SYSTEMS AND METHODS FOR CONTROLLING AN AERIAL REFUELING DEVICE

• US 20070215753A1
• Filed: 09/01/2005
• Published: 09/20/2007
• Est. Priority Date: 09/01/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Feltrop, Ed, Schuster, John
• Granted Patent: US 7,472,868 B2
• Time in Patent Office: Days
• US Class Current: 244/135.A
• 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

Systems and methods for refueling aircraft in flight are disclosed herein. An aerial refueling system in accordance with one aspect of the invention includes a movable aerial refueling boom configured to be carried by an aerial refueling aircraft. The system can also include two or more actuators operably coupled to the boom to control motion of the boom relative to the refueling aircraft. In several embodiments, the boom does not include any boom aerodynamic control surfaces to control motion of the boom relative to the refueling aircraft.

Claims

1. (canceled)

2. (canceled)

3. An aerial refueling system, comprising:

a movable aerial refueling boom configured to be carried by an aerial refueling aircraft;

a boom support carried by the aerial refueling aircraft, wherein the boom support includes a first portion positioned to rotatably move about a first axis and a second portion at least partially aligned with a second axis generally normal to the first axis; and

two or more actuators operably coupled to at least one of the boom support and the boom to control motion of the boom relative to the refueling aircraft, wherein the two or more actuators include (a) a first actuator operably coupled to the boom support and positioned to rotatably move the boom about the first axis, and (b) a second actuator operably coupled to the boom support and positioned to pivotably move the boom about the second axis.

4. The system of claim 3 wherein the first axis is a yaw axis and the second axis is a pitch axis.

5. The system of claim 3 wherein:

the two or more actuators operably coupled to at least one of the boom support and the boom include (a) a first actuator carried by the first portion of the boom support and positioned to move the boom about a pitch axis, and (b) a second actuator and a third actuator carried by the second portion of the boom support and positioned to move the boom about a yaw axis generally normal to the pitch axis.

7. The system of claim 3 wherein the boom does not include any boom aerodynamic control surfaces.

8. The system of claim 3 wherein the two or more actuators include hydraulic actuators.

9. The system of claim 3 wherein the two or more actuators include pneumatic actuators.

10. The system of claim 3 wherein the two or more actuators include electrical actuators.

11. The system of claim 3, further comprising the aerial refueling aircraft.

12. The system of claim 3 wherein the boom is elongated along a boom axis and includes a first portion coupled to the refueling aircraft and a second portion positioned to mate with a receiver aircraft, and wherein the two or more actuators are coupled to the boom proximate to the first portion of the boom and control motion of the boom from the first portion of the boom.

26. The system of claim 3 wherein the first actuator is a rotary actuator and the second actuator is a pitch ram.

27. The system of claim 3 wherein the first actuator extends lengthwise along a first actuator axis and the second actuator extends lengthwise along a second actuator axis, and wherein the first actuator axis and the second actuator axis are generally parallel with each other.

6. (canceled)

13. (canceled)

14. An aerial refueling system, comprising:

a tanker aircraft;

a boom mounting assembly carried by the tanker aircraft, the boom mounting assembly including a boom support having a first portion positioned to rotatably move about a first axis and a second portion at least partially aligned with a second axis generally normal to the first axis;

a movable aerial refueling boom carried by at least one of the boom support and the tanker aircraft, wherein the boom does not include any boom aerodynamic control surfaces; and

one or more actuators operably coupled to at least one of the boom support and the boom to control motion of the boom relative to the tanker aircraft, wherein the one or more actuators carried by the boom support include (a) a first actuator operably coupled to the boom support and positioned to rotatably move the boom about the first axis, and (b) a second actuator operably coupled to the boom support and positioned to pivotably move the boom about the second axis.

15. The system of claim 14 wherein:

the one or more actuators carried by the boom support include (a) a first actuator carried by the first portion of the boom support and positioned to move the boom about a first axis, and (b) a second actuator and a third actuator carried by the second portion of the boom support and positioned to move the boom about a second axis generally normal to the first axis.

17. The system of claim 14 wherein the one or more actuators include hydraulic actuators, the hydraulic actuators including linear rams or helical rotary actuators.

18. The system of claim 14 wherein the one or more actuators include pneumatic actuators.

19. The system of claim 14 wherein the one or more actuators include electrical actuators, the electrical actuators including screw jack or recirculating ball-type drives.

16. (canceled)

20. (canceled)

24. A method for refueling aircraft in flight, the method comprising:

deploying a generally rigid aerial refueling boom without any boom aerodynamic control surfaces from a refueling aircraft; and

controlling a position of the boom relative to the refueling aircraft by controlling one or more actuators operably coupled to at least one of the boom and a boom support carrying the boom, wherein controlling one or more actuators includes (a) moving the boom about a first axis with a first actuator operably coupled to the boom support, and (b) moving the boom about a second axis generally normal to the first axis with a second actuator operably coupled to the boom support.

21. The method of claim 24 wherein controlling a position of the boom relative to the refueling aircraft includes controlling the position of the boom without the use of any boom aerodynamic control surfaces.

22. The method of claim 24 wherein:

deploying a generally rigid aerial refueling boom includes deploying a boom having a first portion proximate to the refueling aircraft and a second portion at a distal end of the boom; and

controlling a position of the boom includes controlling one or more actuators operably coupled to the first portion of the boom.

23. The method of claim 24, further comprising guiding the boom into a coupling position with a receiver aircraft using the one or more actuators.

28. The method of claim 24 wherein controlling a position of the boom relative to the refueling aircraft by controlling one or more actuators includes controlling a position of the boom with one or more hydraulic actuators, pneumatic actuators, or electrical actuators.

25. (canceled)