IP Library Granted Patent US 11,254,419
Granted Patent B2
US 11,254,419 · App. 17/001,391 · Granted Feb 22, 2022

Bistable pitch propeller system with bidirectional propeller rotation

Inventors: Damon Vander Lind (Alameda, CA); Todd Reichert (Mountain View, CA)
Assignee: Kitty Hawk Corporation
B64C11/325B64C11/18B64C11/343B64C11/46B64C27/08B64C27/467B64C27/80B64C29/02B64C2201/108
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Quick Facts
Patent No.
US 11,254,419
App. No.
17/001,391
Granted
Feb 22, 2022
Kind
B2
Abstract

A propeller includes a blade free to rotate. A first stop is positioned to mechanically engage one or both of a first portion of the blade and a first structure coupled to the blade when the blade is in a first position at a first end of the rotational range of motion. A second stop is positioned to mechanically engage one or both of a second portion of the blade and a second structure coupled to the blade when the blade is in a second position at a second end of the defined rotational range. The blade rotates to the first position against the first stop when the propeller is rotated in a first direction and to the second position against the second stop when the propeller is rotated in a second direction.

Claims (82)

1. A method, comprising:

receiving, from a user interface, a desired blade pitch for a first position, wherein the desired blade pitch is associated with a propeller which includes:

a blade free to rotate about a longitudinal axis of the blade within at least a defined range of motion;

a first mechanical stop positioned to engage mechanically one or both of a first portion of the blade and a first structure coupled mechanically to the blade when the blade is in the first position at a first end of said defined rotational range of motion; and

a second mechanical stop positioned to engage mechanically one or both of a second portion of the blade and a second structure coupled mechanically to the blade when the blade is in a second position at a second end of said defined rotational range of motion;

wherein the blade rotates to the first position against the first mechanical stop when the propeller is rotated in a first direction and the blade rotates to the second position against the second mechanical stop when the propeller is rotated in a second direction;

determining a new position for the first mechanical stop based at least in part on the desired blade pitch; and

setting a position control for the first mechanical stop to a value which corresponds to the new position.

2. The method of claim 1 , further comprising, prior to receiving the desired blade pitch for the first position:

determining that the first mechanical stop is in use; and

in the event it is determined that the first mechanical stop is in use, disabling, in the user interface, one or more controls associated with receiving the desired blade pitch for the first position.

3. The method of claim 1 , further comprising, prior to receiving the desired blade pitch for the first position:

determining that the first mechanical stop is not in use; and

in the event it is determined that the first mechanical stop is not in use, enabling one or more controls associated with receiving the desired blade pitch for the first position.

4. The method of claim 1 , further comprising, prior to determining the new position for the first mechanical stop:

determining that the first mechanical stop is in use; and

in the event it is determined that the first mechanical stop is in use, displaying a message indicating the desired blade pitch will not be immediately applied.

5. The method of claim 1 , further comprising, prior to determining the new position for the first mechanical stop:

determining that the first mechanical stop is not in use; and

in the event it is determined that the first mechanical stop is not in use, determining the new position for the first mechanical stop based at least in part on the desired blade pitch.

6. The method of claim 1 , wherein:

the first portion of the blade includes a first side of the blade; and

the second portion of the blade includes a second side of the blade.

7. The method of claim 1 , wherein the first mechanical stop includes a first blade stopper configured to mechanically stop a first side of the blade when the blade is in the first position.

8. The method of claim 1 , wherein the second mechanical stop includes a second blade stopper configured to mechanically stop a second side of the blade when the blade is in the second position.

9. The method of claim 1 , wherein:

the first portion of the blade includes a first side of the blade and the second portion of the blade includes a second side of the blade;

the first mechanical stop includes a first blade stopper configured to mechanically stop the first side of the blade when the blade is in the first position;

the second mechanical stop includes a second blade stopper configured to mechanically stop the second side of the blade when the blade is in the second position; and

a position of the first blade stopper is adjustable.

10. A method, comprising:

receiving, from a user interface, a desired mode for a first position, wherein the desired mode is selected from a plurality of modes and the desired mode is associated with a propeller which includes:

a blade free to rotate about a longitudinal axis of the blade within at least a defined range of motion;

a first mechanical stop positioned to engage mechanically one or both of a first portion of the blade and a first structure coupled mechanically to the blade when the blade is in the first position at a first end of said defined rotational range of motion; and

a second mechanical stop positioned to engage mechanically one or both of a second portion of the blade and a second structure coupled mechanically to the blade when the blade is in a second position at a second end of said defined rotational range of motion;

wherein the blade rotates to the first position against the first mechanical stop when the propeller is rotated in a first direction and the blade rotates to the second position against the second mechanical stop when the propeller is rotated in a second direction;

determining a new position for the first mechanical stop based at least in part on the desired mode; and

setting a position control for the first mechanical stop to a value which corresponds to the new position.

