Offset Drag Reduction Device

Patent metadata

Field	Value
Publication number	US-2026054863-A1
Application number	US-202418778637-A
Country	US
Kind code	A1
Filing date	Jul 19, 2024
Priority date	Oct 4, 2023
Publication date	Feb 26, 2026
Grant date	—

Abstract

In one aspect an uncrewed aerial vehicle (UAV) is provided. The uncrewed aerial vehicle includes a fuselage and a drag reduction device. The fuselage has a front end, a rear end, a top, and a bottom. The drag reduction device includes a proximal end and a distal end. The proximal end of the drag reduction device is coupled to the bottom of the fuselage. The drag reduction device is rotatable between a rest position and an active position in which the drag reduction device extends downward. A standoff is disposed on a rear side of the drag reduction device and is configured to engage a payload secured under the fuselage and hold the drag reduction device at a distance from the payload when the drag reduction device is in the active position.

First claim

What is claimed is:

1 . An uncrewed aerial vehicle (UAV) comprising:
a fuselage having a front end, a rear end, a top, and a bottom; a drag reduction device including a proximal end and a distal end, wherein the proximal end of the drag reduction device is coupled to the bottom of the fuselage, and wherein the drag reduction device is rotatable between a rest position and an active position in which the drag reduction device extends downward; and a standoff disposed on a rear side of the drag reduction device and configured to engage a payload secured under the fuselage and hold the drag reduction device at a distance from the payload when the drag reduction device is in the active position.

2 . The UAV of claim 1 , wherein the drag reduction device is also rotatable to a cruise position in which the distal end of the drag reduction device is further rearward relative to the fuselage than when in the active position.

3 . The UAV of claim 1 , wherein the drag reduction device is also rotatable to a landing position in which the drag reduction device extends forward and the distal end of the drag reduction device is higher relative to the fuselage than when in the rest position.

4 . The UAV of claim 1 , wherein a body of the drag reduction device is in the form of a plate having a front surface and a rear surface, and wherein the standoff extends from the rear surface of the plate.

5 . The UAV of claim 4 , wherein the drag reduction device includes a rib on the rear surface of the plate that extends along an outer perimeter of the plate.

6 . The UAV of claim 1 , wherein the standoff includes a pair of feet that are spaced apart and disposed on opposing halves of the drag reduction device.

7 . The UAV of claim 1 , wherein a contact surface of the standoff is curved with respect to a side view of the UAV.

8 . The UAV of claim 1 , further comprising a bracket mounted to the fuselage, wherein the bracket holds the drag reduction device.

9 . A drag reduction system comprising:
a bracket configured to mount to a fuselage of an uncrewed aerial vehicle; a drag reduction device including a proximal end attached to the bracket and a distal end, wherein the drag reduction device is rotatable between a rest position and an active position in which the drag reduction device extends substantially downward from the bracket; and a standoff disposed on a rear side of the drag reduction device and configured to engage a payload when the drag reduction system is mounted to the fuselage, the payload is secured under the fuselage, and the drag reduction device is in the operating position, such that the drag reduction device is spaced from the payload.

10 . The drag reduction system of claim 9 , wherein the drag reduction device is also rotatable to a cruise position in which the distal end of the drag reduction device is further rearward relative to the bracket than when in the active position.

11 . The drag reduction system of claim 9 , wherein the drag reduction device is also rotatable to a landing position in which the drag reduction device extends forward and a distal end of the drag reduction device is higher relative to the bracket than when in the rest position.

12 . The drag reduction system of claim 9 , wherein a body of the drag reduction device is in the form of a plate having a front surface and a rear surface, and wherein the standoff extends from the rear surface of the plate.

13 . The drag reduction system of claim 10 , wherein the drag reduction device includes a rib on the rear surface of the plate that extends along an outer perimeter of the plate.

14 . The drag reduction system of claim 9 , wherein the standoff includes a pair of feet that are spaced apart and disposed on opposing halves of the drag reduction device.

15 . The drag reduction system of claim 9 , wherein a contact surface of the standoff is curved with respect to a side view of the UAV.

16 . A method of transporting a payload using an uncrewed aerial vehicle (UAV), the method comprising:
securing a payload under a fuselage of the UAV; operating the UAV in a lift mode with a drag reduction device that is coupled to the UAV in a rest position such that the drag reduction device extends substantially forward; and operating the UAV in a forward flight mode with the drag reduction device in an active position and with a standoff that is attached to a rear side of the drag reduction device engaging the payload so as to hold the drag reduction device at a distance from the payload.

17 . The method of claim 16 , wherein the drag reduction device is coupled to the fuselage by a spring that holds the drag reduction device in the rest position, and wherein air resistance moves the drag reduction device from the rest position to the active position during the forward flight mode of the UAV.

18 . The method of claim 16 , further comprising releasing the payload from the UAV during a delivery.

19 . The method of claim 18 , further comprising landing the UAV such that the drag reduction device moves from the rest position to a landing position in which a distal end of the drag reduction device is higher relative to the fuselage than when in the rest position.

20 . The method of claim 18 , further comprising operating the UAV in an unloaded forward flight mode with the drag reduction device in a cruise position in which a distal end of the drag reduction device is further rearward relative to the fuselage than when in the active position.

Assignees

• Wing Aviation Llc

Inventors

• Christian Aaron Bryce
• Prager André Peter
• Marshman Elizabeth Chase
• Ngo Christina Lee

Classifications

• B64C21/08

  adjustable · CPC title

• B64C7/00

  Structures or fairings not otherwise provided for · CPC title

• B64U2101/64

  for parcel delivery or retrieval · CPC title

• B64U30/40 Primary

  Empennages, e.g. V-tails (foldable or collapsible UAVs B64U20/50) · CPC title

• B64U20/00 Primary

  Constructional aspects of UAVs (of lift-producing means B64U30/00) · CPC title