WO1996023715A1 - Passageway for loading and unloading aircraft - Google Patents

Passageway for loading and unloading aircraft Download PDF

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Publication number
WO1996023715A1
WO1996023715A1 PCT/US1996/001312 US9601312W WO9623715A1 WO 1996023715 A1 WO1996023715 A1 WO 1996023715A1 US 9601312 W US9601312 W US 9601312W WO 9623715 A1 WO9623715 A1 WO 9623715A1
Authority
WO
WIPO (PCT)
Prior art keywords
passageway
frame
passageway according
frame sections
frame section
Prior art date
Application number
PCT/US1996/001312
Other languages
French (fr)
Inventor
James Larson
Original Assignee
Commute-A-Walk, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Commute-A-Walk, Inc. filed Critical Commute-A-Walk, Inc.
Priority to CA002187011A priority Critical patent/CA2187011C/en
Priority to DK96903751T priority patent/DK0752969T3/en
Priority to AU47734/96A priority patent/AU4773496A/en
Priority to DE69602497T priority patent/DE69602497T2/en
Priority to EP96903751A priority patent/EP0752969B1/en
Publication of WO1996023715A1 publication Critical patent/WO1996023715A1/en
Priority to FI963946A priority patent/FI963946A/en
Priority to MXPA/A/1996/004533A priority patent/MXPA96004533A/en
Priority to NO964181A priority patent/NO303382B1/en
Priority to GR990402111T priority patent/GR3031033T3/en

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Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H15/00—Tents or canopies, in general
    • E04H15/32—Parts, components, construction details, accessories, interior equipment, specially adapted for tents, e.g. guy-line equipment, skirts, thresholds
    • E04H15/34—Supporting means, e.g. frames
    • E04H15/44—Supporting means, e.g. frames collapsible, e.g. breakdown type
    • E04H15/48—Supporting means, e.g. frames collapsible, e.g. breakdown type foldable, i.e. having pivoted or hinged means
    • E04H15/50—Supporting means, e.g. frames collapsible, e.g. breakdown type foldable, i.e. having pivoted or hinged means lazy-tongs type
    • E04H15/505—Supporting means, e.g. frames collapsible, e.g. breakdown type foldable, i.e. having pivoted or hinged means lazy-tongs type characterised by connecting arches with lazy-tongues
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/30—Ground or aircraft-carrier-deck installations for embarking or disembarking passengers
    • B64F1/305—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable

