System for aligning a propeller

Patent metadata

Field	Value
Publication number	US-10196150-B2
Application number	US-201715417658-A
Country	US
Kind code	B2
Filing date	Jan 27, 2017
Priority date	Aug 19, 2011
Publication date	Feb 5, 2019
Grant date	Feb 5, 2019

Abstract

A motor assembly that includes a motor ( 102 ) having a rotatable shaft, a hub coupled to the rotatable shaft, the hub having a propeller indexer to receive a propeller ( 104 ), when the propeller is present, a sensor trigger rotatable with the shaft ( 100 ) and positioned at a propeller offset angle θ PROP from the propeller indexer, and a sensor coupled to the motor and positioned to detect the sensor trigger so that the propeller indexer may be positioned at the propeller offset angle θ PROP from the sensor through rotation of the shaft so that said sensor is proximate to the sensor trigger.

First claim

What is claimed is:

1. A method, comprising:
rotating a sensor trigger by rotating a shaft of a motor;
sensing the sensor trigger as the sensor trigger rotates to a point adjacent a sensor fixedly coupled to a casing of the motor; and
holding a propeller in alignment with a wing of an aircraft by a control signal to the motor;
wherein the propeller is substantially aligned with the wing of the aircraft when the sensor trigger and the sensor are aligned.

2. The method of claim 1 , further comprising:
rotating the shaft of the motor in response to the sensor trigger drifting away from the sensor.

3. The method of claim 1 , further comprising:
receiving the propeller in a propeller indexer of a hub, the hub coupled to the shaft of the motor, wherein the sensor trigger is coupled to the hub and facing the motor.

4. An assembly, comprising:
a hub coupled to a rotatable shaft of a motor;
a propeller indexer of the hub, the propeller indexer to receive and align a propeller relative to the hub;
a first sensor trigger rotatable with the rotatable shaft of the motor; and
a sensor fixedly coupled to the motor;
wherein the propeller is substantially held in alignment with a wing of an aircraft by a control signal to the motor when the first sensor trigger and the sensor are aligned.

5. The assembly of claim 4 , wherein the first sensor trigger and the sensor are aligned when the propeller is in a horizontal position.

6. The assembly of claim 4 , wherein the first sensor trigger is positioned at a propeller offset angle from the propeller.

7. The assembly of claim 4 , wherein the first sensor trigger is coupled to the hub at an outer diameter of the hub.

8. The assembly of claim 7 , further comprising:
a weight coupled to the hub on a side of the hub opposite from the first sensor trigger to weightably balance the hub.

9. The assembly of claim 7 , further comprising:
a first sensor trigger cavity disposed on a back side of the hub, wherein the first sensor trigger is disposed in the first sensor trigger cavity.

10. The assembly of claim 7 , further comprising:
a second sensor trigger, wherein the second sensor trigger is disposed on an opposite side of the hub as the first sensor trigger to weightably balance the hub during rotation.

11. The assembly of claim 4 , wherein the first sensor trigger is facing the motor.

12. The assembly of claim 4 , wherein the first sensor trigger is a mirror.

13. The assembly of claim 12 , wherein the sensor is a light transceiver.

14. The assembly of claim 4 , wherein the sensor is fixedly coupled to an interior of a casing of the motor.

15. The assembly of claim 4 , wherein the sensor is fixedly coupled to an exterior surface of a casing of the motor.

16. The assembly of claim 4 , wherein the propeller indexer is a channel having a same width as the propeller, and wherein the channel is located on an exterior surface of the hub opposite from the motor.

17. The assembly of claim 16 , wherein the channel is formed through a lip portion of the hub having an angular transition between front and back sides of the hub.

18. The assembly of claim 16 , wherein the channel has one or more contoured side walls that prevent backwards installation of the propeller.

19. An assembly, comprising:
a sensor trigger rotatable with a rotatable shaft of a motor; and
a sensor fixedly coupled to a casing of the motor;
wherein the sensor trigger and the sensor are substantially held in alignment by a control signal to the motor when a propeller coupled to the rotatable shaft of the motor is in a horizontal position.

20. The assembly of claim 19 , wherein the sensor trigger is at least one of:
mounted on the propeller and mounted in the propeller.

21. The assembly of claim 19 , wherein the sensor trigger is a magnet.

22. The assembly of claim 19 , wherein the sensor is a Hall Effect sensor.

Assignees

• Aerovironment Inc

Inventors

• Firanski Jason Allen
• Mcallister Justin Bates
• Olch Ronald Howard
• Dalan Lane Dennis
• Ghapgharan Emil

Classifications

• B64C11/002

  Braking propellers, e.g. for measuring the power output of an engine · CPC title

• H02K29/10

  using light effect devices · CPC title

• H02P6/14

  Electronic commutators · CPC title

• H02K29/12

  using detecting coils {using the machine windings as detecting coil} · CPC title

• H02K29/08

  using magnetic effect devices, e.g. Hall-plates, magneto-resistors (H02K29/12 takes precedence) · CPC title