DRONE CARGO HELICOPTER

• US 20140217230A1
• Filed: 02/05/2013
• Published: 08/07/2014
• Est. Priority Date: 02/05/2013
• Status: Abandoned Application

• Current Assignee: Biosphere Aerospace, LLC
• Original Assignee: Biosphere Aerospace, LLC
• Inventors: Helou, Elie Jr.
• Application Number:
  US13/759,953
• Publication Number:
  US 20140217230A1
• Time in Patent Office: Days
• US Class Current: 244/17.17
• CPC Class Codes: B64C 2025/325 specially adapted for helicopters
• CPC Class Codes: B64C 25/14 fore-and-aft
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/10 Rotorcrafts
• CPC Class Codes: B64U 10/17 Helicopters flying platforms B64U10/13
• CPC Class Codes: B64U 2101/60 for transporting passengers; for transporting goods other than weapons
• CPC Class Codes: B64U 30/24 Coaxial rotors
• CPC Class Codes: B64U 60/40 foldable or retractable

Abstract

A drone cargo helicopter having an elongated body. The elongated body has a low profile and has a front portion, a rear portion, an upper surface, a lower surface and a pair of opposing sides extending between the front and the rear portions. At least a first blade set is coupled to the upper surface and rotating in a first direction. Two or more struts are pivotally coupled to opposing sides or lower surface of the elongated body, the struts being coupled via a joint at a top end of the strut. The lower surface of the elongated body comprises a substantially planar surface between the front and rear portions, the substantially planar surface having one or more attachments to provide a rigid engagement with a container. The struts are pivotally movable between a first position and a second position, wherein in the first position, the struts support the elongated body a distance from a ground surface that is greater than a height of the container.

Claims

1. A drone cargo helicopter comprising:

an elongated body having a low profile and comprising a front portion, a rear portion, an upper surface, a lower surface and a pair of opposing sides extending between the front and the rear portions;

at least a first blade set coupled to the upper surface and rotating in a first direction; and

two or more struts pivotally coupled to opposing sides or lower surface of the elongated body, the struts being coupled to the elongated body via a joint at a top end of the strut;

wherein the lower surface of the elongated body comprises a substantially planar surface between the front and rear portions, the substantially planar surface having one or more attachments to provide a rigid and fixed engagement with a container;

wherein the struts are pivotally movable between a first position and a second position; and

wherein in the first position, the struts support the elongated body a distance from a ground surface that is greater than a height of the container.

2. The drone cargo helicopter of claim 1, further comprising a second blade set coupled to the upper surface of the elongated body, the second blade set rotating in a second direction that opposes the first direction of the first blade set.

3. The drone cargo helicopter of claim 2, wherein the first and second blade sets are positioned on the elongated body in a side-by-side configuration and have separate axes of rotation.

4. The drone cargo helicopter of claim 2, wherein the first and second blade sets are stacked and share a single axis of rotation.

5. The drone cargo helicopter of claim 1, wherein the struts each further comprises a wheel coupled to a bottom end of the strut.

6. The drone cargo helicopter of claim 5, wherein the struts each further comprises a hydraulic piston to adjust the distance of the elongated body from the ground surface when the struts are in the first position between a first distance that is greater than the height of the container and a second distance that is equal to or less than the height of the container.

7. The drone cargo helicopter of claim 1, wherein in the second position, the struts are substantially positioned adjacent and substantially parallel to the sides of the elongated body.

8. The drone cargo helicopter of claim 1, further comprising a fuel tank disposed within the elongated body.

9. The drone cargo helicopter of claim 1, further comprising a fuel tank disposed externally of the elongated body.

10. The drone cargo helicopter of claim 1, wherein the attachments provide the rigid engagement between the elongated body and the container along at least four substantially opposing corners of the elongated body.

11. The drone cargo helicopter of claim 1 further comprising one or both of a forward fairing and an aft fairing coupled to the elongated body at the front portion and the rear portion, respectively.

12. A drone cargo helicopter comprising:

an elongated body comprising a front portion, a rear portion, an upper surface, a lower surface and a pair of opposing sides extending between the front and the rear portions;

at least a first blade set coupled to the upper surface, the first blade set rotating in a first direction; and

two or more telescoping struts coupled to the elongated body, the struts configured to be actuated between a first extended configuration a second retracted configuration;

wherein in the first extended configuration, the elongated body is supported at a distance above the ground surface; and

wherein the lower surface of the elongated body comprises a substantially planar surface between the front and rear portions, the substantially planar surface having one or more attachments to provide a rigid engagement with a container.

13. The drone cargo helicopter of claim 12, wherein the struts are coupled to either the opposing sides of the elongated body or the lower surface of the elongated body.

14. The drone cargo helicopter of claim 12, wherein in the first extended position, the struts support the elongated body at a distance from the ground that is greater than a height of the container.

15. The drone cargo helicopter of claim 12, wherein joints couple the struts to the elongated body, the joints actuating the struts between a first position for actuation of the struts to the first extended configuration and a second position to substantially position the retracted strut adjacent to and substantially parallel the sides of the elongated body for flight.

16. The drone cargo helicopter of claim 15, wherein the elongated body further comprises an internal cavity between the upper and lower surface of the elongated body and wherein the struts are retracted into the internal cavity after or simultaneously with actuating the struts to a second position.

17. The drone cargo helicopter of claim 12 further comprising one or both of a forward fairing and an aft fairing coupled to the elongated body at the front portion and the rear portion, respectively.

18. The drone cargo helicopter of claim 12, further comprising a deployable anti-radar skirt that is configured to cover the peripheral surfaces of a container attached to the elongated body.

19. A drone cargo helicopter comprising:

an elongated body comprising a front portion, a rear portion, an upper surface, a lower surface and a pair of opposing sides extending between the front and the rear portions, wherein the lower surface comprises a substantially planar attachment area between the front and rear portions configured to rigidly attach a container;

at least two blades coupled to the upper surface, the two blades rotating in opposing directions; and

two or more struts coupled to either one of the lower surface or the opposing sides of the elongated body, the struts being actuated between a first position and a second position, wherein in the first position, the struts support the elongated body above a ground surface to receive a couple one or more containers and wherein in the second position, the struts are either telescopically retracted or pivotally positioned adjacent to and substantially parallel to the sides of the elongated body.

20. A drone cargo helicopter wherein the attachment area comprises attachments configured attach the container along at least four corners of the attachment area.