Fully floating gangway

• US 6,678,910 B2
• Filed: 02/13/2002
• Issued: 01/20/2004
• Est. Priority Date: 10/19/2001
• Status: Expired due to Fees

• Current Assignee: Dave W. Smith
• Original Assignee: Dave W. Smith
• Inventors: Smith, Dave W.
• Primary Examiner(s): HARTMANN, GARY S
• Application Number:
  US10/073,325
• Publication Number:
  US 20030074749A1
• Time in Patent Office: 706 Days
• Field of Search: 14/695, 14/711, 14/725, 14/735, D34/32
• US Class Current: 14/69.5
• CPC Class Codes: B64F 1/305 Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable
• CPC Class Codes: B65G 69/2829 extensible by sliding parts
• CPC Class Codes: E01D 15/24 Bridges or similar structures, based on land or on a fixed structure and designed to give access to ships or other floating structures arrangement of ship-based ramps B63B27/14; loading ramps B65G69/28

Abstract

A fully floating gangway comprises a movable frame sandwiched movably in an operating plane between lower and upper parallel bearing surfaces which are supported from and positioned below a first platform. A gangway extends from the frame'"'"'s front end for extending to another platform such as an aircraft doorway so that the gangway can be aligned therewith by manipulating the frame in the operating plane. Preferably the frame and bearing surfaces are supported in a mobile structures such as passenger ramp. The gangway is preferably pivoted from the frame for adapting to differential elevations. The pivoting gangway can be counterbalanced for ease of manipulation. A braking system is provided to lock gangway against movement once positioned.

Claims

1. Apparatus for bridging between a first platform spaced from a second platform comprising:

a movable frame positioned below the first platform and substantially parallel thereto, the frame having a front end and a rear end and movable for translation or rotation within an operating plane; and

a bridge extending forward from the frame'"'"'s front end for extending between the first platform and the second platform, the bridge being pivotally connected to the frame at a pivot and the bridge weight being counterbalanced about the pivot by a spring acting relative to the frame, and so that, as the frame moves within its operating plane, the bridge also translates or rotates with respect to the second platform.

2. Apparatus for bridging between a first platform spaced from a second platform comprising:

a movable frame positioned below the first platform and substantially parallel thereto, the frame having a front end and a rear end and movable for translation or rotation within an operating plane;

a bridge extending forward from the frame'"'"'s front end for extending between the first platform and the second platform;

a lower bearing surface positioned below the frame and parallel to the operating plane;

an upper bearing surface positioned spaced above and parallel to the operating plane, the frame being movably supported between the upper and lower bearing surfaces in the operating plane;

one or more first bearings positioned rearwardly from the bridge pivot and for moveably supporting the front end of the frame so that downward load on the bridge loads the front end of the frame and causes the first bearings to bear against the lower bearing surface and causes the rear end of the frame to rotate upwardly; and

one or more second bearings positioned rearwardly of the first bearings so that, as the rear end of the frame rotates upwardly, the second bearings bear upwardly against the upper bearing surface so that, as the frame moves within its operating plane, the bridge also translates or rotates with respect to the second platform.

3. The apparatus of claim 2 wherein the bridge is pivotally connected to the frame at a pivot.

4. The apparatus of claim 3 wherein the bridge further comprises a flap extending rearwardly from the frame for interfacing between the bridge and the first platform as the frame moves.

5. The apparatus of claim 4 wherein the interfacing flap is pivoted from the frame.

6. The apparatus of claim 3 wherein the weight of the bridge is substantially counterbalanced about the pivot.

7. The apparatus of claim 2 wherein:

the first bearings comprise two or more freely swiveling front castors mounted to an underside of the frame, at least of two of which are spaced laterally; and

the second bearings comprise at least one freely swiveling rear castor mounted to a top of the frame, the front and rear castors permitting substantially full two dimensional translation and rotation of the frame in the operating plane so as to align the bridge with the second platform.

8. The apparatus of claim 7 wherein the angle of the first platform can be varied from horizontal and the apparatus further comprises a system for counteracting frame loads, the system comprising:

a counterweight surface positioned below the first platform and substantially parallel to the operating plane;

a counterweight supported moveably on the counterweight surface; and

a flexible tensile member extending forwards from the frame, around a turning bearing surface and back to the counterweight, so that as the first platform is angled from horizontal, the tendency of the frame to move down slope is counteracted by the counterweights tendency to move down slope.

