Marine propeller with winglets and method of design thereof
A propeller for a marine propulsion device comprises a hub extending along an x-axis and a plurality of blades, each having a blade root attached to the hub and extending radially outwardly from the x-axis toward a respective blade tip. Each blade comprises a y-axis extending radially outwardly from and perpendicular with respect to the x-axis. Each blade also comprises a z-axis extending perpendicularly to both the x- and y-axes. Each blade comprises a winglet with a plurality of winglet sections proximate its blade tip, the winglet sections beginning at a given radial location on the blade and ending at the blade tip. Each winglet section on each blade is rotated about the blade's z-axis such that the blade tip is offset between about 1 degree and about 90 degrees from a surface of the blade that is radially inwardly of and adjacent to the given radial location.
1 . A propeller for a marine propulsion device, the propeller comprising:
a hub extending along an x-axis; and
a plurality of blades, each blade in the plurality of blades having a blade root non-pivotably attached to the hub and extending radially outwardly from the x-axis toward a respective blade tip;
wherein each blade in the plurality of blades comprises a y-axis extending radially outwardly from and perpendicular with respect to the x-axis;
wherein each blade in the plurality of blades comprises a z-axis extending perpendicularly to both the x- and y-axes;
wherein each blade in the plurality of blades comprises a plurality of winglet sections proximate its blade tip, the plurality of winglet sections beginning at a given radial location on the blade and ending at the blade tip, wherein the given radial location on each blade is between about 90% to about 99% of a radius of the propeller;
wherein each winglet section in the plurality of winglet sections of each blade is rotated about the blade's z-axis such that the blade tip is offset between about 1 degree and about 90 degrees from a surface of the blade that is radially inwardly of and adjacent to the given radial location; and
wherein the blade tip of each blade is rotated about the blade's z-axis by between about 1 degree and about 5 degrees.
2 . The propeller of claim 1 , wherein the blade tip is offset between about 1 degree and about 70 degrees from the surface of the blade that is radially inwardly of and adjacent to the given radial location.
3 . The propeller of claim 2 , wherein the blade tip is offset between about 1 degree and about 50 degrees from the surface of the blade that is radially inwardly of and adjacent to the given radial location.
4 . The propeller of claim 3 , wherein the blade tip is offset between about 1 degree and about 30 degrees from the surface of the blade that is radially inwardly of and adjacent to the given radial location.
5 . The propeller of claim 1 , wherein the blade tip is offset toward a pressure side of the blade.
6 . The propeller of claim 1 , wherein the blade tip is offset toward a suction side of the blade.
7 . A propeller for a marine propulsion device, the propeller comprising:
a hub extending along an x-axis; and
a plurality of blades, each blade in the plurality of blades having a blade root non-pivotably attached to the hub and extending radially outwardly from the x-axis toward a respective blade tip;
wherein each blade in the plurality of blades comprises a y-axis extending radially outwardly from and perpendicular with respect to the x-axis;
wherein each blade in the plurality of blades comprises a z-axis extending perpendicularly to both the x- and y-axes;
wherein each blade in the plurality of blades comprises a plurality of winglet sections proximate its blade tip, each winglet section in the plurality of winglet sections being rotated about the blade's z-axis;
wherein the blade tip of each blade in the plurality of blades is rotated about the blade's z-axis by between about 1 degree and about 5 degrees;
wherein the plurality of winglet sections on each blade begins at a given radial location on the blade and ends at the blade tip; and
wherein the given radial location is between about 90% to about 99% of a radius of the propeller.
8 . The propeller of claim 7 ,
wherein the blade tip on each blade is offset between about 1 degree and about 90 degrees from a surface of the blade that is radially inwardly of and adjacent to the given radial location.
9 . The propeller of claim 8 , wherein the blade tip is offset between about 1 degree and about 70 degrees from the surface of the blade that is radially inwardly of and adjacent to the given radial location.
10 . The propeller of claim 9 , wherein the blade tip is offset between about 1 degree and about 50 degrees from the surface of the blade that is radially inwardly of and adjacent to the given radial location.
11 . The propeller of claim 10 , wherein the blade tip is offset between about 1 degree and about 30 degrees from the surface of the blade that is radially inwardly of and adjacent to the given radial location.
12 . The propeller of claim 7 , wherein the blade tip is rotated toward a pressure side of the blade.
13 . The propeller of claim 7 , wherein the blade tip is rotated toward a suction side of the blade.