Definitions

  • the present invention relates to apparatus permitting the swift and safe loading of small aircraft and in particular to a walkway for the protective movement of passengers to and from commuter aircraft.
  • gangways for large aircraft are shown in U. S. Patent 3,683,440; 4,559,660 and 4,984,321.
  • the conventional gangway is essentially a movable articulating steel enclosed corridor or bridge which when docked to an airplane provides a safe pathway for passenger traffic to and from the terminal.
  • These jet bridges as they are known, were designed and intended for use only with large jet engine type aircraft (i.e. Boeing 727, 737, 757, 767, 747) with door sill height ranging between 6' to 16' above ground.
  • Such jet bridges cannot be used for commuter type aircraft which are only a fraction of the height of the jet airplanes and have a door sill well below 6 feet.
  • the smaller commuter aircraft are loaded at ground level and are provided with their own stairway.
  • a weatherproof passageway comprising a series of expandable frame sections which sections stand on wheel assemblies so as to move easily across a pavement or concrete apron.
  • the frame sections are joined in an articulated manner so that the plurality of frame sections are deployable over a large distance and flexible to swing into position properly docking at the door of the aircraft.
  • Over the top of each frame section is a weatherproof fabric cover.
  • Interior fabric panels are suspended inside the walls to hang vertically on both sides to enclose the frame section.
  • the cover and interior panel are spaced to provide a continuous wind relief pocket therebetween thereby reducing the chance of the extended passageway capsizing or overturning in severe weather conditions.
  • each of the frame sections are identical and are joined together front to back with a simple or latch mechanism.
  • the fabric cover and interior panels are preferably secured by VELCRO fasteners both to the frame sections and to each other.
  • the walls of the frame sections are formed utilizing a scissor-like stud assembly so as to enable easy extension and collapse as well as flexible travel.
  • the design is such that the passageway can be deployed manually, it is preferred to deploy and stow the unit via a uniquely built electro-mechanical powered drive unit.
  • Fig. 1 is schematic plan view of a multi-sectional passageway embodying the present invention shown docked with a commuter aircraft;
  • Fig. 2 is a perspective view of one section of the passageway shown in Fig. 1;
  • Fig. 3 is a perspective view of several sections of the passageway and drive unit.
  • the inventive passageway generally illustrated by the numeral 10 is schematically illustrated in Fig. 1.
  • the passageway 10 is secured at its rear end to the apron wall of the terminal 12 so as to cover the exit gate 14 and is extendible outwardly therefrom so that its forward end will dock with the commuter airplane 16 so as to cover the entrance 18 to the airplane.
  • the passageway 10 is formed of a plurality of collapsible frame sections 20, each wheel mounted on casters or rollers to be easily movable over the concrete apron or tarmac.
  • Each of the sections 20 are joined together serially so that the passageway maybe deployed in extended condition in a manner to provide flexibility along its length and so that it may be radiused or swingable into an arc. In this way the airplane 16 can even be parked with its entrance perpendicular and offset to the terminal gate 14.
  • the passageway is likewise collapsible for stowing.
  • passageway may be manually deployed and stowed, it is preferred to provide an electro/mechanical drive unit 22 which is easily attached to the front section so as to facilitate the movement particularly during high peak times.
  • the drive unit 22 will also allow a collapsed passageway to be transported from one gate to another so that a single passageway may serve several gates.
  • each frame section 20 comprises a pair of laterally opposed spaced side walls 24, each wall comprising a forward stanchion 26 and a rear stanchion 28 joined by a scissor like stud assembly 30 .
  • the elements of the frame section are preferably formed of metallic bar stock or hollow tubing. Aluminum members may also be used.
  • Each stanchion 26 and 28 is welded at its lower end to a mounting bracket 32 of wheel assembly 34.
  • the laterally opposed stanchions 26, 28 at the front and rear of each of the paired side walls are respectively joined by a U-shaped brace forming a roof arch beam 36 and having legs 38 which extend along the entire length of the stanchions 26 and 28.
  • the legs 38 are also welded at their lower ends to the wheel assembly support bracket 32.
  • the wheel assemblies are preferably in the form of casters, or rollers which swivel about a vertical axis, thus permitting the frame to be easily moved.
  • each frame section 20 takes on the attribute of being integrally built as a complete unit while maintaining relative movement of the front and rear stanchions with respect to each other.
  • the scissor-like stud assembly 30 comprises a pair of pivoted bars 42 which criss-cross over themselves each being pivotally fixed at one end 44 to the upper ends of the respective stanchions 26, 28.
  • the lower ends 46 of the bars 42 are slidably held in a slotted guide 48 integrally formed on the inner side of the opposite stanchion 26, 28.
  • the slotted guide 48 is mounted at the lower ends of the stanchions 26, 28 and have a length about 10 to 12 inches.
  • the crossing bars overlap each other and may be mutually provided with cut-outs 50 permitting the bars 42 to pivot over each other much like the action of a scissor. They may also be connected with a pivot pin 52 at their crossing point to increase rigidity of the wall.
  • the lower ends of each bar 42 may be provided with laterally extending pins or flanges so as to be able to ride in the slotted guide without being detached therefrom, during movement.