11. The method of claim 10 , further comprising, prior to receiving the desired mode for the first position:

determining if the first mechanical stop is in use; and

in the event it is determined that the first mechanical stop is in use, disabling, in the user interface, one or more controls associated with receiving the desired mode for the first position; and

in the event it is determined that the first mechanical stop is not in use, enabling the controls associated with receiving the desired mode for the first position.

12. The method of claim 10 , further comprising, prior to determining the new position for the first mechanical stop:

determining if the first mechanical stop is in use; and

in the event it is determined that the first mechanical stop is in use, displaying a message indicating the desired mode will not be immediately applied; and

in the event it is determined that the first mechanical stop is not in use, determine the new position for the first mechanical stop based at least in part on the desired mode.

13. The method of claim 10 , wherein:

the first portion of the blade includes a first side of the blade and the second portion of the blade includes a second side of the blade;

the first mechanical stop includes a first blade stopper configured to mechanically stop the first side of the blade when the blade is in the first position; and

the second mechanical stop includes a second blade stopper configured to mechanically stop the second side of the blade when the blade is in the second position.

14. The method of claim 10 , wherein:

the first portion of the blade includes a first side of the blade and the second portion of the blade includes a second side of the blade;

the first mechanical stop includes a first blade stopper configured to mechanically stop the first side of the blade when the blade is in the first position;

the second mechanical stop includes a second blade stopper configured to mechanically stop the second side of the blade when the blade is in the second position; and

a position of the first blade stopper is adjustable.

15. A system, comprising:

a communications interface configured to receive a desired mode for a first position, wherein the desired mode is selected from a plurality of modes and the desired mode is associated with a propeller which includes:

a blade free to rotate about a longitudinal axis of the blade within at least a defined range of motion;

a first mechanical stop positioned to engage mechanically one or both of a first portion of the blade and a first structure coupled mechanically to the blade when the blade is in the first position at a first end of said defined rotational range of motion; and

a second mechanical stop positioned to engage mechanically one or both of a second portion of the blade and a second structure coupled mechanically to the blade when the blade is in a second position at a second end of said defined rotational range of motion;

wherein the blade rotates to the first position against the first mechanical stop when the propeller is rotated in a first direction and the blade rotates to the second position against the second mechanical stop when the propeller is rotated in a second direction;

a processor coupled to the communications interface and configured to:

determine a new position for the first mechanical stop based at least in part on the desired mode; and

determine an instruction for setting a position control for the first mechanical stop to a value which corresponds to the new position.

16. The system of claim 15 , wherein the desired mode includes a desired blade pitch.

17. The system of claim 15 , wherein the processor is further configured to, prior to receiving the desired mode for the first position:

determine if the first mechanical stop is in use; and

in the event it is determined that the first mechanical stop is in use, disable, in a user interface, one or more controls associated with receiving the desired mode for the first position; and

in the event it is determined that the first mechanical stop is not in use, enable the controls associated with receiving the desired mode for the first position.

18. The system of claim 15 , wherein the processor is further configured to, prior to determining the new position for the first mechanical stop:

determine if the first mechanical stop is in use; and

in the event it is determined that the first mechanical stop is in use, display a message indicating the desired mode will not be immediately applied; and

in the event it is determined that the first mechanical stop is not in use, determine the new position for the first mechanical stop based at least in part on the desired mode.

19. The system of claim 15 , wherein:

the first portion of the blade includes a first side of the blade and the second portion of the blade includes a second side of the blade;

the first mechanical stop includes a first blade stopper configured to mechanically stop the first side of the blade when the blade is in the first position; and

the second mechanical stop includes a second blade stopper configured to mechanically stop the second side of the blade when the blade is in the second position.

20. The system of claim 15 , wherein:

the first portion of the blade includes a first side of the blade and the second portion of the blade includes a second side of the blade;

the first mechanical stop includes a first blade stopper configured to mechanically stop the first side of the blade when the blade is in the first position;

the second mechanical stop includes a second blade stopper configured to mechanically stop the second side of the blade when the blade is in the second position; and

a position of the first blade stopper is adjustable.

Assignments (4)
RELEASE OF SECURITY INTEREST Recorded May 22, 2023
From: ONE AERO, LLC
To: KITTY HAWK CORPORATION
Reel/Frame 063713/0367 →
SECURITY INTEREST Recorded Mar 25, 2022
From: KITTY HAWK CORPORATION
To: ONE AERO, LLC
Reel/Frame 059503/0382 →
SECURITY INTEREST Recorded Nov 4, 2021
From: KITTY HAWK CORPORATION
To: ONE AERO, LLC
Reel/Frame 058029/0610 →
SECURITY INTEREST Recorded Oct 22, 2020
From: KITTY HAWK CORPORATION
To: ONE AERO, LLC
Reel/Frame 054206/0714 →
Continuity (2)
Continuation 15225018 · Aug 1, 2016
Related Publication 20200385103A1 · Dec 10, 2020