Granted Patent B2

US 12,448,098 · App. 18/739,753 · Granted Oct 21, 2025

Inventor: Gregory Charles Sharrow (Grosse Pointe Park, MI)

Assignee: Sharrow Engineering LLC

B63H1/265B64C11/00B64C11/005B64C11/16B64C11/18B64C11/20F01D5/141F03D1/06F03D1/0625F04D29/384F04D17/025F04D29/281F05B2210/16F05B2250/24F05B2250/25F05B2250/26

Abstract

Claims (16)

1. A propeller comprising:

a plurality of blades, each of the plurality of blades having an intake portion, an exhaust portion, and a tip portion extending from the intake portion to the exhaust portion;

a hub;

the plurality of blades, each blade forming a loop-extending outward from the hub and disposed around the hub, each blade connected with the hub via a root of the intake portion and a root of the exhaust portion, wherein the root of the exhaust portion is forward of the root of the intake portion when extending outward from the hub;

each blade comprising a plurality of parameter sections having selected one or more of the parameters including skew angle, roll angle, rake, radius, pitch angle, and vertical angle values;

a parameter section of the plurality of parameter sections at the transition from the intake portion to the tip portion defined by parameters to cause the amount of non-axial lift in the tip portion to be greater than the axial lift in the tip portion; and

a parameter section of the plurality of parameter sections or an area between consecutive parameter sections of the plurality of parameter sections in the tip portion having a roll value of 90 degrees.

2. The propeller of claim 1 comprising the plurality of blades each having an irregular helical median line.

3. The propeller of claim 1 wherein the plurality of blades are configured so non-axial lift in the intake portion is less than non-axial lift in tip portion.

4. The propeller of claim 1 wherein the plurality of blades are configured so the amount of non-axial lift in the exhaust portion is less than the non-axial lift in the tip portion.

5. The propeller of claim 1 wherein the tip portion has a 90 degree roll angle closer to the exhaust portion than to the intake portion.

6. The propeller of claim 1 , wherein the plurality of parameter sections include the root of the exhaust portion forward of the root of the intake portion when extending outward from the hub, and skew continually decreases.

7. The propeller of claim 1 , wherein the plurality of parameter sections are aligned along a non-helical median line.

8. The propeller of claim 1 , wherein one or more selected parameters for one or more of the plurality of parameter sections are defined to cause the amount of non-axial lift in the intake portion to be less than the non-axial lift in tip portion.

9. The propeller of claim 1 , wherein one or more selected parameters for one or more of the plurality of parameter sections are defined to cause the amount of non-axial lift in the exhaust portion to be less than the non-axial lift in the tip portion.

10. The propeller of claim 1 , wherein the plurality of parameter sections are planar.

Assignments (4)

Continuity (7)

References Cited (144)