US 4,307,535 AGranted

Aerodynamic device

AssigneeStanley W. Wilcox

InventorLucian D. Martin

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Abstract

An aerodynamic device for being launched for flight through the air and having three inherent parameters of rotation while moving through the air, the first being a yawing vector imparted by the launcher as the device rotates about its own center of symmetry, the second being a roll vector as it rotates about an axis parallel to its direction of flight, and the third being rotation of the device very slowly about a center which is determined by the launching point whereby a boomerang action is provided. The device comprises a substantially annular body having three symmetrically disposed lobes extending radially outwardly therefrom, with each lobe being of a substantially undulated cross-sectional configuration to provide a subtle lateral curvature for the device which is critical to the flight behavior thereof, the lateral curvature of the lobes providing a lifting surface for sustaining the device in a state of levitation during movement through the air, and a reverse curvature at the tips of the lobes providing stabilization and control of the roll flight axis of the device.

Claims2

Dependent claims

An aerodynamic device for launching by hand in which a spinning motion is imparted to the device as it is launched, comprising:

a unitary annular body of relatively thin and rigid material for rotation about an axis, the body having a large axial opening therein and being defined by at least three integral increased radial length lobe portions, each lobe being defined in cross-section in a plane of the rotational axis by a convex upper surface and concave lower surface adjacent the axial opening, such surfaces gradating towards the outer end portions of the lobe which has a reverse curvature formed by an upper slightly concave surface and a lower slightly convex surface, and wherein the portions of the body intermediate the lobe portions are of shorter radial length and are defined in cross-section in a plane of the rotational axis by a convex upper surface and concave lower surface, the surfaces of the intermediate portions gradating to the lobe portions providing smooth aerodynamic transitions in all portions of the body, the body being symmetrical as to all cross-sections taken in a plane parallel the rotational axis and perpendicular a radius extending through each lobe portion or a radius extending through each portion intermediate adjacent lobes.

Dependencies are inferred from the claim text.