Flexible over the wing passenger loading bridge

• US 6,931,687 B2
• Filed: 01/30/2003
• Issued: 08/23/2005
• Est. Priority Date: 02/01/2002
• Status: Expired due to Fees

• Current Assignee: DEW Engineering and Development Limited (Trelleborg AB)
• Original Assignee: DEW Engineering and Development Limited (Trelleborg AB)
• Inventors: Nowak, Christopher, Hutton, Neil
• Primary Examiner(s): Will, Thomas B.
• Assistant Examiner(s): Pechhold, Alexandra K.
• Application Number:
  US10/354,003
• Publication Number:
  US 20030145401A1
• Time in Patent Office: 936 Days
• Field of Search: 14/711, 14/695, 14/713, 14/715, 14/717, 14/725, 702/150, 702/151, 702/159, 382/104
• US Class Current: 14/71.5
• CPC Class Codes: B64F 1/3055 with hinged head interface between aircraft and passenger bridge

Abstract

Apparatus for moving passengers between an airport terminal building and a doorway of an aircraft located rearward of a wing of the aircraft which includes a passageway member pivotally anchored to one of the terminal building and a passenger loading bridge for servicing a front doorway of a same aircraft. The apparatus includes a telescopic passageway member that is pivotally mounted to the passageway member via a flexible connection. In use, the apparatus is cantilevered over the wing of an aircraft with the flexible connection substantially above a highest point along an upper surface of the aircraft wing. The flexible connection allows a cabin carried at an outboard end of the telescopic passageway member to mate to the rear doorway of the aircraft, providing an open passageway between the rear doorway and the terminal building through which passengers deplane. Positioning the flexible connection above the high point of the wing approximately minimizes the inclination of each passageway member floor surface.

Claims

1. A method of automatically aligning a passenger loading bridge to an aircraft having a rear doorway aft of or over a wing, comprising:

a) automatically determining a type of the aircraft;

b) retrieving information relating to an expected stopping position for the rear doorway of the determined type of the aircraft;

c) retrieving other information relating to a predetermined minimum height profile for allowing the passenger loading bridge to maintain a desired minimum safe distance relative to the wing of the aircraft;

d) waiting for the aircraft to stop;

e) automatically moving an aircraft engaging end of the passenger loading bridge toward the expected stopping position of the rear doorway for the determined type of the aircraft; and

f) moving an outboard portion of the passenger loading bridge relatively to an inboard portion of the passenger loading bridge about a first flexible connection disposed therebetween, and adjusting a height of the first flexible connection by pivoting the inboard portion of the passenger loading bridge about a second flexible connection, such that during (e) a point along the lower surface of the passenger loading bridge remains above the predetermined minimum height profile of the wing of the aircraft.

2. A method according to claim 1 wherein the predetermined minimum height profile relates to a height of the point along the lower surface of the passenger loading bridge, at which height every point along the lower surface of the passenger loading bridge is at least the desired minimum safe distance above a corresponding point on the wing of the aircraft.

3. A method according to claim 1 including:

coupling the aircraft engaging end of the passenger loading bridge to the rear doorway of the aircraft;

when coupled, sensing a vertical displacement of the wing of the aircraft relative to the passenger loading bridge; and

automatically moving the passenger loading bridge in dependence upon the sensed vertical displacement of the wing, so as to maintain the desired minimum safe distance between the wing of the aircraft and the passenger loading bridge.

4. A method according to claim 1 including coupling the aircraft engaging end of the passenger loading bridge to the rear doorway of the aircraft, wherein, when coupled, the outboard portion of the passenger loading bridge is aligned substantially parallel to an upper surface of the wing of the aircraft.

5. A method according to claim 1 including prior to determining a type of the aircraft:

waiting to receive a control signal for enabling an automated bridge control system to automatically align the passenger loading bridge to the rear doorway of the aircraft.

6. A method according to claim 5 wherein determining a type of the aircraft includes:

a1) in dependence upon receiving the control signal, capturing an image of the aircraft;

a2) characterizing the image of the aircraft to extract features relating to the aircraft;

a3) comparing the extracted features with stored template features; and

,

a4) identifying the type of the aircraft in dependence upon a result of the comparison.

