Rotor assembly and unmanned aerial vehicle having the same

Patent metadata

Field	Value
Publication number	US-11999470-B2
Application number	US-202117236423-A
Country	US
Kind code	B2
Filing date	Apr 21, 2021
Priority date	Sep 25, 2015
Publication date	Jun 4, 2024
Grant date	Jun 4, 2024

Abstract

A rotor assembly includes a propeller, a motor, and a connection assembly. The motor includes a stator and a rotator rotatable with respect to the stator. The connection assembly is configured to connect the propeller to the motor and includes a locking member that is arranged between the propeller and the motor. The locking member is configured to rotate with respect to the rotator and the propeller in a rotation direction identical to a rotation direction of the propeller in operation to lock the propeller to the motor.

First claim

What is claimed is:

1. A rotor assembly, comprising:
a propeller;
a motor including a stator and a rotator rotatable with respect to the stator, the rotator including a housing; and
a connection assembly configured to connect the propeller to the motor and including a locking member arranged between the propeller and the housing;
wherein the propeller is mounted on the housing and configured to not rotate with respect to the housing, and the locking member is configured to rotate with respect to the housing and the propeller to lock the propeller to the motor.

2. The rotor assembly of claim 1 , wherein:
the propeller includes a locking block;
the locking member includes at least one latch corresponding to the locking block; and
the at least one latch of the locking member is configured to couple with the locking block of the propeller to lock the propeller to the motor.

3. The rotor assembly of claim 2 , wherein:
the propeller includes a seat and one or more blades each fixed to the seat, the one or more blades including a first blade and a second blade; and
the locking block is provided on the seat and arranged between the first blade and the second blade, wherein the locking block is closer to the first blade than to the second blade.

4. The rotor assembly of claim 3 , wherein:
a number of the at least one latch corresponds to a number of the one or more blades.

5. The rotor assembly of claim 3 , wherein:
in response to a rotation of the locking member, the at least one latch is moved along a direction, away from the second blade and toward the first blade, to engage with the locking block to lock the propeller to the motor.

6. The rotor assembly of claim 5 , wherein:
if the one or more blades are counterclockwise rotating blades, the direction is counterclockwise direction; and
if the one or more blades are clockwise rotating blades, the direction is clockwise direction.

7. The rotor assembly of claim 2 , wherein:
the locking block of the propeller is a first locking block;
the at least one latch includes a second locking block at an end of the at least one latch, the second locking block extending toward a rotation axis of the propeller; and
the second locking block is configured to engage with the first locking block to lock the propeller to the motor.

8. The rotor assembly of claim 7 , wherein:
the first locking block includes a first fitting surface configured to engage with a second fitting surface of the second locking block; and
an end of the first fitting surface, proximal to the rotation axis, is closer to the motor than an end of the first fitting surface distal from the rotation axis to form an inclined angle with respect to the rotation axis.

9. The rotor assembly of claim 1 , wherein:
the connection assembly further includes a restrainer arranged between the propeller and the locking member, the restrainer being configured to fix to the motor to rotatably couple the locking member with the motor and preventing the locking member from moving along a rotation axis of the propeller.

10. The rotor assembly of claim 9 , wherein:
the restrainer includes a boss configured to couple with the propeller to restrain a relative rotation between the propeller and the restrainer about the rotation axis.

11. The rotor assembly of claim 9 , wherein:
the connection assembly further includes an elastic member arranged between the locking member and the motor, and configured to fix, through the restrainer, to the motor.

12. The rotor assembly of claim 11 , wherein:
the connection assembly further includes a bolt; and
the bolt is configured to penetrate the restrainer and the elastic member to connect with the motor, the locking member being rotatably arranged between the restrainer and the elastic member.

13. The rotor assembly of claim 11 , wherein:
in response to a rotation of the locking member, a portion of the locking member is moved to a position to elastically abut against a portion of the elastic member to restrain a movement of the locking member.

14. The rotor assembly of claim 11 , wherein:
the locking member includes a bulge;
the elastic member includes an elastic protrusion corresponding to the bulge; and
the bulge is configured to slide on a surface of the elastic protrusion to enable a portion of the elastic protrusion to restrain a movement of the bulge.

15. The rotor assembly of claim 14 , wherein:
the surface of the elastic protrusion includes a smooth curve.

16. The rotor assembly of claim 14 , wherein:
the elastic member further includes:
a connecting portion configured to fix, through the restrainer, to the housing; and
an elastic tab protruding toward the locking member with respect to a surface of the connecting portion of the elastic member, the elastic protrusion being formed by bending the elastic tab.

17. An unmanned aerial vehicle (UAV) comprising:
one or more rotor assemblies each including:
a propeller;
a motor including a stator and a rotator rotatable with respect to the stator, the rotator including a housing; and
a connection assembly configured to connect the propeller to the motor and including a locking member arranged between the propeller and the housing;
wherein the propeller is mounted on the housing and configured to not rotate with respect to the housing, and the locking member is configured to rotate with respect to the housing and the propeller to lock the propeller to the motor.

18. The UAV of claim 17 , further comprising:
a body; and
an arm connecting one of the one or more rotor assemblies to the body.

19. The UAV of claim 18 , wherein:
the arm includes a main arm and a branch arm;
one end of the main arm is connected to the body and another end of the main arm is connected to the branch arm; and
the one of the one or more rotor assemblies is positioned at an end of the branch arm.

20. The rotor assembly of claim 1 , wherein the propeller includes a locking block and a seat, the locking block protruding from a side surface of the seat and extending a length along a circumference of the seat.

Assignees

• Sz Dji Technology Co Ltd

Inventors

• Ye Fangming

Classifications

• B64D35/026

  the electric power plant being integral with the propeller or rotor · CPC title

• B64D35/02

  specially adapted for specific power plants · CPC title

• B64C39/024

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

• B64C27/08

  with two or more rotors · CPC title

• B64U30/20

  Rotors; Rotor supports · CPC title