Controllable refueling drogues and associated systems and methods

• US 7,887,010 B2
• Filed: 05/22/2007
• Issued: 02/15/2011
• 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): Collins; Timothy D
• Assistant Examiner(s): Bonzell; Philip J
• Application Number:
  US11/752,156
• Publication Number:
  US 20080054124A1
• Time in Patent Office: 1,365 Days
• Field of Search: 244/135.A, 244/135.R, 244/1.TD
• 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 including a plurality of vanes arranged circumferentially around a major axis, the vanes having a radially outwardly facing surface and a generally tangentially facing surface, wherein the radially outwardly facing surface is larger than the generally tangentially facing surface, and a canopy coupled to the vanes, the drogue being coupled to the flexible fuel line, wherein the plurality of vanes

comprises a plurality of first and second vanes;

a plurality of actuators wherein individual actuators are operatively coupled to a correspond first cane and a corresponding second vane and with the actuators operable to change a relative circumferential distance between the corresponding first vane and the corresponding second vane;

at least one sensor positioned to detect at least one of a load on and a position of the fuel delivery device and produce a corresponding signal; and

a computer-based system carried by the deployable portion and operatively coupled to the actuators, the computer-based system including instructions to

direct the operation of the actuators in response to the signal in a feedback manner.

2. The system of claim 1 wherein the sensor comprises an image sensor carried by the drogue, the image sensor being positioned to gather image data and provide the data to the computer-based system for processing, and wherein the computer-based system directs operation of the actuators in response to the image data.

3. The refueling system of claim 1, further comprising a self-contained power source carried solely by the deployable portion and coupled to the actuators and the computer-based system.

4. The refueling system of claim 1, further comprising:

a refueling aircraft, wherein the fuel delivery device is carried by the refueling aircraft and wherein the computer-based system directs the operation of the actuators without instructions from the refueling aircraft when deployed.

5. The refueling system of claim 1 wherein the computer-based system includes a controller operatively coupled to the actuators.

6. The refueling system of claim 5 wherein the computer-based system includes a guidance system operatively coupled to the controller, the guidance system being programmed with instructions for issuing directives to the controller based at least in part on a difference between an actual and a target position of the drogue.

7. The refueling system of claim 1, further comprising at least a second sensor positioned to detect a location of an approaching aircraft, and wherein the computer-based system is programmed to use information received from the second sensor to direct the operation of the actuators.

8. The refueling system of claim 7 wherein the second sensor is positioned to detect the location of a receiver aircraft.

9. The refueling system of claim 7 wherein the second sensor includes an optical sensor.

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, the drogue including multiple vanes coupled to a canopy and arranged circumferentially around a major axis, wherein individual vanes have an outwardly facing surface and a generally tangentially facing edge, and wherein the outwardly facing surface is larger than the generally tangentially facing edge;

at least one sensor located to detect at least one of a position of the drogue relative to an approaching aircraft and a load on the drogue, and produce a corresponding signal;

a plurality of actuators wherein individual actuators are operatively coupled to a corresponding first vane and a corresponding second vane with the actuators operable to change a relative circumferential distance between the first vane and the second vane one or more vanes, or the canopy, or one or more vanes and the canopy; and

a guidance system carried by the deployable portion and operatively coupled to at least one of the actuators, the guidance system including instructions to direct the operation of the at least one actuator in a feedback manner to shape the drogue asymmetrically relative to the major axis in response to the signal to stabilize drogue flight and move the drogue.

11. The refueling system of claim 10 wherein the sensor is an image sensor positioned to capture image data and provide the image data to the guidance system, and wherein the guidance system directs the actuators to move the canopy to stabilize the flight of the drogue.

12. The refueling system of claim 10, further comprising a self-contained power system carried solely by the deployable portion and operatively coupled to the actuatable device and the guidance system to power the actuators and the guidance system.

13. The refueling system of claim 10 wherein the guidance system is self-contained and carried solely by the deployable portion.

14. The refueling system of claim 10 wherein the guidance system is a computer-based guidance system and wherein the instructions are computer-based instructions.

15. The refueling system of claim 10 wherein the guidance system forms a portion of a computer-based system that includes instructions directing the operation of the actuators in a manner that shapes the drogue asymmetrically relative to the major axis.

16. 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, wherein the drogue comprises a plurality of vanes and a canopy coupled to the vanes, and wherein the vanes comprise a radially outward facing surface and a generally tangentially facing surface, the radially outward facing surface being larger than the generally tangentially facing surface;

a plurality of actuators wherein individual actuators are operatively coupled to a corresponding first vane and a corresponding second vane;

a sensor positioned to detect at least one of a load on or a position of the fuel delivery device and produce a corresponding signal;

a computer-based system operatively coupled to the actuators, the computer-based system including instructions to direct the operation of the actuators in response to the signal in a feedback manner that shapes the drogue asymmetrically with respect to the flexible fuel line by moving the corresponding first vane circumferentially toward or away from the corresponding second vane; and

a self-contained power system carried by the deployable portion and operatively coupled to the actuators to power the actuators.

17. The refueling system of claim 16 wherein the power system includes a wind-driven power system carried by the deployed portion and coupled to the actuators.

18. The refueling system of claim 16, further comprising a guidance system carried by the deployable portion and operatively coupled to the actuators.

19. 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, the drogue comprising a plurality of first and second vanes extending circumferentially around the drogue to form an exposed surface, wherein individual vanes have a generally tangentially facing edge that is smaller than the exposed surface;

sensing at least one of a load on and a position of the drogue and producing a corresponding signal; and

stabilizing the drogue in flight by changing a shape of the drogue via instructions directed from a computer-based guidance system to a plurality of actuator wherein individual actuators are operatively coupled to a corresponding first vane and a corresponding second vane, wherein the instructions direct the actuators to move the corresponding first vane circumferentially toward or away from the corresponding second vane, with the instructions being generated by the computer-based guidance system in response to the signal and with the actuators and the guidance system carried solely by the deployed portion of the refueling system.

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, the drogue comprising a plurality of first and second vanes and a canopy, wherein the vanes extend circumferentially around the drogue to form an exposed surface, individual vanes having a generally tangential edge and a radially outwardly facing surface that is larger than the generally tangential edge;

sensing at least one of a load on and a position of the drogue;

producing a signal corresponding to the at least one of load on and position of the drogue; and

stabilizing the drogue by powering a plurality of actuator wherein individual actuators are operatively coupled to a corresponding first vane and a corresponding second vane to move the corresponding first vane circumferentially relative to the corresponding second vane in response to the signal in a feedback manner, wherein powering the actuator includes powering the actuators via a power supply carried solely by the deployed portion of the refueling system.