9. The apparatus of claim 8 wherein the turning bearing surface is a pulley mounted adjacent the front of the lower beating surface.

10. The apparatus of claim 7 wherein the lower bearing surface has a breadth which is greater than the lateral spacing of the front casters.

11. The apparatus of claim 10 wherein the second platform is an aircraft doorway.

12. The apparatus of claim 11 wherein the first platform is a passenger ramp.

13. The apparatus of claim 7 further comprising a mechanism for locking the frame relative to the first platform whereby movement of the bridge from the second platform is avoided.

14. The apparatus of claim 13 wherein the locking mechanism comprises:

a first locking means fitted to the frame; and

a second locking means fitted to the first structure which is complementary for locking with the first locking means.

15. The apparatus of claim 14 wherein the first and second locking means comprise, in any order:

an indexing flap having perforations; and

one or more moveable pins, the pins and perforations being cooperatively spaced to ensure engagement of one or more of the one or more moveable pins regardless of the position of the frame.

16. Apparatus for bridging between a mobile structure spaced from an aircraft doorway comprising:

a movable frame positioned below the mobile structure and substantially parallel thereto, the frame having a front end and a rear end and movable for translation or rotation within an operating plane, the mobile structure having an access platform which can be positioned adjacent but not necessarily aligned with the aircraft doorway;

a gangway extending forward from the frame'"'"'s front end for extending to the aircraft doorway and so that, as the frame is manipulated to move within its operating plane, the gangway also translates or rotates with respect to the aircraft doorway for alignment therewith;

a lower bearing surface positioned below the frame and parallel to the operating plane; and

an upper bearing surface positioned spaced above and parallel to the operating plane, the frame being movably supported between the upper and lower bearing surfaces in the operating plane, one or more first bearings positioned rearwardly from the gangway pivot for moveably supporting the front end of the frame so that downward load on the gangway loads the front end of the frame and causes the first bearings to bear against the lower bearing surface and causes the rear end of the frame to rotate upwardly; and

one or more second bearings positioned rearwardly of the first bearings so that, as the rear end of the frame rotates upwardly, the second bearings bear upwardly against the upper bearing surface, so that the gangway can be aligned therewith by manipulating the frame to move within the operating plane.

17. The apparatus of claim 16 wherein:

the first bearings comprise two or more freely swiveling front castors mounted to an underside of the frame, at least of two of which are spaced laterally; and

the second bearings comprise at least one freely swiveling rear castor mounted to a top of the frame, the front and rear castors permitting substantially full two dimensional translation and rotation of the frame in the operating plane so as to align the bridge with the aircraft doorway.

18. The apparatus of claim 17 wherein the lower bearing surface has a breadth which is greater than the lateral spacing of the front casters so as to enable lateral movement of the frame.

19. The apparatus of claim 16 wherein the gangway is pivotally connected to the frame about a pivot.

20. The apparatus of claim 19 wherein the gangway further comprises a flap extending rearwardly for into acing between the gangway and the first platform as the frame moves, the interfacing flap being pivoted from the frame.

21. The apparatus of claim 19 wherein the weight of the gangway is substantially counterbalanced about the pivot.

22. The apparatus of claim 21 wherein the gangway is counterbalanced by a spring acting relative to the frame.

23. The apparatus of claim 16 further comprising a mechanism for locking the frame relative to the first platform for avoiding movement of the bridge from the second platform.

24. The apparatus of claim 23 wherein the looking mechanism comprises:

a first locking means fitted to the frame; and

a second locking means fitted to the first structure which is complementary for locking with the first locking means.

25. The apparatus of claim 24 wherein the first and second locking means comprise, in any order:

an indexing flap having perforations; and

one or more moveable pins, the pins and perforations being cooperatively spaced to ensure engagement of one or more of the one or more movable pins regardless of the position of the frame.

26. Apparatus for bridging between a mobile structure spaced from an aircraft doorway comprising;

a movable frame positioned below the mobile structure and substantially parallel thereto, the frame having a front end and a rear end and movable for translation or rotation within an operating plane, the mobile structure having an access platform which can be positioned adjacent but not necessarily aligned with the aircraft doorway; and

a gangway extending forward from the frame'"'"'s front end for extending to the aircraft doorway and so that, as the frame is manipulated to move within its operating plane, the gangway also translates or rotates with respect to the aircraft doorway for alignment therewith,

wherein the gangway is pivotally connected to the frame about a pivot and the weight of the gangway is substantially counterbalanced about the pivot by a spring acting relative to the frame.