads, each of said leads having an intermediate portion connecting opposite end portions and including an elongated non-stretchable flexible cable having multiple twisted strands each having multiple twisted wires, a flexible braided tube of electrical conducting material surrounding said cable, said braided tube having sufficient clearance with said cable to provide for free axial movement of said braided tube on said cable along said intermediate portion of said lead in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and electrical connecting means for said opposite end portions of said leads and connected to said cable and said braided tube.
An improved elongated flexible lead adapted for use on an aircraft, said lead comprising an elongated non-stretchable flexible cable having multiple twisted strands each having multiple twisted wires and providing for a limited degree of flexibility, a flexible braided tube of electrical conducting material surrounding said cable, said braided tube having sufficient clearance with said cable to provide for free axial movement of said braided tube on said cable along the length of said cable in response to flexing of said lead, a flexible insulating tube of electrical insulation material surrounding said braided tube, and means connected to said braided tube for conducting electricity.
Dependencies are inferred from the claim text.