Controllable refueling drogues and associated systems and methods

• US 7,219,857 B2
• Filed: 06/20/2005
• Issued: 05/22/2007
• Est. Priority Date: 06/20/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Takacs, John F., Stecko, Stephen M., Jefferson, Gordon R., Roberts, Gregory A., Shoore, Joseph D.
• Primary Examiner(s): Luu; Teri Pham
• Assistant Examiner(s): Mayle; Edward J.
• Application Number:
  US11/157,245
• Publication Number:
  US 20060284019A1
• Time in Patent Office: 701 Days
• Field of Search: 244/135.A
• US Class Current: 244/135.00A
• CPC Class Codes: B64D 39/00 Refuelling during flight filling or emptying fuel tanks B64D37/14
• CPC Class Codes: B64D 39/04 Adaptations of hose construction pipes in general F16L

Abstract

Controllable refueling drogues and associated systems and methods are disclosed. A system in accordance with one embodiment includes a fuel delivery device having a deployable portion configured to be deployed overboard an aircraft during aerial refueling. The deployable portion can include at least a portion of a flexible fuel line, a drogue coupled to the flexible fuel line, and an actuatable device operatively coupled to at least one of the drogue and the fuel line. The deployable portion can further include a guidance system that is operatively coupled to the actuatable device and that includes instructions to direct the operation of the actuatable device and move the drogue during flight.

Claims

1. An airborne refueling system, comprising:

a fuel delivery device having a deployable portion configured to be deployed overboard an aircraft during aerial refueling, the deployable portion including;

at least a portion of a flexible fuel line;

a drogue coupled to the flexible fuel line, the drogue having multiple vanes arranged around an axis, and movable in a circumferential direction relative to the axis;

an actuable device operatively coupled to at least one of the vanes to move the vanes in a circumferential direction relative to the axis; and

a guidance system carried by the deployable portion and operatively coupled to the actuable device, the guidance system including instructions to direct the operation of the actuable device and move the drogue during flight.

2. The system of claim 1, further comprising:

a refueling aircraft, wherein the fuel delivery device is carried by the refueling aircraft;

and wherein the guidance system directs the operation of the actuatable device without instructions from the refueling aircraft when deployed;

further wherein the guidance system includes a database of receiver aircraft image data, and wherein the system further comprises at least one sensor configured to detect a characteristic of a receiver aircraft, and wherein the guidance system is programmed to compare the image data with information received from the at least one sensor and direct the operation of the actuatable device to position the drogue for coupling with the receiver aircraft.

3. The system of claim 1, further comprising at least one sensor configured to detect a location of a receiver aircraft probe, and wherein the guidance system is programmed to use information received from the at least one sensor to direct the operation of the actuatable device to position the drogue for coupling with the probe of the receiver aircraft.

4. The system of claim 1, further comprising a refueling aircraft, wherein the fuel delivery device is carried by the refueling aircraft, and wherein the guidance system directs the operation of the actuatable device without instructions from the refueling aircraft when deployed.

5. The system of claim 1, further comprising a controller carried by the deployed portion and coupled to the guidance system and the actuatable device, the controller being programmed with instructions to receive guidance commands from the guidance system and direct commands to the actuatable device based at least in part on the commands received from the guidance system.

6. The system of claim 1, further comprising a wind-driven power system carried by the deployed portion and coupled to the guidance system.

7. The system of claim 1, further comprising at least one sensor carried by the deployable portion, the sensor being positioned to detect the location of at least one of the deployable portion and a receiver aircraft proximate to the deployable portion.

8. The system of claim 1 wherein the drogue includes a canopy coupled to the vanes.

9. The system of claim 8 wherein the acutuatable device includes an electro-active polymer actuator.

26. The system of claim 1 wherein adjacent vanes overlap each other and wherein actuation of the actuatable device changes an amount by which adjacent vanes overlap each other.

27. The system of claim 1 wherein the actuatable device is connected between adjacent overlapping vanes.

10. An airborne refueling system, comprising:

a fuel delivery device having a deployable portion configured to be deployed overboard an aircraft during aerial refueling, the deployable portion including;

at least a portion of a flexible fuel line;

a drogue coupled to the flexible fuel line and arranged around a major axis;

actuation means for changing a shape of the drogue to be eccentric relative to the major axis; and

guidance means for directing the operation of the actuation means.

