Closure curtain for aircraft passenger boarding bridge cab

• US 5,267,368 A
• Filed: 09/24/1992
• Issued: 12/07/1993
• Est. Priority Date: 09/24/1992
• Status: Expired due to Fees

• Current Assignee: Blue Mountain Ventures Partnership
• Original Assignee: Blue Mountain Ventures
• Inventors: Saunders, Robert L.
• Primary Examiner(s): Eley, Timothy V.
• Application Number:
  US07/950,274
• Time in Patent Office: 439 Days
• Field of Search: 14/69.5, 14/71.5, 135/102, 135/103, 135/104, 135/106, 135/109, 135/111, 135/112, 135/113, 135/906
• US Class Current: 14/71.5
• CPC Class Codes: B64F 1/305 Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable

Abstract

A closure for a cab forming a longitudinally extending passageway that connects a passenger loading bridge to a doorway formed in the fuselage of an aircraft has a curtain with sleeves formed on the outer surface thereof which receive spaced pairs of vertical support members and horizontal support members which connect the outer ends of the vertical support members such that the curtain is suspended from the horizontal support members between the pairs of vertical support members.

Claims

1. A closure for a cab forming a longitudinally extending passageway that connects a passenger loading bridge to a doorway formed in the fuselage of an aircraft which comprises:

a support plate having a pair of laterally spaced side walls;

a plurality of longitudinally spaced pairs of rigid vertical support members having inner and outer ends;

pivot means for pivotally connecting the inner ends of said vertical support members to said side walls;

a plurality of rigid horizontal support members which extend between the outer ends of said pairs of vertical support members;

attachment means for attaching the ends of said horizontal support members to said outer ends of said vertical support members such that said pairs of vertical support members and said horizontal support members form a curtain frame;

a curtain having an inner side surface and an outer side surface; and

a plurality of longitudinally spaced laterally extending sleeves formed on the outer surface of said curtain adapted to receive said pairs of vertical support members and said horizontal support members such that said curtain is suspended from said horizontal support members between said pairs of vertical support members.

2. The closure of claim 1 in which said attachment means includes second pivot means for pivotally connecting said horizontal members to said outer ends about a vertical axis;

and wherein said attachment means operates to prevent lateral movement of said horizontal members.

3. The closure of claim 1 in which said attachment means is detachable to enable said horizontal support members to be detached from said vertical support members.

4. The closure of claim 1 in which the first said pivot means includes a plurality of rigid pivot blocks each of which receives said inner end of one of said vertical support tubes and a plurality of fasteners each of which pivotally connects one of said pivot blocks to said support plate side wall for movement about a horizontal axis.

5. The closure of claim 4 further including two strips of adhesive backed bearing material having an adhesive on one side and a bearing material on the other side, said adhesive sides being attached one to each of said support plate side walls with said bearing material interposed between said pivot block and said side wall.

6. The closure of claim 1 further comprising restraint means connected to the outer ends of said vertical support members to limit the pivotal movement of the outer ends.

7. A closure for a cab forming a longitudinally extending passageway that connects a passenger loading bridge to a doorway formed in the fuselage of an aircraft which comprises:

a support plate having a pair of laterally spaced side walls;

a plurality of longitudinally spaced pairs of rigid vertical support members having inner and outer ends;

a pair of segmented vertical support members positioned one on each side of said support plate;

each of said segmented vertical support members having an inner segment pivotally connected to an outer segment;

pivot means for pivotally connecting the inner ends of said rigid vertical support members and the inner ends of said inner segments to said side walls;

wherein said segmented vertical support members are positioned at the aircraft end of said support plate;

a plurality of rigid horizontal support members which extend between the outer ends of said rigid pairs of vertical support members and the outer ends of said outer segments;

attachment means for attaching the ends of said horizontal support members to said outer ends of said rigid vertical support members and the outer ends of said outer segments;

a curtain having an inner side surface and an outer side surface; and

a plurality of longitudinally spaced laterally extending sleeves formed on the outer surface of said curtain adapted to receive said pairs of rigid and said segmented vertical support members and said horizontal support members such that said curtain is suspended from said horizontal support members between said pairs of said rigid and segmented vertical support members.

