Methods and apparatus for resisting torsional loads in aerial refueling booms

• US 7,959,110 B2
• Filed: 03/28/2008
• Issued: 06/14/2011
• Est. Priority Date: 04/11/2007
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Slusher, Harry S., Johnson, Joel J., Pruitt, Albert S.
• Primary Examiner(s): Ellis; Christopher P
• Application Number:
  US12/058,275
• Publication Number:
  US 20080251643A1
• Time in Patent Office: 1,173 Days
• Field of Search: 244/135.A, 244/135.R, 244/172.4
• US Class Current: 244/135.00A
• CPC Class Codes: B64D 39/04 Adaptations of hose construction pipes in general F16L

Abstract

A refueling boom for an aerial tanker includes an outer member operatively connected to the tanker, an inner member operatively and telescopically configured with the outer member, and one or more torque rollers. The torque roller is disposed on the outer member such that the torque roller engages with the inner member when the inner member is telescoping and reacts to torsional loads subject on the inner member when the boom is deployed in an aerial refueling operation. The inner member may include a plurality of longitudinally disposed torsion surfaces or races for respectively engaging with the torque rollers.

Claims

1. A torsional load resisting aerial refueling boom comprising:

a telescopic boom having a fixed portion and an extendable portion;

a support fitting attached to one end of the fixed portion for allowing the extendable portion to pass therethrough; and

a plurality of rollers mounted on the support fitting for rolling with respect to the movement of the extendable portion of the boom and for providing a counter force to the boom in response to a torsional load subject on the boom during aerial refueling.

2. The refueling boom of claim 1, wherein the plurality of the rollers includes two sets of rollers disposed on generally opposing sides of the boom to provide opposing forces.

3. The refueling boom of claim 2, wherein each set has two rollers and the first roller from the first set and the second roller from the second set provide the counter force to the torsional load and if the torsional load is in the opposite direction, the second roller from the first set and the first roller from the second set provide the counter force to the torsional load.

21. A method of performing an aerial refueling operation, the method comprising:

providing an aerial refueling tanker including the refueling boom of claim 1; and

deploying the boom when the tanker is in flight.

22. The method of claim 21 further comprising:

engaging a receiver aircraft when the boom is deployed; and

transferring fuel from the tanker to the receiver aircraft.

23. The method of claim 22 further comprising:

repeating the deploying, engaging and transferring steps a plurality of times.

4. A refueling boom for an aerial tanker, the boom comprising:

an outer member operatively connected to the tanker;

an inner member operatively and telescopically configured with the outer member; and

a torque roller disposed on the outer member such that the torque roller;

engages with the inner member when the inner member is telescoping; and

reacts to torsional loads subject on the inner member when the boom is deployed in an aerial refueling operation.

5. The boom of claim 4 further comprising a plurality of the torque rollers.

6. The boom of claim 5 wherein the plurality of torque rollers includes pairs of torque rollers respectively disposed on the outer member.

7. The boom of claim 5 wherein the torque rollers are disposed on the outer member in a substantially lateral arrangement.

8. The boom of claim 4 further comprising a plurality of the torque rollers including a first pair of torque rollers and a second pair of torque rollers;

and

wherein;

the inner member includes a plurality of longitudinally disposed torsion surfaces including a first pair disposed in a substantially coplanar manner for engaging the first pair of torque rollers and a second pair disposed in a substantially coplanar manner for engaging the second pair of torque rollers.

9. The boom of claim 8 wherein a first plane and a second plane are respectively defined through the first and second pairs of surfaces such that the planes are substantially parallel with each other.

10. The boom of claim 9 wherein the inner member is defined as having a transverse axis, the rollers of each of the pairs of rollers being offset from the transverse axis.

11. The boom of claim 4 further comprising an upper roller and a lower roller disposed on the outer member in a substantially vertical arrangement such that the upper and lower rollers:

engage with the inner tube when the inner tube is telescoping; and

react to side loads subject on the inner member when the boom is deployed in an aerial refueling operation.

12. The boom of claim 4 further comprising a plurality of load rollers disposed on the outer member such that the load rollers:

engage with the inner member when the inner member is telescoping; and

react to any horizontal and vertical loads subject on the inner member when the boom is deployed in an aerial refueling operation.

13. An aerial refueling tanker including the boom of claim 4.

24. A method of operating an aerial refueling tanker including the refueling boom of claim 11, the method comprising deploying the tanker to refuel a receiver aircraft.

25. The method of claim 24 further comprising repeating the deploying step a plurality of times.

26. The method of claim 25 further comprising performing a maintenance operation on the refueling boom.

14. A refueling boom comprising:

an outer member;

an inner member substantially concentrically disposed with respect to the outer member about a telescopic axis and including a plurality of races, the inner member being subjectable to a torsional load about the telescopic axis;

a plurality of rollers operatively disposed on the outer member substantially circumferentially about the inner member such that the rollers are respectively engageable with races of the inner member when the inner member moves relative to the outer member along the telescopic axis;

the races being disposed on the inner member such that;

a number of the rollers bear the torsional load when the torsional load is bearing in a substantially clockwise direction about the telescopic axis; and

a number of the rollers bear the torsional load when the torsional load is bearing in a substantially counter-clockwise direction about the telescopic axis.

15. The boom of claim 14 wherein the races are disposed on the inner member such that:

a number of the races respectively engage with the rollers to substantially prevent rotation of the inner member when a torsional load urges the inner member in a clockwise direction about the telescopic axis; and

a number of the races respectively engage with the rollers to substantially prevent rotation of the inner member when a torsional load urges the inner member in a counterclockwise direction about the telescopic axis.

16. A method of refueling a receiver aircraft with an aerial refueling tanker including a telescopic boom having an outer member and an inner member, the latter of which being subjectable to torsional loads during an aerial refueling operation, the method comprising:

telescopically extending the inner member from the outer member when the boom is deployed; and

operatively deploying a plurality of rollers on the outer member that will react to any torsional load subject on the inner member when extended from the outer member.

17. The method of claim 16 wherein the reacting step further comprises substantially preventing rotation of the inner member about a telescopic axis along which the inner member is extensible.

18. The method of claim 17 wherein the reacting step further comprises substantially preventing clockwise rotation of the inner member at at least two locations on the inner member and substantially preventing counter-clockwise rotation of the inner member at at least two locations on the inner member.

19. The method of claim 16 further comprising transferring fuel to the receiver aircraft when the boom is engaged therewith.

20. The method of claim 19 further comprising:

deploying the boom including the extending and reacting steps; and

repeating the deploying and transferring steps a plurality of times.