Aerial refueling system and method

Patent metadata

Field	Value
Publication number	US-9227735-B2
Application number	US-201313860533-A
Country	US
Kind code	B2
Filing date	Apr 11, 2013
Priority date	Apr 11, 2013
Publication date	Jan 5, 2016
Grant date	Jan 5, 2016

Abstract

A refueling system may include a refueling hose and a refueling drone coupled to the hose aft end. The refueling drone may be rearwardly deployable from the tanker aircraft such that the refueling drone is towed by the refueling hose behind the tanker aircraft. The refueling drone may be engaged to a receiver aircraft for transferring fuel from the tanker aircraft to the receiver aircraft.

First claim

What is claimed is:

1. A refueling system, comprising:
a refueling hose extendable from a tanker aircraft in flight; and
a refueling drone coupled to a hose aft end and being rearwardly deployable from the tanker aircraft such that the refueling drone is towed by the refueling hose behind the tanker aircraft;
the refueling drone having a drone longitudinal axis and including a refueling boom outwardly pivotable from the refueling drone from a retracted position to a deployed position wherein the refueling boom is oriented at a boom pivot angle relative to a drone longitudinal axis, the refueling drone configured to engage a receiver aircraft and transfer fuel from the tanker aircraft to the receiver aircraft.

2. The refueling system of claim 1 , wherein the refueling drone includes:
the refueling boom having a fitting configured to mate with a receptacle of the receiver aircraft.

3. The refueling system of claim 1 , wherein:
the refueling boom includes a boom section that is telescopically extendable.

4. The refueling system of claim 1 , further comprising:
a wing pod mountable to a wing of the tanker aircraft; and
the refueling drone being extendable out of the wing pod and retractable into the wing pod.

5. The refueling system of claim 4 , wherein:
the wing pod is configured to contain the refueling hose when the refueling drone is in a retracted position.

6. The refueling system of claim 1 , wherein:
the refueling drone is deployable from an aircraft interior of the tanker aircraft.

7. The refueling system of claim 1 , further including:
a drogue mounted on a drone aft end of the refueling drone.

8. The refueling system of claim 1 , further comprising:
at least one control surface mounted on the refueling drone;
the control surface being outwardly pivotable into an air stream.

9. The refueling system of claim 8 , wherein:
an orientation of the control surface is controllable in a manner providing control of at least one of roll, pitch, and yaw of the refueling drone.

10. The refueling system of claim 8 , wherein:
a plurality of control surfaces are positioned on the refueling drone;
the control surfaces being independently controllable for attitude control of the refueling drone.

11. An aerial refueling system, comprising:
a refueling hose being extendable from a wing pod mounted to a wing of a tanker aircraft;
a refueling drone having a drone longitudinal axis and coupled to the refueling hose and being rearwardly deployable from the wing pod such that the refueling drone is towed by the refueling hose behind the tanker aircraft;
a refueling boom being pivotable outwardly from the refueling drone from a retracted position to a deployed position wherein the refueling boom is oriented at a boom pivot angle relative to a drone longitudinal axis, the refueling drone configured to mate with a receptacle of a receiver aircraft; and
a plurality of control surfaces positioned on the refueling drone and being controllable for attitude control of the refueling drone.

12. A method of refueling an aircraft, comprising the steps of:
extending a refueling hose from a tanker aircraft;
towing a refueling drone coupled to an end of the refueling hose and having a drone longitudinal axis;
pivoting a refueling boom outwardly from the refueling drone from a retracted position to a deployed position wherein the refueling boom is oriented at a boom pivot angle relative to a drone longitudinal axis;
engaging the refueling drone with a receiver aircraft; and
transferring fuel from the tanker aircraft to the receiver aircraft.

13. The method of claim 12 , further comprising:
mating a fitting on the refueling boom with a receptacle of the receiver aircraft.

14. The method of claim 12 , further comprising:
telescopically extending a boom section of the refueling boom.

15. The method of claim 12 , further comprising:
retracting and extending the refueling drone into and out of a wing pod.

16. The method of claim 15 , further comprising:
storing the refueling hose in the wing pod.

17. The method of claim 12 , further comprising:
deploying a drogue from a drone aft end of the refueling drone;
generating aerodynamic drag using the drogue.

18. The method of claim 12 , further comprising:
retracting and extending the refueling drone into and out of an interior of the tanker aircraft.

19. The method of claim 12 , wherein:
deploying a control surface mounted on the refueling drone;
maneuvering the refueling drone in response to deploying the control surface.

20. The method of claim 19 , wherein the step of maneuvering the refueling drone comprises:
controlling any combination of roll, pitch, and yaw of the refueling drone.

Assignees

• Boeing Co

Inventors

• Kusnitz Joshua M

Classifications

• B64D39/04

  Adaptations of hose construction · CPC title

• B64D39/00 Primary

  Refuelling during flight · CPC title

• B64D39/06

  Connecting hose to aircraft; Disconnecting hose therefrom · CPC title