8. The closure of claim 7 in which said attachment means includes second pivot means for pivotally connecting said horizontal members to said outer ends about a vertical axis;

and

wherein said attachment means operates to prevent lateral movement of said horizontal members.

9. The closure of claim 7 in which said attachment means is detachable to enable said horizontal support members to be detached from said rigid and said segmented vertical support members.

10. The closure of claim 7 in which the first said pivot means includes a plurality of rigid pivot blocks of which each receives said inner end of one of said rigid and segmented vertical support tubes and a plurality of fasteners one of which pivotally connects each of said pivot blocks to said support plate side wall for movement about a horizontal axis.

11. The closure of claim 10 further comprising two strips of adhesive backed bearing material each having an adhesive on one side and a bearing material on the opposite side, said adhesive side being attached each to one of said support plate side walls with said bearing material side interposed between said pivot blocks and said side walls.

12. The closure of claim 7 further comprising connecting means for connecting each of said segmented vertical support members to its adjacent rigid vertical support member.

13. The closure of claim 7 further comprising restraint means connected to one outer ends of said vertical support members to limit the pivotal movement of these outer ends.

14. A closure for a cab forming a longitudinally extending passageway that connects a passenger loading bridge to a doorway formed in the fuselage of an aircraft and movable between a retracted position in which the outer end of said closure is moved toward said bridge and an extended position in which said outer end of said closure is moved away from said bridge and has a positive curvature which substantially complements that of the fuselage of an adjacent aircraft which comprises:

a support plate having a pair of laterally spaced side walls;

a plurality of longitudinally spaced pairs of rigid vertical support members having inner and outer ends;

a pair of segmented vertical support members positioned one on each side of said support plate;

each of said segmented vertical support members having an inner segment pivotally connected to an outer segment;

a pair of longitudinally flexible vertical pad supports having inner and outer ends positioned one on each side of said support plate;

pivot means for pivotally connecting the inner ends of said rigid vertical support members to said side walls;

first connecting means for connecting the inner ends of said vertical pad supports to said support plate;

second connecting means for connecting the inner ends of said inner segments to said side walls;

wherein said vertical pad supports are positioned at the aircraft end of said support plate and said segmented vertical support members are positioned between said rigid vertical support members and said pad support;

a plurality of rigid horizontal support members which extend between the outer ends of said rigid pairs of vertical support members and the outer ends of said outer segments;

attachment means for attaching the ends of said horizontal support members to said outer ends of said rigid vertical support members and the outer ends of said outer segments;

a longitudinally flexible horizontal pad support which extends between the outer ends of said vertically pad supports;

a curtain having an inner side surface and an outer side surface;

a plurality of longitudinally spaced laterally extending sleeves formed on the outer surface of said curtain adapted to receive said pairs of rigid and said segmented vertical support members and said horizontal support members such that said curtain is suspended from said horizontal support members between said pairs of said rigid and said segmented vertical support members;

first fastening means for fastening said curtain to said vertical pad supports; and

second fastening means for fastening said curtain to said horizontal pad support.

15. The closure of claim 14 in which said attachment means includes second pivot means for pivotally connecting said horizontal members to said outer ends about a vertical axis;

and

wherein said attachment means operates to prevent lateral movement of said horizontal members.

16. The closure of claim 14 in which said attachment means is detachable to enable said horizontal support members to be detached from said rigid and said segmented vertical support members.

17. The closure of claim 14 in which the first said pivot means includes a plurality of rigid pivot blocks of which each receives said inner end of one of said rigid and segmented vertical support tubes and a plurality of fasteners one of which pivotally connects each of said pivot blocks to said support plate side wall for movement about a horizontal axis.