  • the cover 54 Draped over the frame section and resting on the top of the roof arch 38 is « weatherproof (and, if desired, flameproof) fabric cover 54 which is preferably held in place by providing the cover 54 and the outer surface of the roof arch with mating VELCRO strips 56. Similarly, the leading and trailing edges of the cover 54 can also be provided with VELCRO strips 58 on its upper and lower surfaces so that the cover 54 of one section can be secured to that of its adjacent sections. If desired, cord lashing or other fastening means may be used.
  • the lower edge 60 of the exterior covers 54 can fall below the arc of the roof arch, but it preferably does not extend fully down the side wall.
  • the fabric weatherproof material used as the exterior cover 54 may be of any kind, although preferably the material sold under the trademark (BridgeTech Inc. , Brentwood, NY) which is used in the more common fixed loading bridges may be used here.
  • each wall 24 Mounted on the interior of each wall 24 is vertical panel 62 which may have at least its upper half 64 of transparent material.
  • the interior panel 62 is attached to the wall, employing a mounting bar 66 fixed to the stanchions 26 and 28 to which VELCRO strips 68 may be secured.
  • the leading and trailing edges of the panel 62 are also provided with VELCRO strips to secure the panel.
  • small hooks 70 spaced along the length of the bar may be used with the leading and trailing edge of the panel 62 provided with corresponding spaced grommets 72 which fit over the hooks 70.
  • the interior panel 62 may be made of the same weatherproof and fireproof material as the exterior cover 54 although this is not critical as the panel 62 is sheltered somewhat from the weather.
  • the panels 62 may be of vinyl material, canvas or other long lasting fabric.
  • each frame section 20 is itself collapsible and extendible. Depending upon the exact geometric length of the stanchions and the connecting scissor stud assembly, the frame section can be extended as much as 48" and collapsed to approximately 6 inches. Of course, by varying the geometry the length can be varied. In practice it has been found that a commuter aircraft are generally parked between 50-100 feet from the terminal. Therefore, a train of approximately 20 frame sections should be sufficiently long when deployed. If necessary more or fewer sections can be used.
  • a train or series of sections are formed by providing the front stanchions and the rear stanchions with cooperating latch or connecting means whereby adjacent frame sections be articulately connected.
  • the front stanchions 26 may be provided with eye bolts 74 or other forms of staples while the rear stanchions are provided with pivotable latches.
  • Other standard fastening means may be employed.
  • a resilient elastic strap 78 may be stretched between the front frame section and the last frame section on each side.
  • the exterior faces of the stanchions 26, 28 are provided with U-shaped handles 80 through which the strap 78 passes.
  • the leading frame section will dock in abutment with the aircraft, straddling the staircase 82 which leads down from the aircraft and may be secured to the stairs. If this cannot be done then the staircases may be enclosed by an extendible belt 84 and portable stanchions 86.
  • the leading frame section differs from the other frame sections in minor ways. First the roof 88 of the leading frame section is extended forwardly and upwardly following the line of the aircraft stairs 82 so that it terminates above the aircraft entrance 18. In addition, the edge of the roof 88 is padded as at 90 so as to softly abut against the aircraft. Solar powered battery operated lights 92 for general illumination. The leading frame section may also be provided with forwardly directed docking lights 94.
  • the wheel assembly support bracket 32 may be slightly enlarged to allow the portable stanchion 86 to be placed thereon during deployment or storage of the passageway.
  • a significant modification to the leading frame section may be described in that the scissor-like stud assembly 42 is arranged so as not to be collapsible.
  • the criss-crossing studs may be locked together by suitable bolt means, in view of pivot pin 52.
  • the leading frame section is, of course, hooked to the drive unit for deployment by suitable latch means.
  • the drive unit 22 comprises a small wheeled truck 94 accommodating one operator and is provided with an electric propulsion motor 96 having a battery and charging system, control mechanisms such as forward/reverse 98, left/right 100 and hydraulic brake 102.
  • the drive unit 22 and the front stanchion of the leading frame section are provided with cooperating hook and latch members 106 allowing the drive unit to be removably attached to the passageway whereby it may move and maneuver the passageway into deployment or storage position.
  • a significant advantage of the present invention lies in the absence of a floor for the frame sections.
  • the frame sections are thus light in weight and materially cheaper to construct.
  • the frame sections each roll easily over the ground. Small accumulation of snow or debris on the ground will not interfere with movement. Larger accumulations will normally not exit, being uncovered promptly by airport personnel.
  • the passageway is easily used and moved into position relative to the aircraft, no matter the parked position of the aircraft. Since the frame sections are identical they may be easily removed from or added to the passageway so that even the length of the fully extended passageway may be varied.
  • the passageway as a whole is designed to be independent of any permanent facility and may be moved from terminal gate to terminal gate, when necessary.
  • the wheel support brackets 32 may be vertically offset so as not to interfere with each other when the passageway is collapsed.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Paper (AREA)
  • Spinning Or Twisting Of Yarns (AREA)
  • Storage Of Web-Like Or Filamentary Materials (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Escalators And Moving Walkways (AREA)
  • Packaging Of Machine Parts And Wound Products (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
  • Ship Loading And Unloading (AREA)
  • Control And Safety Of Cranes (AREA)
  • Bridges Or Land Bridges (AREA)
  • Lining And Supports For Tunnels (AREA)

