Abstract A propeller hub rotatable about an axis is provided with a plurality of airfoil surfaces peripherally arranged about the axis and defining a first pitch angle that is acute and adjustable with respect to the tangent on the circular arc described by rotation of the airfoil surface as seen in a plane perpendicular to the axis, and further by a second pitch angle being acute and ajustable and measured with respect to the axis of rotation within a plane containing the axis of rotation. Peripherally adjacent airfoil surfaces may have their first pitch angles oppositely oriented and second pitch angles oppositely oriented to respectively propel fluid inwardly and outwardly with respect to the axis of rotation. The air foil surfaces may be directly connected to the hub and extend conically outward or connected to the hub by means of arms that may be angled airfoil surfaces functioning as conventional screw propellers. The hub may be mounted coaxially adjacent a counter rotating screw.
A propeller for providng forward thrust to a body travelling at relatively high speed through a surrounding fluid medium, comprising: (a) a propeller hub having an axis of rotation; (b) a plurality of airfoil surfaces mounted to and distributed radially about said hub; the position of each said airfoil surface being defined by first and second pitch angles, respectively, said first pitch angle being the angle in the rotation direction between the profile longitudinal axis of said airfoil surface and a tangent on the circular arc described by the rotation of said airfoil surface about said propeller shaft, and said second pitch angle being the angle between the profile transversal axis of said airfoil and said axis or rotation, said second pitch angle being less than 90°, whereby the volume described by said rotation propeller is substantially conical in shape and wherein a large volume of said fluid medium is accelerated only slightly by said propeller, thereby resulting in a relatively high level of propeller efficiency; and (c) peripherally adjacent airfoil surfaces having oppositely oriented first pitch angles with respect to their tangents and oppositely oriented second pitch angles with respect to the axis of rotation, so that alternate airfoil surfaces will direct fluid radially outward, whereas the remaining airfoil surfaces will direct the fluid radially inward.
Claim 2
Dependent Claim
217 words
A propeller for providng forward thrust to a body travelling at relatively high speed through a surrounding fluid medium, comprising: (a) a propeller hub having an axis of rotation; (b) a plurality of airfoil surfaces mounted to and distributed radially about said hub; the position of each said airfoil surface being defined by first and second pitch angles, respectively, said first pitch angle being the angle in the rotation direction between the profile longitudinal axis of said airfoil surface and a tangent on the circular arc described by the rotation of said airfoil surface about said propeller shaft, and said second pitch angle being the angle between the profile transversal axis of said airfoil and said axis or rotation, said second pitch angle being less than 90°, whereby the volume described by said rotation propeller is substantially conical in shape and wherein a large volume of said fluid medium is accelerated only slightly by said propeller, thereby resulting in a relatively high level of propeller efficiency; and (c) peripherally adjacent airfoil surfaces having oppositely oriented first pitch angles with respect to their tangents and oppositely oriented second pitch angles with respect to the axis of rotation, so that alternate airfoil surfaces will direct fluid radially outward, whereas the remaining airfoil surfaces will direct the fluid radially inward.