Automated variable pitch propeller blade

Patent metadata

Field	Value
Publication number	US-11352125-B2
Application number	US-202016844672-A
Country	US
Kind code	B2
Filing date	Apr 9, 2020
Priority date	Aug 9, 2016
Publication date	Jun 7, 2022
Grant date	Jun 7, 2022

Abstract

A variable pitch propeller is designed to adjust the pitch of the propeller blade during flight to maximize the propeller efficiency. The propeller blade may comprise airfoil cross-sections. Each cross-section may be composed of different materials at the leading edge and trailing edge. In various embodiments, these materials are selected and oriented to achieve the necessary elastic moduli of the leading and trailing edge for the airfoil cross-section. During liftoff, the airfoil at the blade tip possesses a high blade pitch (e.g. 20 degrees), thereby increasing the generated lift on the propeller blades. During flight or hover conditions when maximal lift is no longer required, the trailing edge of the airfoil displaces upward and reduces the blade pitch to minimize the drag forces on the blade tip.

First claim

What is claimed is:

1. A propeller blade comprising:
a first material corresponding to a chord line of the propeller blade; and
a second material different from the first material, the first material being interspersed through the second material, a volume fraction of the first material decreasing in non-continuous fashion from a leading edge of the propeller blade to a trailing edge of the propeller blade.

2. The propeller blade of claim 1 , wherein the volume fraction of the first material decreases from the leading edge of the propeller blade to the trailing edge of the propeller blade in a continuous fashion.

3. The propeller blade of claim 2 , wherein the continuous fashion comprises a decay model.

4. The propeller blade of claim 3 , wherein the decay model comprises any of exponential decay, logarithmic decay, and polynomial decay.

5. The propeller blade of claim 1 , wherein the non-continuous fashion comprises discrete sections with a constant volume fraction of the first material interspersed through the second material.

6. The propeller blade of claim 1 , wherein the first material corresponding to the chord line of the propeller blade comprises the first material traveling along the chord line of the propeller blade.

7. The propeller blade of claim 1 , wherein the first material corresponding to the chord line of the propeller blade comprises the first material traveling perpendicular to the chord line of the propeller blade.

8. The propeller blade of claim 1 , wherein the first material is interspersed as fibers through the second material.

9. The propeller blade of claim 1 , wherein the first material comprises any of carbon fiber and glass fiber and the second material comprises any of polycarbonate and nylon.

10. The propeller blade of claim 9 , wherein the volume fraction of the carbon fiber decreases linearly from 99% at the leading edge to 65% at the trailing edge.

11. The propeller blade of claim 9 , wherein the leading edge comprises 66% carbon fiber and 34% polycarbonate and the trailing edge comprises 4% carbon fiber and 96% polycarbonate.

12. The propeller blade of claim 1 , wherein the first material has a volume fraction greater than or equal to 66% interspersed as fibers through the second material.

13. The propeller blade of claim 1 , wherein the first material is interspersed as fibers through the second material at a higher volume fraction near the leading edge than the trailing edge.

14. A propeller blade comprising:
a first material; and
a second material different from the first material, the first material being interspersed through the second material, a volume fraction of the first material decreasing in non-continuous fashion from a first edge of the propeller blade to a second edge of the propeller blade.

15. The propeller blade of claim 14 , wherein the volume fraction of the first material decreases from the first edge to the second edge in a continuous fashion.

16. The propeller blade of claim 15 , wherein the continuous fashion comprises any of exponential decay, logarithmic decay, and polynomial decay.

17. The propeller blade of claim 14 , wherein the non-continuous fashion comprises discrete sections with a constant volume fraction of the first material interspersed through the second material.

18. The propeller blade of claim 14 , wherein the first material comprises carbon fiber and the second material comprises polycarbonate.

19. A propeller blade comprising:
a first material; and
a second material being interspersed through the first material, a volume fraction of the first material decreasing in non-continuous fashion from a first edge of the propeller blade to a second edge of the propeller blade.

Assignees

• Gopro Inc

Inventors

• Campbell Scott Patrick
• Baldwin Leo
• Fong Gary

Classifications

• B64C39/024

  of the remote controlled vehicle type, i.e. RPV · CPC title

• B64U10/13

  Flying platforms · CPC title

• B64U10/14

  with four distinct rotor axes, e.g. quadcopters · CPC title

• B64U30/20

  Rotors; Rotor supports · CPC title

• B64C11/26 Primary

  Fabricated blades · CPC title