Abstract

A plurality of independent U-shaped frame sections (20) are articulately connected in an end series to form a flexible corridor (10). Each frame section (20) is U-shaped being opened at the bottom and supported on a wheel assembly (34) and covered by a weatherproof fabric roof (54). Each frame section (20) is formed with collapsible side walls (24) allowing collapsing in the longitudinal direction.

Description

Title: PASSAGEWAY FOR LOADING AND UNLOADING AIRCRAFT
Background of the Invention
The present invention relates to apparatus permitting the swift and safe loading of small aircraft and in particular to a walkway for the protective movement of passengers to and from commuter aircraft.
Examples of gangways for large aircraft are shown in U. S. Patent 3,683,440; 4,559,660 and 4,984,321. The conventional gangway is essentially a movable articulating steel enclosed corridor or bridge which when docked to an airplane provides a safe pathway for passenger traffic to and from the terminal. These jet bridges, as they are known, were designed and intended for use only with large jet engine type aircraft (i.e. Boeing 727, 737, 757, 767, 747) with door sill height ranging between 6' to 16' above ground. Such jet bridges cannot be used for commuter type aircraft which are only a fraction of the height of the jet airplanes and have a door sill well below 6 feet. Further, the smaller commuter aircraft are loaded at ground level and are provided with their own stairway. At present there is no bridge or pathway apparatus which can dock with a commuter aircraft on ground level having the capability of extending and retracting while simultaneously swinging left and right, so as to meet the aircraft where parked.
Presently, some users have constructed short permanent type awning walkways which protect passengers only part of the way to the aircraft. Due to the nature of commuter aircraft operation, no permanent fixed structure can be constructed so as to extend all the way out from the terminal to the parking position because it will interfere with and prohibit the aircraft from parking or eventually turn out under its own power for departure. Therefore, commuter airline passengers have always had to walk to the aircraft in an uncontrolled dangerous environment across the aircraft apron or airport tarmac. This exposure places the passengers in an endless amount of danger, chaos, inclement weather and inconvenience.
It is an object of the present invention to provide an apparatus overcoming the disadvantages inherent in present commuter aircraft loading and to provide a safe and protective walkway for the passengers.
It is an object of the present invention to provide a passenger walkway for "zero" height application and at the same time be capable of extending, retracting and radiusing left and right.
It is a further object of the present invention to make the apparatus totally self-contained and mobile so as to be utilized at any gate location of the user's terminal facilities throughout the entire terminal network, in other words, completely independent from any permanent facility.
It is a particular object of the present invention to form the passageway of generic interchangeable sections so the user can readily accommodate the ongoing changing criteria of aircraft operations without costly engineering expense.
These objects and others together with their advantages and uses will be apparent from the following description of the present invention. Brief Statement of the Invention
In accordance with the present invention there is provided a weatherproof passageway comprising a series of expandable frame sections which sections stand on wheel assemblies so as to move easily across a pavement or concrete apron. The frame sections are joined in an articulated manner so that the plurality of frame sections are deployable over a large distance and flexible to swing into position properly docking at the door of the aircraft. Over the top of each frame section is a weatherproof fabric cover. Interior fabric panels are suspended inside the walls to hang vertically on both sides to enclose the frame section. The cover and interior panel are spaced to provide a continuous wind relief pocket therebetween thereby reducing the chance of the extended passageway capsizing or overturning in severe weather conditions. Preferably, each of the frame sections are identical and are joined together front to back with a simple or latch mechanism. The fabric cover and interior panels are preferably secured by VELCRO fasteners both to the frame sections and to each other.
The walls of the frame sections are formed utilizing a scissor-like stud assembly so as to enable easy extension and collapse as well as flexible travel. Although the design is such that the passageway can be deployed manually, it is preferred to deploy and stow the unit via a uniquely built electro-mechanical powered drive unit.
Full details of the present invention are set forth in the following description and accompanying illustration of the preferred method and product. Brief Description of the Drawings
In the drawings:
Fig. 1 is schematic plan view of a multi-sectional passageway embodying the present invention shown docked with a commuter aircraft;
Fig. 2 is a perspective view of one section of the passageway shown in Fig. 1; and
Fig. 3 is a perspective view of several sections of the passageway and drive unit.
Description of the Invention
The inventive passageway generally illustrated by the numeral 10 is schematically illustrated in Fig. 1. In use the passageway 10 is secured at its rear end to the apron wall of the terminal 12 so as to cover the exit gate 14 and is extendible outwardly therefrom so that its forward end will dock with the commuter airplane 16 so as to cover the entrance 18 to the airplane. The passageway 10 is formed of a plurality of collapsible frame sections 20, each wheel mounted on casters or rollers to be easily movable over the concrete apron or tarmac. Each of the sections 20 are joined together serially so that the passageway maybe deployed in extended condition in a manner to provide flexibility along its length and so that it may be radiused or swingable into an arc. In this way the airplane 16 can even be parked with its entrance perpendicular and offset to the terminal gate 14. The passageway is likewise collapsible for stowing.
While the passageway may be manually deployed and stowed, it is preferred to provide an electro/mechanical drive unit 22 which is easily attached to the front section so as to facilitate the movement particularly during high peak times. The drive unit 22 will also allow a collapsed passageway to be transported from one gate to another so that a single passageway may serve several gates.
The construction of each frame section 20 is shown in detail in Fig. 2. Each frame section 20 comprises a pair of laterally opposed spaced side walls 24, each wall comprising a forward stanchion 26 and a rear stanchion 28 joined by a scissor like stud assembly 30 . The elements of the frame section are preferably formed of metallic bar stock or hollow tubing. Aluminum members may also be used. Each stanchion 26 and 28 is welded at its lower end to a mounting bracket 32 of wheel assembly 34. The laterally opposed stanchions 26, 28 at the front and rear of each of the paired side walls are respectively joined by a U-shaped brace forming a roof arch beam 36 and having legs 38 which extend along the entire length of the stanchions 26 and 28. The legs 38 are also welded at their lower ends to the wheel assembly support bracket 32. The wheel assemblies are preferably in the form of casters, or rollers which swivel about a vertical axis, thus permitting the frame to be easily moved.
In addition spacers 40 are arranged at intervals between the legs 38 of the U-shaped brace and the adjacent stanchions 26, 28 being also welded thereto. Thus, by fixedly joining each of the paired front stanchions 26 and the paired rear stanchions 28, respectively, with a continuous U-shaped brace 36, each frame section 20 takes on the attribute of being integrally built as a complete unit while maintaining relative movement of the front and rear stanchions with respect to each other.
