CA2640645A1 - An apparatus for loading and unloading aircrafts - Google Patents

An apparatus for loading and unloading aircrafts Download PDF

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Publication number
CA2640645A1
CA2640645A1 CA002640645A CA2640645A CA2640645A1 CA 2640645 A1 CA2640645 A1 CA 2640645A1 CA 002640645 A CA002640645 A CA 002640645A CA 2640645 A CA2640645 A CA 2640645A CA 2640645 A1 CA2640645 A1 CA 2640645A1
Authority
CA
Canada
Prior art keywords
conveyor
units
supported
unit
aircraft
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
CA002640645A
Other languages
French (fr)
Other versions
CA2640645C (en
Inventor
Lars Thogersen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RASN AS
Original Assignee
Rasn A/S
Lars Thogersen
Rampsnake A/S
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=8158909&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CA2640645(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rasn A/S, Lars Thogersen, Rampsnake A/S filed Critical Rasn A/S
Publication of CA2640645A1 publication Critical patent/CA2640645A1/en
Application granted granted Critical
Publication of CA2640645C publication Critical patent/CA2640645C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65G—TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
    • B65G67/00—Loading or unloading vehicles
    • B65G67/02—Loading or unloading land vehicles
    • B65G67/04—Loading land vehicles
    • B65G67/08—Loading land vehicles using endless conveyors
    • 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
    • B64F1/32—Ground or aircraft-carrier-deck installations for handling freight
    • B64F1/324—Luggage loaders specially adapted for loading individual luggage items into or out of the aircraft

Abstract

An apparatus for loading and unloading aircrafts comprises a tiltable first conveyor part (7) adjustable in height and provided with a conveyor path (11) advancing and removing luggage (59), such as suitcases, parcels and the like cargo items, to and from the apparatus. The apparatus comprises further a second conveyor part (8) extendable from the first conveyor part and being adapted to be moved through an opening in the aircraft and into the cargo compartment of said aircraft. This second conveyor part (8) comprises a conveyor path advancing or removing the luggage to or from the storing site inside the cargo compartment. The second conveyor part (8) comprises a plurality of pivotally interconnected conveyor units (30, 31) with their respective activatable conveyor paths and their respective sets of wheels (44).

Claims (14)

1. A ground apparatus for loading and unloading an aircraft with a cargo compartment, said apparatus comprising:

a chassis supported by wheels, a tiltable ramp connected to said chassis, a conveyor having a first end and a second end and being at least partially extendable from said apparatus into said cargo compartment, said conveyor including a succession of conveyor units, wherein each conveyor unit has a set of wheels and wherein the conveyor units are mutually interconnected by means of coupling members that allow for a pivotal movement between each of said conveyor units, said apparatus including a compartment located below said ramp, said apparatus being constructed for storing said conveyor in a folded configuration wherein a portion of the conveyor is supported by said ramp while another portion of said conveyor is received within said compartment.
2. The apparatus according to claim 1, characterised in that it comprises an endless conveyor belt supported by said ramp and running above said conveyor.
3. The apparatus according to claim 1 or 2, wherein said coupling members allow for a sideways mutual pivotal movement of said conveyor units and for a mutual pivotal movement of said conveyor units about an essentially horizontal axis.
4. The apparatus according to any one of claims 1 to 3, wherein said apparatus includes a bridge member adapted to be supported by said aircraft to support a part of said conveyor when said conveyor is extended from said apparatus, said bridge member comprising guiding means for guiding said conveyor units.
5. The apparatus according to any one of claims 1 to 4 wherein the first end conveyor unit at said first end includes means for varying the inclination of said conveyor path of said first end conveyor unit.
6. The apparatus according to claim 5 wherein said first end conveyor unit comprises a support member with said set of wheels, said support member having a conveyor pivotally connected thereto, said conveyor defining said conveyor path of said first end conveyor unit, said means for varying the inclination of said conveyor path of said first end conveyor unit acting to pivot said conveyor in relation to said support member.
7. The apparatus according to claim 5 or 6, characterized in that it comprises a conveyor front member which is hingedly mounted to said first end conveyor unit and which can be set with a desired inclination relative to the conveyor path of the first end conveyor unit.
8. The apparatus according to any one of claims 1 to 7, characterised in that each conveyor unit comprises an endless conveyor belt.
9. The apparatus according to claim 8, wherein each endless conveyor belt is driven by a driving roller and one or more further rollers, which are supported by a frame, which in turn is supported by a wheel-carrying support member.
10. The apparatus according to claim 8 or 9 wherein said conveyor belt has a width that is greater than a distance between said rollers.
11. The apparatus according to any one of claims 1 to 10, characterised in that it comprises control means whereby an operator present inside the aircraft can control said conveyor.
12. The apparatus according to any one of claims 1 to 11, characterised in that the conveyor units are interconnected by means of releasable coupling members.
13. The apparatus according to any one of claims 1 to 12, characterised in that it comprises driving means cooperating with said conveyor units for extending said conveyor from said apparatus.
14. The apparatus according to any one of claims 1 to 13, placed on a vehicle.
CA2640645A 2000-01-11 2001-01-10 An apparatus for loading and unloading aircrafts Expired - Fee Related CA2640645C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DK200000031A DK173750B1 (en) 2000-01-11 2000-01-11 Aircraft loading and unloading apparatus
DKPA200000031 2000-01-11
CA002396198A CA2396198C (en) 2000-01-11 2001-01-10 An apparatus for loading and unloading aircrafts

