Automated refuelling system

• US 5,634,503 A
• Filed: 06/05/1995
• Issued: 06/03/1997
• Est. Priority Date: 06/05/1995
• Status: Expired due to Fees

• Current Assignee: Shell Oil Company (Shell Plc)
• Original Assignee: Shell Oil Company (Shell Plc)
• Inventors: Root, George N. P., Williams, Owen R., Ramsey, William D. Jr., Padula, Joseph A., Musil, David I.
• Primary Examiner(s): JACYNA, J CASIMER
• Application Number:
  US08/461,276
• Time in Patent Office: 729 Days
• Field of Search: 141/231, 141/232, 141/98, 141/279, 141/387, 141/388, 137/234.6, 137/615, 901/6, 901/16, 901/41
• US Class Current: 141/232
• CPC Class Codes: B67D 2007/0436 according to a spatial coordinate system
• CPC Class Codes: B67D 2007/0453 recognising the fuel to be dispensed
• CPC Class Codes: B67D 2007/0469 by interrogating a transponder
• CPC Class Codes: B67D 7/0401 arrangements for automatically fuelling vehicles, i.e. without human intervention
• CPC Class Codes: B67D 7/145 by wireless communication means, e.g. RF, transponders or the like
• CPC Class Codes: Y10T 137/3802 With vehicle guide or support, e.g., service station
• CPC Class Codes: Y10T 137/8807 Articulated or swinging flow conduit

Abstract

A refuelling system is provided, the system comprising: a plurality of vertically telescoping elements, the telescoping elements containing a constant length of flexible conduit for transfer of fuel; at least one vertically movable pulley to maintain a constant length of flexible hose within the telescoping elements; an overhead gantry capable of moving the vertically telescoping elements in two horizontal essentially perpendicular axes; and a rotating lower portion of the telescoping elements capable of rotating about an essentially vertical axis and supporting a fuel nozzle. The refuelling system of the present invention does not result in significant segments of unsupported lengths of conduits for fuel, compressed air, vapor recovery, electrical power or control or sensor signals. It is relatively simple and utilizes readily available components and parts, and does not required significant machining of components. This results in an installation that is economical to install and operate.

Claims

1. A refuelling system comprising:

a plurality of vertically telescoping elements, the telescoping elements containing a constant length of flexible conduit for transfer of fuel;

at least one vertically movable pulley to maintain a constant length of flexible hose within the telescoping elements;

an overhead gantry capable of moving the vertically telescoping elements in two horizontal essentially perpendicular axes; and

a rotating lower portion of the telescoping elements capable of rotating about an essentially vertical axis and supporting a fuel nozzle.

2. The refuelling system of claim 1 wherein the overhead gantry comprises a longitudinal axis and an axis essentially perpendicular to the longitudinal axis, and a set of rails along the longitudinal axis on which a crossmember rides.

3. The refuelling system of claim 2 further comprising a longitudinal flexible track along the longitudinal axis wherein the longitudinal flexible track supports a flexible conduit for supply of fuel.

4. The refuelling system of claim 3 further comprising a flexible track within the crossmember wherein the flexible track within the crossmember supports a flexible conduit for supply of fuel, compressed air, vapor recovery, electrical power and control signals.

5. The refuelling system of claim 4 wherein the crossmember and the longitudinal flexible track support conduits for power and control signals.

6. The refuelling system of claim 1 wherein the rotating lower of the telescoping elements rotate about at least a 180°

arc.

7. The refuelling system of claim 1 wherein the plurality of vertically telescoping elements comprise a fixed upper segment and a movable segment that is attached to a movable pulley effective to guide at least one flexible conduit from a lower portion of the fixed upper segment to above the movable segment and down the inside of the movable segment.

8. The refuelling system of claim 7 further comprising a lower movable telescoping segment suspended from the movable segment, the at least one flexible conduit passing through the inside of the lower movable telescoping segment.

9. The refuelling system of claim 8 wherein the position of the movable segment is controlled by a threaded shaft that is rotatable and threadably connected to a ball nut fixed to the movable segment.

10. The refuelling system of claim 8 wherein the position of the lower movable telescoping segment is controlled by a rigid chain attached to a lower portion of the fixed upper segment, extending to an upper portion of the movable segment, and passing down through the movable segment and attached to the lower movable segment wherein the rigid chain if forced to turn essentially 180°

at the upper portion of the middle segment.

11. The refuelling system of claim 10 wherein the overhead gantry comprises a longitudinal axis and an axis essentially perpendicular to the longitudinal axis, and a set of rails along the longitudinal axis on which a crossmember rides.

12. The refuelling system of claim 11 further comprising a longitudinal flexible track along the longitudinal axis wherein the longitudinal flexible track supports a flexible conduit for supply of fuel.

13. The refuelling system of claim 12 further comprising a flexible track within the crossmember wherein the flexible track within the crossmember supports a flexible conduit for supply of fuel.

14. The refuelling system of claim 13 wherein the crossmember and the longitudinal flexible track support conduits for power and control signals.

15. The refuelling system of claim 14 wherein the rotating lower portion of the telescoping elements contain a purged section and a nonpurged segment.

16. The refuelling system of claim 1 wherein the rotating lower portion of the telescoping elements contain a purged section and a nonpurged segment.

17. The refuelling system of claim 16 wherein the purged section contains any electrical relays and valves required for operation of a refueling nozzle.

18. The refuelling system of claim 1 further comprising a bracket for support of a refuelling end effector wherein the bracket is rotatable about a horizontal axis.

19. The refuelling system of claim 1 further comprising a means effective to move the fuel nozzle to varying pitches.