Propeller

1. A propeller for use with fluids, the propeller provided to propel an object or person or to move the fluid, the propeller comprising:

a plurality of blades;

a means for generating non-axial lift and non-axial fluid flow;

a means for redirecting the non-axial fluid flow to axial fluid flow;

a rotational axis coincident with a hub;

the plurality of blades extending radially outward from the rotational axis and disposed around the rotational axis;

each blade forming a loop and having an intake portion, an exhaust portion and a tip portion extending radially outward from the rotational axis;

wherein the means for generating non-axial lift and non-axial fluid flow is the blades being configured wherein in a cross-sectional profile taken perpendicularly from the rotational axis through the tip portion of each of the plurality of blades, the distance from the rotational axis to the leading edge of the blade is greater than the distance from the rotational axis to the trailing edge of the blade in at least part of the tip portion, each of the plurality of blades has a roll value of 40 degrees to 50 degrees at a transition point from the intake portion to the tip portion, wherein the transition point occurs where the amount of non-axial lift produced by a given parameter section is greater that the axial lift produced; and

wherein the means for redirecting the non-axial fluid flow to axial fluid flow includes a vertical angle between −45 degrees and 45 degrees throughout the blade.

2. The propeller of claim 1 wherein the tip portion of the blades includes a blade section having a roll angle of ninety degrees.

3. The propeller of claim 1 wherein the blades have an irregular helical median line.

4. The propeller of claim 1 wherein:

the intake portion is defined by a plurality of parameter sections, each of the plurality of the parameter sections in the intake portion having a roll value; and

wherein the roll values for the plurality of parameter sections in the intake portion of the blades progress from zero to between about 1 degree to 35 degrees where the intake portion transitions to the tip portion and the intake portion encompasses between 0 percent and 45 percent of the blade.

5. The propeller of claim 4 wherein a roll range of the plurality of parameter sections in the intake portion is from zero to between about 5 degrees to 25 degrees.

6. The propeller of claim 1 wherein the tip portion of the blades produces more non-axial lift than either the intake or the exhaust portion.

7. The propeller of claim 1 wherein the roll value of parameter sections of the blades in the tip portion transition from less than 90 degrees to greater than 90 degrees.

8. The propeller of claim 1 wherein the tip portion of the blades has a non-zero pitch angle throughout.

9. The propeller of claim 1 wherein non-axial lift of the blades is generated by 10 percent to 75 percent of the blade.

10. The propeller of claim 1 wherein the pitch angle of the blades is positive throughout the blade.

11. The propeller of claim 1 wherein throughout at least a portion of the tip portion of the blades before a 90 degree roll and toward the intake end of the tip section, the distance (N) to the nose of a cross-section as measured perpendicularly from the rotational axis is greater than the distance (T) to the tail of the cross-section as measured perpendicularly from the rotational axis.

12. The propeller of claim 11 wherein average pitch angle of the exhaust section of the blades is greater than the average pitch of the intake section.

13. The propeller of claim 1 wherein the intake root rake position of the blades is less than the exhaust root rake position resulting in a gap between the intake root and the exhaust root.

14. The propeller of claim 1 wherein the intake root of the blades is forward of the exhaust root and skew begins at zero and ends at a positive value.

15. The propeller of claim 1 wherein pitch angle of the exhaust portion of the blades at its root end is greater than pitch angle of the intake blade at its root end.

16. The propeller of claim 1 wherein the blades have a closed loop structure.

17. The propeller of claim 1 wherein each blade section has a roll angle in the intake blade portion range from zero at or near the first root end area, increases to the tip portion to about 90 degrees at a tip portion blade section, and increases through the exhaust portion to about 180 degrees at or near the second root.

18. The propeller of claim 1 wherein roll angles of blade sections of the blades from the intake root to the exhaust root are 0 to 180 degrees.

19. A device having a propeller according to claim 1 selected from the group consisting of, jet engines, propulsors, shrouded propellers, encased propellers, impellers, aircraft, watercraft, turbines, including wind turbines, cooling devices, heating devices, automobile engines, unmanned aerial vehicles, turbofans (hydrojets), air circulation devices, compressors, and pump jets.

20. The propeller of claim 1 wherein vertical angles throughout the tip portion of the blades is zero.

21. The propeller of claim 1 wherein pitch angle of the exhaust portion of the blade at its root end for the blades is less than pitch angle of the intake portion at its root end.

22. The propeller of claim 1 defined by planar parameter sections.

23. The propeller of claim 1 where the intake portion has a higher average pitch value than the average pitch value of the exhaust portion.

24. The propeller of claim 1 wherein the transition from the intake portion to the tip portion occurs when the amount of non-axial lift produced by a given parameter section of the blade is greater than the axial lift produced.

25. A propeller of claim 1 wherein the range of values for vertical angle for any given parameter section is between negative 45 degrees to 45 degrees.

26. The propeller of claim 1 wherein rake values of the blades decrease from the intake root and in the intake portion of the blade and increase in the exhaust portion of the blade.