11. The system of claim 10, further comprising sensing means configured to detect a location of a receiver aircraft probe, and wherein the guidance means is configured to direct the operation of the actuation means to position the drogue for coupling with the probe.

12. The system of claim 10, further comprising a refueling aircraft, wherein the fuel delivery device is carried by the refueling aircraft, and wherein the guidance means directs the operation of the actuation means without instructions from the refueling aircraft when deployed.

13. The system of claim 10, further comprising control means carried by the deployed portion and coupled to the guidance means and the actuation means, the control means being programmed with instructions to receive guidance commands from the guidance means and direct commands to the actuation means based at least in part on the commands received from the guidance means.

14. The system of claim 10, further comprising sensor means for sensing the location of at least one of the deployable portion and a receiver aircraft proximate to the deployable portion, the sensing means being carried by the deployable portion.

28. The system of claim 10 wherein the drogue includes multiple vanes that are movable relative to each other in a circumferential direction to assume the eccentric shape.

15. An airborne refueling system, comprising:

a fuel delivery device that includes;

a flexible fuel line;

a drogue coupled to the flexible fuel line, the drogue including multiple vanes arranged around an axis, the drogue further including a canopy coupled to the vanes; and

at least one actuator coupled to at least one of the vanes to move the vane in a circumferential direction relative to the axis.

16. The system of claim 15 wherein the at least one actuator includes an electro-active polymer actuator.

17. The system of claim 15 wherein the at least one actuator is positioned to move at least one of the vanes relative to another of the vanes.

18. The system of claim 15 wherein the at least one actuator is positioned to control a size, shape or size and shape of the canopy.

19. The system of claim 15, further comprising a guidance system operatively coupled to the at least one actuator, the guidance system being programmed with instructions to control a motion of the drogue by selectively directing the at least one actuator to actuate.

29. The system of claim 15 wherein adjacent vanes overlap each other and wherein actuation of the actuatable device changes an amount by which adjacent vanes overlap each other.

20. A method for refueling an aircraft, comprising:

aerially deploying from a tanker aircraft a portion of a refueling system that includes a flexible fuel line and a drogue arranged around a major axis; and

changing a position of the drogue by controlling an actuator operatively coupled to the drogue and carried by the deployed portion of the refueling system, wherein activation of the actuator causes the drogue to assume an eccentric shape relative to the major axis.

21. The method of claim 20 wherein changing a position of the drogue includes automatically changing the position of the drogue based at least in part on information received from a guidance system carried by the deployed portion of the refueling system.

22. The method of claim 20, further comprising guiding the drogue into a coupling position with a receiver aircraft without guidance instructions from the tanker aircraft.

23. The method of claim 20 wherein the drogue includes multiple vanes arranged around an axis, and a canopy coupled to the vanes, and wherein changing a position of the drogue includes steering the drogue by changing a position of the canopy, at least one of the vanes, or both the canopy and at least one of the vanes.

24. The method of claim 20, further comprising detecting a difference between an actual position of a receiver aircraft and a target position of a receiver aircraft and directing the drogue to move in a manner that reduces the difference.

25. The method of claim 20, further comprising:

detecting a characteristic of a receiver aircraft;

comparing the detected characteristic with information corresponding to known receiver aircraft; and

identifying the receiver aircraft.

30. The method of claim 20 wherein changing a position of the drogue includes changing an amount by which adjacent vanes of the drogue overlap each other in a circumferential direction.

31. An airborne refueling system, comprising:

a fuel delivery device that includes;

a flexible fuel line;

a drogue coupled to the flexible fuel line, the drogue including multiple vanes arranged around an axis; and

at least one actuator coupled to at least one of the vanes to move the at least one vane in a circumferential direction relative to the axis.

32. The system of claim 31 wherein adjacent vanes overlap each other and wherein actuation of the actuatable device changes an amount by which adjacent vanes overlap each other.

33. The system of claim 31 wherein the actuatable device is connected between adjacent overlapping vanes.