FRICTIONLESS SERVICE CARRIAGE SYSTEM

Abstract

A frictionless service carriage system including: a shaft 1 having a first 2 and a second 3 helix-shaped guide in its surface, each helix shaped-guide 2, 3 defining a linear movement along the longitudinal axis of the shaft 1 of a carriage 4 in opposite directions and both helix shaped-guides 2, 3 crossing each other 2, 3 along the longitudinal axis of the shaft 1, wherein the carriage 4 includes a movable element 5 located into a helix-shaped guide 2, 3 and movable along it 2, 3, the movable element 5 comprising a set of rolling elements 6 along the first or second helix-shaped guide 2, 3 of the shaft 1 and configured such that in a crossing with the other helix-shaped guide 2, 3, the set of rolling elements 6 has at least two contact points with the helix-shaped guide 2, 3 for which it rolls.

Claims

1. A service carriage system comprising: a shaft including a first and a second helix-shaped guide in a surface of the shaft, each helix shaped-guide configured to define a linear movement along a longitudinal axis of the shaft in opposite directions and both the first and second helix shaped-guides crossing each other along the longitudinal axis of the shaft, and a carriage including a movable element configured to be located in and move along the first and second helix-shaped guides, wherein in that the movable element includes rolling elements configured to roll one behind the other along at least one of the first and second helix-shaped guides, and configured such that in a crossing with the other helix-shaped guide, the rolling elements have at least two contact points with the first and second helix-shaped guides.

2. The service carriage system according to claim 1, wherein the carriage comprises a support configured to support the set of rolling elements and the support has an arcuate shape configured to position the rolling elements in at least one of the helix-shaped guides.

3. The service carriage system according to claim 1, wherein the set of rolling elements comprises three rolling elements.

4. The service carriage system according to claim 3, wherein the three rolling elements are balls.

5. The service carriage system according to claim 4, wherein a cross-section of the helix-shaped guides is semi-circular.

6. The service carriage system according to claim 3, wherein the three rolling elements are bearings 9 each having a cylindrical shape.

7. The service carriage system according to claim 6, wherein a cross-section of the helix-shaped guides is rectangular.

8. The service carriage system according to claim 2, wherein the carriage comprises a rod attached to and perpendicular to the support 7, wherein the rod and the support are configured such the support is rotatable around a longitudinal axis of the rod.

9. The service carriage system according to claim 1, wherein the helix-shaped guides both intersect at an end of the shaft and the intersection forms a progressively widening of the guides.

10. A service carriage assembly configured to be mounted adjacent a drum in a hose refueling system in a tanker aircraft, the service carriage system includes: a shaft configured to turn with the drum, be offset from the drum and have a rotational axis parallel to a rotational axis of the drum; helical guide grooves in the shaft wherein each of the helical guide grooves forms a helix coaxial to the rotational axis of the shaft and the helical guide grooves are angularly offset from each other on the shaft; a service carriage configured to move back and forth along the shaft and driven by rotation of the shaft, wherein the service carriage includes an arcuate shaped support, and rolling elements mounted to the arcuate shaped support wherein the rolling elements are aligned along an arcuate line.

11. The service carriage assembly of claim 10 wherein the arcuate line conforms to a curvature of each of the helical guide grooves.

12. The service carriage assembly of claim 10 wherein the rolling elements include at least three rolling elements.

13. The service carriage assembly of claim 10 wherein the service carriage includes a shaft extending from the arcuate shaped support in a direction opposite to the rolling elements, wherein the shaft is configured to turn to rotate the rolling elements about an axis of the shaft.

14. The service carriage assembly of claim 10 wherein a hose guide is fixed to the service carriage.

15. The service carriage assembly of claim 10, wherein the rolling elements are spherical bearings.

16. The service carriage assembly of claim 15, wherein the helical guide grooves are semi-circular in cross section.

17. The service carriage assembly of claim 10, wherein the rolling elements are cylindrical bearings.

18. The service carriage assembly of claim 17, wherein the helical guide grooves each include a bottom which is straight in a cross section of each of the grooves.

19. The service carriage assembly of claim 10, wherein the helical guide grooves intersect at an end region of the shaft and the intersection of the guide grooves forms a groove which is wider than each of the guide grooves.

Description

SUMMARY OF FIGURES

[0023] To complete the description and in order to provide for a better understanding of the invention, a set of drawings is provided. The set of drawings form an integral part of the description and illustrate preferred embodiments of the invention. The set of drawings are:

[0024] FIG. 1 shows a schematic front view of a first embodiment of the movable elements having a set of rolling elements, specifically three balls.

[0025] FIG. 2 shows a schematic front view of a second embodiment of the movable element having a set of rolling elements, specifically three bearings having a cylindrical shape.

[0026] FIG. 3 shows a guide having a spherical cross section adapted for the rolling of set of rolling elements shown in FIG. 1.

[0027] FIG. 4 shows a guide having a rectangular cross section adapted for the rolling of set of rolling elements shown in FIG. 2.

[0028] FIG. 5 shows the transition between both helixes at the end of the shaft.