The scissor-like stud assembly 30 comprises a pair of pivoted bars 42 which criss-cross over themselves each being pivotally fixed at one end 44 to the upper ends of the respective stanchions 26, 28. The lower ends 46 of the bars 42 are slidably held in a slotted guide 48 integrally formed on the inner side of the opposite stanchion 26, 28. The slotted guide 48 is mounted at the lower ends of the stanchions 26, 28 and have a length about 10 to 12 inches. The crossing bars overlap each other and may be mutually provided with cut-outs 50 permitting the bars 42 to pivot over each other much like the action of a scissor. They may also be connected with a pivot pin 52 at their crossing point to increase rigidity of the wall. The lower ends of each bar 42 may be provided with laterally extending pins or flanges so as to be able to ride in the slotted guide without being detached therefrom, during movement.
Draped over the frame section and resting on the top of the roof arch 38 is « weatherproof (and, if desired, flameproof) fabric cover 54 which is preferably held in place by providing the cover 54 and the outer surface of the roof arch with mating VELCRO strips 56. Similarly, the leading and trailing edges of the cover 54 can also be provided with VELCRO strips 58 on its upper and lower surfaces so that the cover 54 of one section can be secured to that of its adjacent sections. If desired, cord lashing or other fastening means may be used. The lower edge 60 of the exterior covers 54 can fall below the arc of the roof arch, but it preferably does not extend fully down the side wall. The fabric weatherproof material used as the exterior cover 54 may be of any kind, although preferably the material sold under the trademark (BridgeTech Inc. , Brentwood, NY) which is used in the more common fixed loading bridges may be used here.
Mounted on the interior of each wall 24 is vertical panel 62 which may have at least its upper half 64 of transparent material. The interior panel 62 is attached to the wall, employing a mounting bar 66 fixed to the stanchions 26 and 28 to which VELCRO strips 68 may be secured. The leading and trailing edges of the panel 62 are also provided with VELCRO strips to secure the panel. On the other hand, if desired, small hooks 70 spaced along the length of the bar may be used with the leading and trailing edge of the panel 62 provided with corresponding spaced grommets 72 which fit over the hooks 70. The interior panel 62 may be made of the same weatherproof and fireproof material as the exterior cover 54 although this is not critical as the panel 62 is sheltered somewhat from the weather. Thus, if desired, the panels 62 may be of vinyl material, canvas or other long lasting fabric.
As seen from Fig. 2, because the edges of the roof cover purposely do not extend below the arch and the upper edges of the interior panels 64 do not extend above the arch, there is left a space through which wind may flow as indicated by the arrow A. This space relieves the effect of any wind gust on the passageway so that the passageway will neither move or tip when fully extended in rough weather.
It will thus be understood that each frame section 20 is itself collapsible and extendible. Depending upon the exact geometric length of the stanchions and the connecting scissor stud assembly, the frame section can be extended as much as 48" and collapsed to approximately 6 inches. Of course, by varying the geometry the length can be varied. In practice it has been found that a commuter aircraft are generally parked between 50-100 feet from the terminal. Therefore, a train of approximately 20 frame sections should be sufficiently long when deployed. If necessary more or fewer sections can be used.
As seen from Fig. 3 a train or series of sections are formed by providing the front stanchions and the rear stanchions with cooperating latch or connecting means whereby adjacent frame sections be articulately connected. For example, the front stanchions 26 may be provided with eye bolts 74 or other forms of staples while the rear stanchions are provided with pivotable latches. Other standard fastening means may be employed.
In addition, it may be desirable to provide a resilient biasing strap drawing the successive frame sections together, to this end a resilient elastic strap 78 may be stretched between the front frame section and the last frame section on each side. The exterior faces of the stanchions 26, 28 are provided with U-shaped handles 80 through which the strap 78 passes.
In general, the leading frame section will dock in abutment with the aircraft, straddling the staircase 82 which leads down from the aircraft and may be secured to the stairs. If this cannot be done then the staircases may be enclosed by an extendible belt 84 and portable stanchions 86. Preferably the leading frame section differs from the other frame sections in minor ways. First the roof 88 of the leading frame section is extended forwardly and upwardly following the line of the aircraft stairs 82 so that it terminates above the aircraft entrance 18. In addition, the edge of the roof 88 is padded as at 90 so as to softly abut against the aircraft. Solar powered battery operated lights 92 for general illumination. The leading frame section may also be provided with forwardly directed docking lights 94. The wheel assembly support bracket 32 may be slightly enlarged to allow the portable stanchion 86 to be placed thereon during deployment or storage of the passageway. A significant modification to the leading frame section may be described in that the scissor-like stud assembly 42 is arranged so as not to be collapsible. The criss-crossing studs may be locked together by suitable bolt means, in view of pivot pin 52. By preventing the leading frame section from collapsing, the train or entire passageway may be more easily pulled or pushed for deployment.
The leading frame section is, of course, hooked to the drive unit for deployment by suitable latch means. The drive unit 22 comprises a small wheeled truck 94 accommodating one operator and is provided with an electric propulsion motor 96 having a battery and charging system, control mechanisms such as forward/reverse 98, left/right 100 and hydraulic brake 102. The drive unit 22 and the front stanchion of the leading frame section are provided with cooperating hook and latch members 106 allowing the drive unit to be removably attached to the passageway whereby it may move and maneuver the passageway into deployment or storage position.
It is to be noted that a significant advantage of the present invention lies in the absence of a floor for the frame sections. The frame sections are thus light in weight and materially cheaper to construct. The frame sections each roll easily over the ground. Small accumulation of snow or debris on the ground will not interfere with movement. Larger accumulations will normally not exit, being uncovered promptly by airport personnel.
It is, thus, seen from the foregoing that a simple, easily constructed protective corridor for the swift movement of passengers is provided. The passageway is easily used and moved into position relative to the aircraft, no matter the parked position of the aircraft. Since the frame sections are identical they may be easily removed from or added to the passageway so that even the length of the fully extended passageway may be varied. The passageway as a whole is designed to be independent of any permanent facility and may be moved from terminal gate to terminal gate, when necessary.
To facilitate stowing as well as movement of the passageway, the wheel support brackets 32 may be vertically offset so as not to interfere with each other when the passageway is collapsed.
Various modifications and changes have been disclosed herein, and others will be apparent to those skilled in this art. Therefore, it is to be understood that the present disclosure is by way of illustration and not limiting of the present invention.

