초록 ▼

A propeller attached to an output shaft of a boat motor is provided. The propeller may have a plurality of blades which define a leading edge. The leading edge may define leading edge angles which increase in a logarithmic manner from a base of the blade to a tip of the blade. This allows the blades

A propeller attached to an output shaft of a boat motor is provided. The propeller may have a plurality of blades which define a leading edge. The leading edge may define leading edge angles which increase in a logarithmic manner from a base of the blade to a tip of the blade. This allows the blades of the propeller to cut and shed seaweed and/or kelp off of the blades when the boat is maneuvered into waters containing seaweed and/or kelp. Additionally, boats that employ the propeller of the present invention are quieter compared to boats that utilize prior art propellers.

대표청구항 ▼

What is claimed is: 1. A propeller for a motor of a boat, the motor having a rotating output shaft extending along a propeller axis, the propeller comprising: a hub connectable to the rotating output shaft; and a plurality of blades, each blade including: a concave blade base connected to the hub;

What is claimed is: 1. A propeller for a motor of a boat, the motor having a rotating output shaft extending along a propeller axis, the propeller comprising: a hub connectable to the rotating output shaft; and a plurality of blades, each blade including: a concave blade base connected to the hub; and a blade body portion connected to the blade base, the blade body portion having a leading edge and a trailing edge each extending from the blade base and intersecting at a blade tip, the leading edge being sized and configured in the shape of a logarithmic spiral, the trailing edge being linear and extending along an axis offset from intersection with the propeller axis; wherein a leading edge angle of the leading edge increases logarithmically from the concave blade base to the tip of the blade, the leading edge angle being defined by a tangent line to the leading edge and a radial line from a center of the propeller to the intersection of the tangent line to the leading edge. 2. The propeller of claim 1 wherein the leading edge angle at the blade base is at least 27 degrees. 3. The propeller of claim 1 wherein the blades are fabricated from urethane plastic. 4. The propeller of claim 1 wherein cross sections of each blade has a thickness ratio of about 12%, the thickness ratio being defined by a ratio of a maximum thickness of the cross section and a chord length of the cross section. 5. The propeller of claim 1 wherein cross sections of each blade has a percentage camber of less than 3%, the percentage camber defined by a ratio of the largest distance between a mean chord line and a mean camber line to a chord length of the cross section. 6. The propeller of claim 1 having five blades. 7. The propeller of claim 6 wherein the five blades are attached to the hub and angularly equidistantly spaced apart from each other. 8. The propeller of claim 1, wherein the blade body portion further includes: front and rear surfaces extending between the leading and trailing edges. 9. The propeller of claim 8, wherein the blade base further includes: a forward base portion extending between the forward surface to the hub, the forward base portion defining a concave forward base surface; and a rear base portion extending between the rear surface to the hub, the rear base portion defining a concave rear base surface. 10. The propeller of claim 1, wherein the logarithmic spiral being characterized by the following equation, r=aebθ, wherein r is the radial line, a and b are constants, and θ is an angle defined by the trailing edge axis and the radial line. 11. A propeller for a motor of a boat, the motor having a rotating output shaft, the propeller comprising: a hub connectable to the rotating output shaft; and a plurality of blades, each blade including: a blade body portion; a concave blade base extending between the blade body portion and the hub, the concave blade base smoothly extending onto the exterior surface of the hub; a leading edge extending between the concave blade base and a blade tip, the leading edge being sized and configured in the shape of a logarithmic spiral, each blade having a radial cross section being orthogonal to the leading edge, the radial cross section having a cross section periphery in the shape of an airfoil defining an angle of attack that increases from the blade tip to the blade base; and a trailing edge extending linearly between the blade tip and the blade base, the trailing edge being non-orthogonal to the tangent of the hub at the intersection of the hub and the axis along which the trailing edge extends; wherein a leading edge angle of the leading edge increases logarithmically from the blade base to the blade tip, the leading edge angle being defined by a tangent line to the leading edge and a radial line from a center of the propeller to the intersection of the tangent line to the leading edge. 12. The propeller of claim 11, wherein the blade base further includes: front and rear surfaces extending between the leading and trailing edges; a forward base portion extending between the forward surface to the hub, the forward base portion defining a concave forward base surface; and a rear base portion extending between the rear surface to the hub, the rear base portion defining a concave rear base surface. 13. The propeller of claim 11, wherein the logarithmic spiral being characterized by the following equation, r=aebθ, wherein r is the radial line, a and b are constants, and θ is an angle defined by the trailing edge axis and the radial line. 14. The propeller of claim 11 wherein the leading edge angle at the blade base is at least 27 degrees. 15. The propeller of claim 14 wherein cross sections of each blade has a thickness ratio of about 12%, the thickness ratio being defined by a ratio of a maximum thickness of the cross section and a chord length of the cross section. 16. The propeller of claim 11 wherein cross sections of each blade has a thickness ratio of about 12%, the thickness ratio being defined by a ratio of a maximum thickness of the cross section and a chord length of the cross section. 17. The propeller of claim 11 wherein cross sections of each blade has a percentage camber of less than 3%, the percentage camber defined by a ratio of the largest distance between a mean chord line and a mean camber line to a chord length of the cross section. 18. The propeller of claim 1, wherein the trailing edge is non-orthogonal to the tangent of the hub at the intersection of the hub and the axis along which the trailing edge extends. 19. The propeller of claim 11, wherein the rotating output shaft extends along a propeller axis and the trailing edge extends along an axis offset from intersection with the propeller axis.