[0029] FIG. 6 shows a tanker aircraft refueling another aircraft in an air-to-air refueling operation.

[0030] FIG. 7 schematically shows a hose and drogue refueling system for a tanker aircraft.

DETAILED DESCRIPTION

[0031] FIGS. 1 to 5 show two embodiments for the set of rolling elements 6, one based on the use of balls 8 and another based on the use of bearings 9 having a cylindrical shape and configured to roll around its longitudinal axis.

[0032] The balls 8 offer low friction rolling through the guide 2, 3. The bearings 9 are easier to manufacture than the balls 8 but may have higher friction as the bearings move through the guide.

[0033] The carriage includes a support 7 for supporting the set of rolling elements 6. The carriage positions the rolling elements 6 such that all rolling elements 6 are simultaneously and continuously in contact with the helix-shaped guide 2, 3 when rolling.

[0034] The support 7 may have an arquated shape, e.g., arcuate. In this regard, the support may have a concave bow shape which conforms to the curvature of the shaft 1 along the directions of the surfaces of the guides 2, 3. The support holds mounts for the rolling elements 6 such that the rolling elements are all positioned in the guides 2, 3 while the support is positioned next to the shaft.

[0035] The set of rolling elements 6 may include three rolling elements, such as three balls 8 or three bearings 9. The set of rolling elements and support 7 are configured to roll along the guides 2, 3. The rolling elements may be aligned along a line having a curvature conforming to a curvature of each of the guides 2, 3. The rolling elements may each include a housing fixed to the support and a roller, such as a spherical or cylindrical bearing, supported by the housing. The roller rolls while in the housing. The rollers roll as they move along the guides 2, 3. The rolling of the rollers minimize friction between the rolling elements and the guides 2, 3.

[0036] The design of a cross-section of the helix-shaped guide 2, 3 in an outer surface of the shaft 1 may be selected to conform to the type of rolling elements 6. As shown in FIG. 3, a guide 2, 3 formed by grooves in the shaft 1 that are semi-circular in cross-section conforms to the outer circular surface of the balls 8 of the rolling elements 6. As shown in FIG. 4, a guide 2, 3 formed by grooves in the shaft 1 that are rectangular in cross section conform to bearings 9 that form the rolling elements 6.

[0037] The carriage may also include a rod 10 located perpendicular to and attached to the support 7. The rod 10 and the support 7 rotate about a longitudinal axis of the rod 10. The rod 10 allows the support 7 to turn and hence allows the turning of the set of rolling elements 6 when they reach ends of the helix 2, 3 at the end of the shaft 1. The rolling elements 6 are turned so that they may be positioned to enter the other helix 2, 3.

[0038] On both sides of the shaft 1, in the transition between both helixes 2, 3, the guide 2, 3 is modified to allow the movement of the set of rolling elements 6. This is achieved by progressively widening the cross-section of the grooves forming the guide 2, 3 at the meeting point of both helixes 2, 3 as can be seen in FIG. 5.

[0039] FIG. 6 shows a tanker aircraft 20 refueling a fuel receiving aircraft 22 in an air-to-air refueling operation. A refueling hose 24 is extended from the tanker aircraft 22 towards the other aircraft 22. The hose is extended by unwinding the hose from a drum within the tanker aircraft.

[0040] FIG. 7 schematically shows a hose and drogue refueling system 26 for a tanker aircraft 20. The system 26 may include a hose 24 with a drogue 28 at a distal end of the hose. The drogue 28 connects to a fuel receiver in the other aircraft 22 to allow fuel to flow from the hose into the other aircraft. The proximal end of the hose 24 is connected to a fuel pump 30 which pumps fuel from a fuel tank 32 within the tanker aircraft. A controller 34 controls the pump, fuel delivery through the hose and the winding and unwinding of the hose 24 on a drum 36

[0041] A service carriage assembly 38 is offset and near the drum 36. The service carriage assembly includes the carriage 4 shown in FIGS. 1 and 2. The service carriage assembly 38 includes a shaft 40 and is supported by refueling system such that the service carriage assembly can carry the forces (load) of the hose as the hose is wound and unwound for air-to-air refueling operations. The shaft 40 is offset from the drum and parallel to the drum. The shaft 40 is the same as the shaft 1 shown in FIGS. 3 to 5 and includes the helical guides 2, 3 shown in those figures.

[0042] The service carriage assembly may include a hose guide 42 that includes an opening to receive the hose 24. The hose guide 42 is supported by the service carriage 38. The hose guide positions the hose with respect to the drum as the hose is wound onto the drum or unwound from the drum. The hose guide 42 moves back and forth across the width of the drum (in a direction perpendicular to the plane of FIG. 7). The hose guide may be attached to the rod 10 of the service carriage 38. The hose guide 42 is supported by and moved by the support 7 (FIGS. 1 and 2) as the support moves along the guides 2, 3 as the shaft 1 rotates with the rotation of the drum 36.

[0043] While at least one exemplary embodiment of the present inventions is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiments. In addition, in this disclosure, the terms comprise or comprising do not exclude other elements or steps, the terms a or one do not exclude a plural number, and the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.