Rotor centrifugal force retention device
AssigneeTextron Innovations Inc.
InventorsGeorge Matthew Thompson, Jonathan Andrew Knoll, Nicholas Carlson
Life of this patent
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AssigneeTextron Innovations Inc.
InventorsGeorge Matthew Thompson, Jonathan Andrew Knoll, Nicholas Carlson
Estimating the term…
A rotor blade retention device for use in an aircraft having a plurality of blades includes an array of cavities, each cavity adapted to receive a portion of a tension-torsion strap therein. Each cavity is oriented such that, when the portion of the tension-torsion strap is received therein, a central plane of the tension-torsion strap is inclined relative to a blade plane of rotation defined by the plurality of blades. The retention device may have a body that defines an aperture adapted to receive a portion of a rotor mast of the aircraft, may comprise a rotor mast of the aircraft, or may comprise first and second plates that cooperate to form the array of cavities and that are adapted to receive a portion of the rotor mast of the aircraft.
A propulsor for an aircraft, the propulsor comprising:
A rotor assembly for use in an aircraft, the assembly comprising:
A rotor blade retention assembly for use in an aircraft having a plurality of blades, the retention assembly comprising:
Dependencies are inferred from the claim text.