Self-tightening rotor

Patent metadata

Field	Value
Publication number	US-9284040-B2
Application number	US-201514718021-A
Country	US
Kind code	B2
Filing date	May 20, 2015
Priority date	May 31, 2013
Publication date	Mar 15, 2016
Grant date	Mar 15, 2016

Abstract

Systems, methods, and devices for propelling self-propelled movable objects are provided. In one aspect, a rotor assembly for a self-propelled movable object comprises: a hub comprising a first fastening feature; a drive shaft comprising a second fastening feature and directly coupled to the hub by a mating connection of the first and second fastening features, wherein the drive shaft is configured to cause rotation of the hub such that the mating connection of the first and second fastening features is tightened by the rotation; and a plurality of rotor blades coupled to the hub and configured to rotate therewith to generate a propulsive force.

First claim

What is claimed is:

1. A multi-rotor self-propelled movable object, the movable object comprising:
(a) a first rotor assembly comprising:
a first hub coupled to a first plurality of blades;
a first adapter coupled to the first hub and comprising a first fastening feature; and
a first drive shaft comprising a second fastening feature and coupled to the first hub through the first adapter by a mating connection of the first and second fastening features, wherein the first drive shaft is configured to cause rotation of the first hub in a first direction, and the mating connection of the first and second fastening features is able to be tightened by the rotation of the first drive shaft in only the first direction,

wherein the first plurality of blades coupled to the first hub are configured to rotate therewith in the first direction to generate a first propulsive force; and
(b) a second rotor assembly comprising:
a second hub coupled to a second plurality of blades;
a second adapter coupled to the second hub and comprising a third fastening feature;
a second drive shaft comprising a fourth fastening feature and coupled to the second hub through the second adapter by a mating connection of the third and fourth fastening features, wherein the second drive shaft is configured to cause rotation of the second hub in a second direction that is opposite to the first direction, and the mating connection of the third and fourth fastening features is able to be tightened by the rotation of the second drive shaft in only the second direction,

wherein the second plurality of blades coupled to the second hub are configured to rotate therewith in the second direction to generate a second propulsive force,
wherein (1) the first fastening feature of the first adapter is threaded in a right-handed direction and the third fastening feature of the second adapter is threaded in a left-handed direction, or (2) the first fastening feature of the first adapter is threaded in a left-handed direction and the third fastening feature of the second adapter is threaded in a right-handed direction,
wherein the second fastening feature is threaded to mate with the first fastening feature of the first adapter, and the fourth fastening feature is threaded to mate with the third fastening feature,
wherein the first propulsive force (1) includes a lift component that provides lift to the movable object, and (2) is imparted via contact between the first hub, the first adapter and the first drive shaft; and wherein the second propulsive force (1) includes a lift component that provides lift to the movable object, and (2) is imparted via contact between the second hub, the second adapter and the second drive shaft, and
wherein the rotation of the first hub in the first direction imparts a rotational force component that is transmitted from the first drive shaft to the first hub via contact between the first fastening feature and the second fastening feature, and wherein the rotation of the second hub in the second direction imparts a rotational force component that is transmitted from the second drive shaft to the second hub via contact between the third fastening feature and the fourth fastening feature.

2. The movable object of claim 1 , wherein the self-propelled movable object is an unmanned aerial vehicle.

3. The movable object of claim 1 , wherein the first plurality of blades coupled to the first hub are integrally formed with the first hub or the second plurality of blades coupled to the second hub are integrally formed with the second hub.

4. The movable object of claim 1 , further comprising a drive unit configured to drive the first drive shaft or the second drive shaft, wherein the drive unit comprises a motor that rotates, thereby driving the first drive shaft or the second drive shaft.

5. The movable object of claim 1 , wherein the first adapter is formed from a material having greater durability than a material of the first hub, or the second adapter is formed from a material having greater durability than a material of the second hub.

6. The movable object of claim 1 , wherein the first fastening feature is integrally formed with the first adapter, or the third fastening feature is integrally formed with the second adapter.

7. The movable object of claim 1 , wherein the first adapter is coupled to a cavity of the first hub, or the second adapter is coupled to a cavity of the second hub.

8. The movable object of claim 7 , wherein the first adapter is coupled to the cavity of the first hub via a threaded connection, or the second adapter is coupled to the cavity of the second hub via a threaded connection.

9. The movable object of claim 1 , wherein the first adapter is fixedly coupled to the first hub, or the second adapter is fixedly coupled to the second hub.

10. The movable object of claim 9 , wherein the first adapter is not detachable from the first hub, or the second adapter is not detachable from the second hub.

11. The movable object of claim 1 , wherein the first adapter is releasably coupled to the first hub, or the second adapter is releasably coupled to the second hub.

12. The movable object of claim 1 , wherein the first adapter is coupled to at least one protrusion of the first hub, or the second adapter is coupled to at least one protrusion of the second hub.

13. The movable object of claim 12 , wherein the first adapter is coupled to the protrusion of the first hub via a threaded connection, or the second adapter is coupled to the protrusion of the second hub via a threaded connection.

14. The movable object of claim 1 , wherein the lift component of the first propulsive force (2) is imparted via contact between threads of the first adapter and threads of the first drive shaft; and wherein the lift component of the second propulsive force is imparted via contact between threads of the second adapter and threads of the second drive shaft.

15. The movable object of claim 1 , wherein the first hub further comprises a fifth fastening feature and the first adapter comprises a sixth fastening feature, such that the first adapter is coupled to the first hub by a mating connection of the fifth and sixth fastening features, and wherein the second hub further comprises a seventh fastening feature and the second adapter comprises an eighth fastening feature, such that the second adapter is coupled to the second hub by a mating connection of the seventh and eighth fastening features.

16. The movable object of claim 15 , wherein the mating connection of the fifth and sixth fastening features is able to be tightened by the rotation of the first drive shaft in only the first direction, and wherein the mating connection of the seventh and eighth fastening features is able to be tightened by the rotation of the second drive shaft in only the second direction.

17. A multi-rotor self-propelled movable object, the movable object comprising:
(a) a first rotor assembly comprising:
a first hub coupled to a first plurality of blades and comprising a first fastening feature;
a first adapter coupled to the first hub and comprising a second fastening feature; and
a first drive shaft coupled to the first hub through the first adapter by a mating connection of the first and second fastening features, wherein the first drive shaft is configured to cause rotation of the first hub in a first direction, and the mating connection of the first and second fastening features is able to be tightened by the rotation of the first drive shaft in only the first direction,

wherein the first plurality of blades coupled

Assignees

• Sz Dji Technology Co Ltd

Inventors

• Wang Tao
• Zhao Tao
• Ou Zhi Gang

Classifications

• B64C11/04 Primary

  Blade mountings · CPC title

• B64C27/14

  Direct drive between power plant and rotor hub · CPC title

• B64C11/02

  Hub construction · CPC title

• F01D5/021

  for flow machines or engines with only one axial stage (for more than one stage F01D5/06) · CPC title

• B64C27/32 Primary

  Rotors · CPC title