FOLDABLE ROTOR BLADE ASSEMBLY AND AERIAL VEHICLE WITH A FOLDABLE ROTOR BLADE ASSEMBLY

• US 20190210718A1
• Filed: 01/09/2019
• Published: 07/11/2019
• Est. Priority Date: 01/10/2018
• Status: Active Grant

• Current Assignee: Hangzhou Zero Zero Technology Co.Ltd (Shenzhen Zero Zero Infinite Technology Co. Ltd.)
• Original Assignee: Hangzhou Zero Zero Technology Co.Ltd (Shenzhen Zero Zero Infinite Technology Co. Ltd.)
• Inventors: Wang, Zhaozhe
• Granted Patent: US 11,008,095 B2
• Time in Patent Office: Days
• CPC Class Codes: B64C 2027/7211 without flaps
• CPC Class Codes: B64C 27/39 with individually articulated blades, i.e. with flapping or drag hinges
• CPC Class Codes: B64C 27/48 Root attachment to rotor head
• CPC Class Codes: B64C 27/72 Means acting on blades
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 20/80 Arrangement of on-board electronics, e.g. avionics systems or wiring
• CPC Class Codes: B64U 30/293 Foldable or collapsible rotors or rotor supports
• CPC Class Codes: B64U 50/19 using electrically powered motors

Abstract

An aerial vehicle is described herein. The aerial vehicle includes a lift mechanism that includes a rotor blade assembly coupled to a motor assembly. The rotor blade assembly includes a plurality of rotor blades that are pivotably coupled to a rotor blade clamping mechanism. The rotor blade clamping mechanism includes an upper paddle clamp that is coupled to a lower paddle clamp. The upper paddle clamp includes a center protrusion and a plurality of blade support protrusions extending outwardly from the lower outer surface. The center protrusion includes a center shaft aperture sized and shaped to receive a motor shaft therein. Each blade support protrusion is sized and shaped to be inserted through a corresponding positioning aperture of a corresponding rotor blade. The lower paddle clamp includes a central recess to receive the center protrusion therein and a plurality of blade recesses to receive a corresponding blade support protrusion therein.

Claims

1. An unmanned aerial vehicle, comprising:

a fuselage body; and

a lift mechanism coupled to the fuselage body, the lift mechanism including;

a motor assembly including a rotor and a stator operatively coupled to the rotor for rotating the rotor about a rotor centerline axis, the rotor including a blade assembly support member and a motor shaft extending outwardly from the blade assembly support member along the rotor centerline axis; and

a rotor blade assembly coupled to the rotor, the rotor blade assembly including;

a plurality of rotor blades, each rotor blade extending between a root portion and a tip portion, the root portion including a positioning aperture extending through the root portion; and

a rotor blade clamping mechanism including;

an upper paddle clamp including;

an upper support body including an upper outer surface and a lower outer surface; and

,

a plurality of blade support protrusions extending outwardly from the lower outer surface, each of the blade support protrusions configured to be inserted through a corresponding positioning aperture of a corresponding rotor blade to facilitate pivotably coupling the corresponding rotor blade to the upper paddle clamp, each blade support protrusion having a length that is greater than a thickness of the root portion of the corresponding rotor blade, wherein each blade support protrusion includes a blade fastener positioning aperture configured to receive a blade fastener; and

a lower paddle clamp including;

a lower support body; and

a plurality of apertures defined along an outer surface of the lower support body, each aperture in the outer surface of the lower support body being aligned with a respective blade fastener positioning aperture for receiving the respective blade fastener, the upper and lower support bodies forming a gap configured to receive the root portion of a respective rotor blade, the gap having a predefined distance, the upper and lower paddle clamps forming a center shaft aperture configured to receive the motor shaft therethrough.

2. The unmanned aerial vehicle of claim 1, wherein the predefined distance associated with the gap is greater than the thickness of the root portion of the corresponding rotor blade.

3. The unmanned aerial vehicle of claim 1, wherein the lower paddle clamp includes a plurality of blade recesses defined along the outer surface of the lower support body, each blade recess configured to receive a corresponding blade support protrusion therein.

4. The unmanned aerial vehicle of claim 1, wherein the lower paddle clamp includes a pair of opposing support flanges extending outwardly from the lower support body in opposite directions.

5. The unmanned aerial vehicle of claim 1, wherein the blade assembly support member includes a plurality of positioning openings, each positioning opening includes a threaded inner surface configured to receive a corresponding rotor blade assembly fastener therethrough to facilitate coupling the rotor blade assembly to the rotor.

6. The unmanned aerial vehicle of claim 1, wherein the upper paddle clamp includes a center protrusion extending outwardly from the lower outer surface, the center protrusion including a upper center shaft aperture extending therethrough, the lower paddle clamp includes a central recess defined along an outer surface of the lower support body, the central recess configured to receive the center protrusion therein, wherein the lower paddle clamp further includes a lower center shaft aperture extending through the lower support body and defined within the central recess, the upper center shaft aperture and the lower center shaft aperture forming the center shaft aperture.