Claims

1. A passageway through which passengers may move for unloading and loading aircraft comprising a plurality of independent frame sections, each section having means enabling movement on the ground, said frames being articulately connected in a longitudinal end to end series to form an elongated flexible corridor, each frame section being collapsible in the longitudinal end to end series to form an elongated flexible corridor, each frame section being collapsible in the longitudinal direction selectively enable extended deployment of said passageway or stowing of said passageway in retracted collapsed condition.
2. The passageway according to claim 1, wherein each of said frame sections comprise a pair of spaced side walls, each of said side walls having a front and rear stanchion fixedly mounted on roller means and being connected by a longitudinally collapsible stud assembly, the corresponding front and rear stanchions of said pairs being fixedly joined to a roof beam.
3. The passageway according to claim 2, wherein said roof beams are U-shaped having its legs extending downwardly adjacent the respective stanchions with its ends fixedly secured to said roller means, and to said stanchions.
4. The passageway according to claim 2, including a fabric foldable cover extending over each frame section and secured to said roof beam.
5. The passageway according to claim 4, including a fabric foldable panel mounted within said frame on each of said paired walls.
6. The passageway according to claim 5, wherein the lower end of said roof cover and the upper end of said wall panels are spaced from each other to provide an opening for the flow of air through said frame.
7. The passageway according to claim 2, wherein said stud assembly comprises a pair of stud bars arranged to criss-cross each other, the upper end of each of said stud bars being pivotally fixed to a respective one of said front and rear stanchions, the lower ends of each steel bar being slidably attached to the other one of said stanchions.
8. The passageway according to claim 7, wherein each stanchion is provided with a slotted guide into which the lower end of the respective stud bar is slidingly held.
9. The passageway according to claim 1, wherein said frame sections are connected to each other by a removable latch mechanism.
10. The passageway according to claim 9, including a resilient expandable band extending from the leading frame section to the trailing frame section so as to normally bias said series of sections together.
11. The passageway according to claim 2, wherein the leading frame section includes means for preventing the collapse of said shed assembly and frame.
12. The passageway according to claim 2, wherein the leading frame section is provided with an enlarged canopy at its front end extending above and forward of the roof beam to provide a cover for the aircraft door.
13. The passageway according to claim 1, including motorized drive means, and means for connecting said drive means to the leading frame sections, whereby said frame sections may be pulled into extended condition or pushed into collapsed condition.
14. The passageway according to claim 2, including motorized drive means, and means for connecting said drive means to the leading frame sections, whereby said frame sections may be pulled into extended condition or pushed into collapsed condition.
15. The passageway according to claim 12, including motorized drive means, and means for connecting said drive means to the leading frame sections, whereby said frame sections may be pulled into extended condition or pushed into collapsed condition.
PCT/US1996/001312 1995-02-03 1996-01-30 Passageway for loading and unloading aircraft WO1996023715A1 (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
CA002187011A CA2187011C (en) 1995-02-03 1996-01-30 Passageway for loading and unloading aircraft
DK96903751T DK0752969T3 (en) 1995-02-03 1996-01-30 Corridor for loading and unloading aircraft
AU47734/96A AU4773496A (en) 1995-02-03 1996-01-30 Passageway for loading and unloading aircraft
DE69602497T DE69602497T2 (en) 1995-02-03 1996-01-30 PLANE FOR LOADING AND UNLOADING PLANES
EP96903751A EP0752969B1 (en) 1995-02-03 1996-01-30 Passageway for loading and unloading aircraft
FI963946A FI963946A (en) 1995-02-03 1996-10-02 Walkway for loading and unloading aircraft
MXPA/A/1996/004533A MXPA96004533A (en) 1995-02-03 1996-10-02 Telescopic hall to load and download
NO964181A NO303382B1 (en) 1995-02-03 1996-10-02 Passenger tunnel to be moved into or out of aircraft
GR990402111T GR3031033T3 (en) 1995-02-03 1999-08-19 Passageway for loading and unloading aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/383,060 US5603343A (en) 1995-02-03 1995-02-03 Passageway for loading and unloading aircraft
US08/383,060 1995-02-03

