Folding heavy-lift unmanned aerial vehicle frame

• US 10,266,245 B2
• Filed: 09/15/2016
• Issued: 04/23/2019
• Est. Priority Date: 04/06/2016
• Status: Active Grant

• Current Assignee: Harris Aerial, LLC
• Original Assignee: Harris Aerial, LLC
• Inventors: Harris, Benjamin
• Primary Examiner(s): Collins, Timothy D
• Assistant Examiner(s): Abell, Tye William
• Application Number:
  US15/265,948
• Publication Number:
  US 20170291677A1
• Time in Patent Office: 950 Days
• CPC Class Codes: B64C 1/061 Frames
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 20/65 Composite materials
• CPC Class Codes: B64U 2101/60 for transporting passengers; for transporting goods other than weapons
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/293 Foldable or collapsible rotors or rotor supports

Abstract

A heavy-lift UAV frame includes a central frame portion having a symmetrical shape and forming a pocket area for receiving an avionics package. Top and bottom plates are secured to the central frame portion and include four corner members that extend diagonally outward therefrom. A plurality of boom arms are pivotally connected to the corner members and transition between an extended position for flight and a retracted position for storage and transport. Each boom arm includes a complementary dimension to one side of the central frame portion and is arranged parallel thereto when in the retracted position.

Claims

1. A UAV frame, comprising:

a symmetrical-shaped central body portion,

a top plate that is secured along a top portion of the central body portion, wherein the top plate comprises a plurality of top corner members extending diagonally outward from the central body portion;

a bottom plate that is secured along a bottom portion of the central body portion, wherein the bottom plate comprises a plurality of bottom corner members extending diagonally outward from the central body portion; and

a plurality of elongated boom arms, each of said boom arms including a first end that is pivotally connected to one of the plurality of top corner members along a top surface, and one of the plurality of bottom corner members along a bottom surface,

wherein each of the plurality of boom arms are configured to pivot between a retracted position and an extended position,

wherein the plurality of top corner members and the plurality of bottom corner members are outermost components of the frame when each of the plurality of boom arms are in the retracted position.

2. The frame of claim 1, wherein each of the plurality of top corner members further includes a latching mechanism that is disposed along a distal end thereof.

3. The frame of claim 2, wherein each of the plurality of elongated boom arms further includes a bracket that is disposed along the top surface at a location adjacent to the first end, said bracket and latching mechanisms being configured to be removably engaged so as to lock the frame into the extended position.

4. The frame of claim 1, wherein the symmetrical-shaped central body portion includes a square shape having a bottom wall and four side walls, each of said side walls including identical dimensions.

5. The frame of claim 4, wherein each of the plurality of boom arms includes a dimension that is complementary to a dimension of one of the four side walls of the central body portion, and

each of the plurality of boom arms are positioned parallel to one of the four side walls of the central body portion when the frame is in the retracted position.

6. The frame of claim 4, wherein the bottom wall is positioned along a bottom edge of each of the side walls forming a pocket area for receiving avionics.

7. The frame of claim 6, wherein the plurality of top and bottom corner members consist of:

four pairs of top and bottom corner members, each pair having a single top corner member and a single bottom corner member that are positioned parallel to the other.

8. The frame of claim 7, wherein the plurality of boom arms consists of:

four identical boom arms, each including a dimension that is complementary to a dimension of one of the four side walls of the central body portion, and being positioned parallel to one of the four side walls of the central body portion when the frame is in the retracted position.

9. The frame of claim 1, wherein the plurality of top corner members and the plurality of bottom corner members are outermost components from the center of the frame when each of the plurality of boom arms are in the retracted position.

10. A UAV frame, comprising:

a symmetrical-shaped central body portion,

a top plate that is secured along a top portion of the central body portion, wherein the top plate comprises a plurality of top corner members extending diagonally outward from the central body portion;

a bottom plate that is secured along a bottom portion of the central body portion, wherein the bottom plate comprises a plurality of bottom corner members extending diagonally outward from the central body portion; and

a plurality of elongated boom arms, each of said boom arms including a first end that is pivotally connected to one of the plurality of top corner members along a top surface, and one of the plurality of bottom corner members along a bottom surface,

wherein each of the plurality of boom arms are configured to pivot between a retracted position and an extended position;

wherein two adjacent top corner members and two adjacent bottom corner members are positioned to protect at least one boom arm against impact when the at least one boom arm is in the retracted position.