7. The unmanned aerial vehicle of claim 1, wherein the lower support body includes a blade fastener aperture defined through each blade recess and configured to receive a corresponding blade fastener therein, each blade fastener aperture including a threaded interior surface configured to engage a threaded outer surface of the corresponding blade fastener to facilitate coupling the upper paddle clamp to the lower paddle clamp.

8. The unmanned aerial vehicle of claim 1, wherein each blade fastener positioning aperture extends through the upper outer surface of the upper support body.

9. The unmanned aerial vehicle of claim 8, wherein the upper outer surface includes a plurality of fastener recesses, each fastener recess is orientated coaxially with a corresponding blade fastener positioning aperture and is configured to receive a corresponding blade fastener therein such that a top surface of the corresponding blade fastener is substantially flush with the upper outer surface.

10. The unmanned aerial vehicle of claim 6, wherein the center protrusion and each blade support protrusion has the same length.

11. The unmanned aerial vehicle of claim 6, wherein the center protrusion has a larger diameter than each of the blade support protrusions.

12. The unmanned aerial vehicle of claim 6, wherein the central recess and each blade recess has the same depth.

13. A rotor blade assembly for use with unmanned aerial vehicle including a fuselage body and a lift mechanism coupled to the fuselage body, the lift mechanism including a motor assembly including a motor shaft, the rotor blade assembly including:

a plurality of rotor blades, each rotor blade extending between a root portion and a tip portion, the root portion including a positioning aperture extending through the root portion; and

a rotor blade clamping mechanism including;

an upper paddle clamp including;

an upper support body including an upper outer surface and a lower outer surface; and

,

a plurality of blade support protrusions extending outwardly from the lower outer surface, each of the blade support protrusions configured to be inserted through a corresponding positioning aperture of a corresponding rotor blade to facilitate pivotably coupling the corresponding rotor blade to the upper paddle clamp, each blade support protrusion having a length that is greater than a thickness of the root portion of the corresponding rotor blade, wherein each blade support protrusion includes a blade fastener positioning aperture configured to receive a blade fastener; and

a lower paddle clamp including;

a plurality of apertures defined along an outer surface of the lower support body, each aperture in the outer surface of the lower support body being aligned with a respective blade fastener positioning aperture for receiving the respective blade fastener, the upper and lower support bodies forming a gap configured to receive the root portion of a respective rotor blade, the gap having a predefined distance, the upper and lower paddle clamps forming a center shaft aperture configured to receive the motor shaft therethrough.

14. The rotor blade assembly of claim 13, wherein the predefined distance associated with the gap is greater than the thickness of the root portion of the corresponding rotor blade.

15. The rotor blade assembly of claim 13, wherein the lower paddle clamp includes a plurality of blade recesses defined along the outer surface of the lower support body, each blade recess configured to receive a corresponding blade support protrusion therein.

16. The rotor blade assembly of claim 13, wherein the lower paddle clamp includes a pair of opposing support flanges extending outwardly from the lower support body in opposite directions.

17. The rotor blade assembly of claim 13, wherein the blade assembly support member includes a plurality of positioning openings, each positioning opening includes a threaded inner surface configured to receive a corresponding rotor blade assembly fastener therethrough to facilitate coupling the rotor blade assembly to the rotor.

18. The rotor blade assembly of claim 13, wherein the upper paddle clamp includes a center protrusion extending outwardly from the lower outer surface, the center protrusion including a upper center shaft aperture extending therethrough, the lower paddle clamp includes a central recess defined along an outer surface of the lower support body, the central recess configured to receive the center protrusion therein, wherein the lower paddle clamp further includes a lower center shaft aperture extending through the lower support body and defined within the central recess, the upper center shaft aperture and the lower center shaft aperture forming the center shaft aperture.

19. The rotor blade assembly of claim 13, wherein the lower support body includes a blade fastener aperture defined through each blade recess and configured to receive a corresponding blade fastener therein, each blade fastener aperture including a threaded interior surface configured to engage a threaded outer surface of the corresponding blade fastener to facilitate coupling the upper paddle clamp to the lower paddle clamp.

20. The rotor blade assembly of claim 13, wherein each blade fastener positioning aperture extends through the upper outer surface of the upper support body.

21. The rotor blade assembly of claim 20, wherein the upper outer surface includes a plurality of fastener recesses, each fastener recess is orientated coaxially with a corresponding blade fastener positioning aperture and is configured to receive a corresponding blade fastener therein such that a top surface of the corresponding blade fastener is substantially flush with the upper outer surface.

22. The rotor blade assembly of claim 18, wherein the center protrusion and each blade support protrusion has the same length.

23. The rotor blade assembly of claim 18, wherein the center protrusion has a larger diameter than each of the blade support protrusions.

24. The rotor blade assembly of claim 18, wherein the central recess and each blade recess has the same depth.