Indirect motor drive train for RC vehicles

Patent metadata

Field	Value
Publication number	US-10689101-B2
Application number	US-201715416592-A
Country	US
Kind code	B2
Filing date	Jan 26, 2017
Priority date	Jan 27, 2016
Publication date	Jun 23, 2020
Grant date	Jun 23, 2020

Abstract

The present disclosure describes an indirect motor drive train for RC vehicles. Example embodiments include RC vehicles such as helicopters (and more specifically quadcopters) with a housing and housing arms that extend radially from the housing. Protected within each housing arm is a motor and indirect drive train. In operation, the drive train may include a first gear and a second gear with corresponding teeth that mesh together to translate motion from the motor axis to a propeller axis.

First claim

What is claimed is:

1. An RC rotorcraft comprising:
a housing comprising a plurality of housing arms extending radially outward from the housing;
wherein each of the plurality of housing arms at least partially encloses:
a motor with a motor output shaft that rotates around a motor axis of rotation;
a first gear coupled to the motor output shaft; and
a second gear;
wherein each second gear is coupled to a propeller drive shaft that rotates around a propeller axis of rotation that is not parallel to the motor axis of rotation;
wherein each first gear meshes with each second gear to translate motion between the motor axis of rotation and the propeller axis of rotation; and
wherein at least one propeller is coupled to each propeller drive shaft.

2. The RC rotorcraft of claim 1 , wherein motor axis of rotation and the propeller axis of rotation are orthogonal.

3. The RC rotorcraft of claim 1 , wherein the first gear is a pinion gear.

4. The RC rotorcraft of claim 1 , wherein the second gear is a spur gear or a bevel gear.

5. The RC rotorcraft of claim 1 , wherein the first axis motor axis of rotation is coplanar with a central axis of the housing arm.

6. The RC rotorcraft of claim 1 , wherein each of the plurality of housing arms comprises a first portion and a second portion.

7. The RC rotorcraft of claim 6 , wherein the motor, motor output shaft, first gear, and second gear of each of the plurality of housing arms are enclosed between the first portion and the second portion.

8. A quadcopter comprising:
a housing comprising four housing arms extending radially outward from the housing;
wherein each of the four housing arms at least partially encloses:
a motor with a motor output shaft that rotates around a motor axis of rotation;
a first gear coupled to the motor output shaft; and
a second gear;
wherein each second gear is coupled to a propeller drive shaft that rotates around a propeller axis of rotation that is not parallel to the motor axis of rotation;
wherein each first gear meshes with each second gear to translate motion between the motor axis of rotation and the second axis; and
wherein at least one propeller is coupled to each propeller drive shaft.

9. The quadcopter of claim 8 , wherein the motor axis of rotation and the propeller axis of rotation are orthogonal.

10. The quadcopter of claim 8 , wherein the first gear is a pinion gear.

11. The quadcopter of claim 8 , wherein the second gear is a spur gear or a bevel gear.

12. The quadcopter of claim 8 , wherein the motor axis of rotation is coplanar with a central axis of the housing arm.

13. The quadcopter of claim 8 , wherein each of the plurality of housing arms comprises a first portion and a second portion.

14. The quadcopter of claim 13 , wherein the motor, motor output shaft, first gear, and second gear of each of the plurality of housing arms are enclosed between the first portion and the second portion.

15. A quadcopter comprising:
a housing comprising at least one housing arm that extends radially outward from the housing;
wherein the at least one housing arm encloses:
a motor with a motor output shaft that rotates around a motor axis of rotation;
a first gear coupled to the motor output shaft; and
a second gear;
wherein the second gear is coupled to a propeller drive shaft that rotates around a propeller axis of rotation that is not parallel to the motor axis of rotation;
wherein the first gear meshes with the second gear to translate motion between the motor axis of rotation and the propeller axis of rotation; and
wherein a propeller is coupled to the propeller drive shaft.

16. The quadcopter of claim 15 , further comprising a shaft seal coupled to the propeller drive shaft.

17. The quadcopter of claim 15 , further comprising at least one bearing coupled to the propeller drive shaft.

18. The quadcopter of claim 15 , further comprising a motor housing configured to hold the motor in a fixed position relative to the housing.

19. The quadcopter of claim 18 , wherein the motor housing is coupled to the housing arm.

20. The quadcopter of claim 18 , wherein the motor fits within the motor housing such that the motor axis of rotation is coplanar with a central axis of the housing arm.

Assignees

• Horizon Hobby Llc

Inventors

• Haley James
• Eichstedt David

Classifications

• B64U2201/20

  Remote controls · CPC title

• B64U50/19 Primary

  using electrically powered motors · CPC title

• B64U10/14

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

• B64C27/14 Primary

  Direct drive between power plant and rotor hub · CPC title

• B64C2201/027

  Operations & Transport · mapped topic