7. A method according to claim 5 wherein determining a type of the aircraft includes:

a1) extracting from the control signal, data relating to the type of the aircraft; and

a2) based on the extracted data, identifying the type of the aircraft.

8. A method according to claim 1 including prior to waiting for the aircraft to stop:

c1) moving the passenger loading bridge to a predetermined pre-position for avoiding contact with determined type of the aircraft.

9. A method according to claim 1 wherein automatically moving an aircraft engaging end of the passenger loading bridge toward the expected stopping position of the rear doorway for the determined type of the aircraft includes:

e1) positioning the flexible connection of the passenger loading bridge approximately above a leading edge of the wing of the aircraft and at a height that is sufficient for allowing the point along the lower surface of the passenger loading bridge to remain above the predetermined minimum height profile of the wing of the aircraft.

10. A method according to claim 1 wherein automatically moving an aircraft engaging end of the passenger loading bridge toward the expected stopping position of the rear doorway for the determined type of the aircraft includes:

e1) sensing a distance between the passenger loading bridge and the aircraft;

e2) comparing the sensed distance to the desired minimum safe distance; and

e3) when the sensed distance is i) one of greater than and equal to the desired minimum safe distance, continuing the movement of the bridge toward the expected stopping position of the rear doorway for the determined type of aircraft, and ii) less than the desired minimum safe distance, moving the bridge along a predetermined escape route in a direction away from the aircraft.

11. A method according to claim 1 wherein automatically moving an aircraft engaging end of the passenger loading bridge toward the expected stopping position of the rear doorway for the determined type of the aircraft includes:

e1) sensing a distance between the passenger loading bridge and the aircraft;

e2) comparing the sensed distance to the desired minimum safe distance; and

e3) when the sensed distance is i) one of greater than and equal to the desired minimum safe distance, continuing the movement of the bridge toward the expected stopping position of the rear doorway for the determined type of aircraft, and ii) less than the desired minimum safe distance, correcting the predetermined minimum height profile such that, during future motion, the sensed distance is at least equal to the desired minimum safe distance.

12. A method of automatically aligning a passenger loading bridge to an aircraft having a rear doorway aft of or over a wing, comprising:

adjusting a height of a flexible connection disposed between an outboard portion and an inboard portion of the passenger loading bridge to a first height;

adjusting a height of an aircraft engaging end of the passenger loading bridge by relatively moving the outboard portion and the inboard portion of the passenger loading bridge about the flexible connection, so as to adjust an angle between the outboard portion and the inboard portion of the passenger loading bridge about the flexible connection while maintaining the flexible connection at approximately the first height; and

,

moving the aircraft engaging end over the wing of the aircraft in a direction that is toward the rear doorway of the aircraft.

13. A method according to claim 12, wherein the first height is selected to provide a desired minimum safe distance between an upper surface of the wing of the aircraft and the passenger loading bridge.

14. A method according to claim 12, wherein the first height is a height that is above an upper surface of the wing of the aircraft.

15. A method according to claim 14, wherein the first height is selected to provide a desired minimum safe distance between the upper surface of the wing of the aircraft and the passenger loading bridge.

16. A method according to claim 12, comprising:

controllably varying a length of the outboard portion of the passenger loading bridge such that the aircraft engaging end is substantially aligned with the rear doorway of the aircraft.

17. A method according to claim 16, comprising:

coupling the aircraft engaging end of the passenger loading bridge with the rear doorway of the aircraft, so as to support passenger movement therebetween.

18. A method according to claim 12, comprising:

coupling the aircraft engaging end of the passenger loading bridge with the rear doorway of the aircraft, so as to support passenger movement therebetween.

19. A method according to claim 17, comprising:

when coupled, sensing a vertical displacement of the wing of the aircraft relative to the passenger loading bridge; and

automatically moving the passenger loading bridge in dependence upon the sensed vertical displacement of the wing, so as to maintain a desired minimum safe distance between the wing of the aircraft and the passenger loading bridge.

20. A method according to claim 12, comprising:

positioning the flexible connection of the passenger loading bridge approximately vertically above a leading edge of the wing of the aircraft.