Publications (1)

Publication Number Publication Date
WO1996023715A1 true WO1996023715A1 (en) 1996-08-08

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Application Number Title Priority Date Filing Date
PCT/US1996/001312 WO1996023715A1 (en) 1995-02-03 1996-01-30 Passageway for loading and unloading aircraft

Country Status (13)

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US (1) US5603343A (en)
EP (1) EP0752969B1 (en)
AT (1) ATE180236T1 (en)
AU (1) AU4773496A (en)
CA (1) CA2187011C (en)
DE (1) DE69602497T2 (en)
DK (1) DK0752969T3 (en)
ES (1) ES2135209T3 (en)
FI (1) FI963946A (en)
GR (1) GR3031033T3 (en)
NO (1) NO303382B1 (en)
WO (1) WO1996023715A1 (en)
ZA (1) ZA96800B (en)

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FR3036100A1 (en) * 2015-05-13 2016-11-18 Acet-Cod EQUIPMENT FOR THE COMFORT AND SAFETY OF PASSENGERS AND FOR AIRPORT SAFETY DURING LANDING AND LANDING OPERATIONS IN A RESERVED AREA.
US9932130B2 (en) * 2015-07-02 2018-04-03 East Island Aviation Services, Inc. Passageway to board and deplane an airplane

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JPH11282684A (en) * 1998-03-27 1999-10-15 Canon Inc Image processor, method for controlling image processor and storage medium
WO2000060173A1 (en) * 1999-04-02 2000-10-12 Infra-Structure, Inc. Passageway for loading and unloading commuter aircraft
US6929217B2 (en) * 1999-06-24 2005-08-16 Gatelink Aircraft Boarding Systems, Inc. Interstitial regional aircraft boarding piers, and methods of using same
WO2001024601A2 (en) * 1999-10-06 2001-04-12 Infra-Structures, Inc. Improved cover system for aircraft loading passageway
WO2001025557A2 (en) * 1999-10-06 2001-04-12 Infra-Structures, Inc. Improved frame construction for aircraft loading passageway
US7069611B2 (en) * 2000-05-12 2006-07-04 Infra-Structures, Inc Regional boarding ramp for commuter aircraft
US6684443B2 (en) * 2001-02-07 2004-02-03 United Air Lines, Inc. Multiple-door access boarding bridge
US6691361B2 (en) 2001-03-30 2004-02-17 Dew Engineering And Development Limited Extensible platform on an extensible passenger loading bridge
DE10201723A1 (en) * 2002-01-18 2003-07-31 Thyssen Henschel Airport Syste Stationary telescopic gangway for processing of passengers and/or freight has fixed walkway connected at ground level to terminal and with sidewalls and roof lined with fire-insulated plates or prefabricated sandwich-type panels
FR2886624B1 (en) * 2005-06-02 2007-09-28 Air France Sa Soc SAFETY EQUIPMENT FOR PASSENGER TRANSFER TUNNEL AND TUNNEL HAVING SUCH EQUIPMENT
US7658199B2 (en) * 2005-06-03 2010-02-09 Ronald Lee Ayers Work cubicle cover
DE102005039472B4 (en) * 2005-08-20 2016-06-09 Hübner GmbH Passenger stairs or passenger boarding seal
US7520290B2 (en) 2005-10-18 2009-04-21 Dalbo Michele A Portable collapsible awning
US20100025156A1 (en) * 2008-07-09 2010-02-04 Lewis Mark A Emergency evacuation system for multi-story buildings
JP5513878B2 (en) * 2009-12-25 2014-06-04 新明和工業株式会社 Boarding bridge
US8266750B2 (en) 2010-03-24 2012-09-18 Gatelink Aircraft Boarding Systems, Inc. Microbridges for regional aircraft and methods of using same
CA2857552C (en) 2013-06-03 2018-04-03 James Larson Apparatus to interface a boarding bridge and a low doorsill airplane
FR3018504B1 (en) * 2014-03-13 2017-10-13 Sominex DEPLOYABLE DEVICE FOR COVERING THE PATHWAY OF PASSENGERS BETWEEN A TERMINAL BUILDING AND A MEANS OF TRANSPORT BY AIR EXAMPLE
DE102016001273A1 (en) * 2016-02-04 2017-08-10 HÜBNER GmbH & Co. KG Access device to an aircraft
DE102016001293A1 (en) * 2016-02-05 2017-08-10 HÜBNER GmbH & Co. KG Access tunnel system for the covered guidance of persons
JP7318923B2 (en) * 2019-09-30 2023-08-01 明治商工株式会社 Mobile protective fence for pedestrian protection