18. The closure of claim 14 further comprising connecting means for connecting each of said segmented vertical support members to its adjacent rigid vertical support member such that each of said inner segments pivots with its adjacent vertical support member.

19. The closure of claim 14 further comprising two strips of adhesive backed bearing material each having an adhesive on one side and a bearing material on the opposite side, said adhesive side being attached each to one of said support plate side walls with said bearing material side interposed between said pivot blocks and said side wall.

20. The closure of claim 14 further comprising restraint means connected to the outer ends of said vertical support members to limit the pivotal movement of these outer ends when said closure is in said extended position.

21. The closure of claim 14 in which said vertical pad supports are formed from a single piece of metal which may be flexed in a longitudinal direction but resists flexing in a lateral direction.

22. The closure of claim 14 in which the inner end of at least one of said vertical pad supports is rigidly affixed to said support plate.

23. The closure of claim 14 in which said vertical pad supports are formed from a plurality of segments which are hinged together to provide a support which may be flexed in a longitudinal direction but resists flexing in a lateral direction.

24. The closure of claim 14 in which said first fastening means includes a hook and loop type fastener in which one of said hook or said loop is attached to said vertical pad supports and the other of said hook or said loop is attached to said curtain.

25. The closure of claim 14 in which said second fastening means includes a hook and loop type fastener in which one of said hook or said loop is attached to said horizontal pad support and the other of said hook or said loop is attached to said curtain.

26. The closure of claim 14 further comprising two sets of negative curvature restraint blocks attached one set to each of said vertical pad supports;

each set of blocks extending from one end of said vertical pad support to the other end thereof;

said blocks in each set being aligned such that one edge of each block is in contact with an edge of an adjacent block when said closure is in said retraced position and said vertical pad support is unflexed and extend substantially in a straight line to prevent said support from flexing in negative direction towards said bridge; and

said edges of adjacent blocks are disengaged when said closure is in said extended position and said vertical pad support is flexed in a positive direction away from said bridge.

27. The closure of claim 26 further comprising a pair of positive curvature restraint straps;

third fastening means for fastening one strap to each of said negative curvature restraint blocks on one of said vertical pad supports to limit the maximum curvature of said pad supports in a positive direction when said support is flexed in a positive direction.

28. The closure of claim 27 in which said third fastening means includes adjustment means for adjusting the length of said positive curvature restraint straps to provide the proper maximum curvature of said pad supports in a positive direction to enable said closure to accommodate different sized aircraft fuselages.

29. The closure of claim 26 further comprising a pair of negative restraint blocks affixed one to each end of said horizontal pad support and in alignment with the set of negative restraint blocks on one of said vertical pad supports;

and resilient alignment means for connecting each of said end blocks on said horizontal pad support to the adjacent block at the end of a vertical pad support to limit the movement of the ends of said horizontal pad support with respect the outer ends of the vertical pad supports.

30. The closure of claim 26 further comprising a plurality of negative curvature restraint blocks attached to said horizontal pad support and aligned such that one edge of each block is in contact with an edge of an adjacent block when said closure is in said retracted position and said horizontal pad support is unflexed and extend substantially in a straight line to prevent one end of said horizontal support form flexing in a negative direction towards said bridge and said edge of adjacent blocks are separated when said closure is in said extended position and one end of said horizontal pad support is flexed in a positive direction away from said bridge.

31. The closure of claim 26 further comprising a horizontal positive curvature restraint strap;

fourth fastening means for fastening said strap to each of said negative curvature restraint blocks on one of said horizontal pad support to limit the maximum curvature of said pad support in a positive direction.

32. The closure of claim 31 in which said fourth fastening means includes adjustment means for adjusting the length of said horizontal positive curvature restraint strap to provide the proper maximum curvature of said horizontal pad support in a positive direction to enable said closure to accommodate different sized aircraft fuselages.

33. The closure of claim 26 further comprising a vertical pad detachably attached to each of said vertical pad supports and a horizontal pad detachably attached to said horizontal pad support.