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US2700169A (en) * 1949-03-04 1955-01-25 Henry M Henion Aircraft loading and unloading arrangement
GB749847A (en) * 1953-07-29 1956-06-06 John Smith & Co London Ltd Improvements in or relating to shelters or the like
US2967534A (en) * 1957-11-07 1961-01-10 Joseph P Silye Tent shelter
US3046850A (en) * 1958-03-10 1962-07-31 Clair W Tellefson Foldable walkway and storage apparatus therefor
US3131705A (en) * 1962-02-12 1964-05-05 Marino Inc L Stabilized portable canopy
US3703737A (en) * 1971-05-24 1972-11-28 Boothe Airside Services Canopy apparatus
US3808626A (en) * 1970-09-08 1974-05-07 J Magill Self-contained mobile passenger bridge for aiplane loading and unloading operations
US4559660A (en) * 1983-11-14 1985-12-24 Yusaf Tarkan Aircraft loading ramp
US5331777A (en) * 1993-04-26 1994-07-26 Chi Yuan Huang Collapsible folding frame assembly for a collapsible folding vehicle barn

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US2828757A (en) * 1956-07-17 1958-04-01 Tepee Trail Inc Collapsible passageway
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US2470337A (en) * 1947-01-20 1949-05-17 Richard L Campbell Extensible canopy
US2700169A (en) * 1949-03-04 1955-01-25 Henry M Henion Aircraft loading and unloading arrangement
GB749847A (en) * 1953-07-29 1956-06-06 John Smith & Co London Ltd Improvements in or relating to shelters or the like
US2967534A (en) * 1957-11-07 1961-01-10 Joseph P Silye Tent shelter
US3046850A (en) * 1958-03-10 1962-07-31 Clair W Tellefson Foldable walkway and storage apparatus therefor
US3131705A (en) * 1962-02-12 1964-05-05 Marino Inc L Stabilized portable canopy
US3808626A (en) * 1970-09-08 1974-05-07 J Magill Self-contained mobile passenger bridge for aiplane loading and unloading operations
US3703737A (en) * 1971-05-24 1972-11-28 Boothe Airside Services Canopy apparatus
US4559660A (en) * 1983-11-14 1985-12-24 Yusaf Tarkan Aircraft loading ramp
US5331777A (en) * 1993-04-26 1994-07-26 Chi Yuan Huang Collapsible folding frame assembly for a collapsible folding vehicle barn

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3036100A1 (en) * 2015-05-13 2016-11-18 Acet-Cod EQUIPMENT FOR THE COMFORT AND SAFETY OF PASSENGERS AND FOR AIRPORT SAFETY DURING LANDING AND LANDING OPERATIONS IN A RESERVED AREA.
US9932130B2 (en) * 2015-07-02 2018-04-03 East Island Aviation Services, Inc. Passageway to board and deplane an airplane
US10377505B2 (en) 2015-07-02 2019-08-13 East Island Aviation Services, Inc. Passageway to board and deplane an airplane

Also Published As

Publication number Publication date
DE69602497D1 (en) 1999-06-24
NO964181D0 (en) 1996-10-02
FI963946A (en) 1996-12-03
DK0752969T3 (en) 1999-11-29
NO964181L (en) 1996-11-29
GR3031033T3 (en) 1999-12-31
EP0752969B1 (en) 1999-05-19
CA2187011A1 (en) 1996-08-08
MX9604533A (en) 1997-09-30
EP0752969A4 (en) 1997-02-26
ES2135209T3 (en) 1999-10-16
AU4773496A (en) 1996-08-21
EP0752969A1 (en) 1997-01-15
US5603343A (en) 1997-02-18
ZA96800B (en) 1996-08-07
ATE180236T1 (en) 1999-06-15
CA2187011C (en) 2001-05-08
DE69602497T2 (en) 2000-02-10
NO303382B1 (en) 1998-07-06
FI963946A0 (en) 1996-10-02

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