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CA002396198A Division CA2396198C (en) 2000-01-11 2001-01-10 An apparatus for loading and unloading aircrafts

Publications (2)

Publication Number Publication Date
CA2640645A1 true CA2640645A1 (en) 2001-07-19
CA2640645C CA2640645C (en) 2010-12-21

Family

ID=8158909

Family Applications (2)

Application Number Title Priority Date Filing Date
CA2640645A Expired - Fee Related CA2640645C (en) 2000-01-11 2001-01-10 An apparatus for loading and unloading aircrafts
CA002396198A Expired - Lifetime CA2396198C (en) 2000-01-11 2001-01-10 An apparatus for loading and unloading aircrafts

Family Applications After (1)

Application Number Title Priority Date Filing Date
CA002396198A Expired - Lifetime CA2396198C (en) 2000-01-11 2001-01-10 An apparatus for loading and unloading aircrafts

Country Status (17)

Country Link
US (4) US7033125B2 (en)
EP (3) EP1248726B1 (en)
JP (1) JP4937476B2 (en)
CN (1) CN1162303C (en)
AT (3) ATE320375T1 (en)
AU (1) AU774012B2 (en)
BR (1) BR0107552B1 (en)
CA (2) CA2640645C (en)
DE (3) DE60118043T2 (en)
DK (4) DK173750B1 (en)
EA (1) EA003548B1 (en)
ES (3) ES2222330T3 (en)
MX (1) MXPA02006757A (en)
NZ (1) NZ520399A (en)
PL (1) PL205783B1 (en)
WO (1) WO2001051356A1 (en)
ZA (1) ZA200205298B (en)

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Also Published As

Publication number Publication date
BR0107552B1 (en) 2010-09-08
DK200000031A (en) 2001-07-12
DE60104280D1 (en) 2004-08-19
DK1666357T3 (en) 2008-07-14
EP1666357A1 (en) 2006-06-07
EP1273517A3 (en) 2003-12-10
DK200800051U1 (en) 2008-04-11
NZ520399A (en) 2003-04-29
DK200800051U3 (en) 2008-05-23
EP1248726A1 (en) 2002-10-16
DE60133327T2 (en) 2009-03-05
AU774012B2 (en) 2004-06-10
EA003548B1 (en) 2003-06-26
DK200500245U4 (en) 2006-03-10
DK200500245U1 (en) 2005-11-25
AU2353401A (en) 2001-07-24
ATE320375T1 (en) 2006-04-15
US6893200B2 (en) 2005-05-17
JP4937476B2 (en) 2012-05-23
BR0107552A (en) 2002-10-08
PL205783B1 (en) 2010-05-31
ATE271002T1 (en) 2004-07-15
US20030049107A1 (en) 2003-03-13
CA2396198A1 (en) 2001-07-19
US7033125B2 (en) 2006-04-25
ES2222330T3 (en) 2005-02-01
DE60133327D1 (en) 2008-04-30
EA200200744A1 (en) 2002-12-26
DE60118043T2 (en) 2006-10-12
PL355969A1 (en) 2004-05-31
CN1162303C (en) 2004-08-18
ES2308644T3 (en) 2008-12-01
CN1396877A (en) 2003-02-12
ATE389583T1 (en) 2008-04-15
DK173750B1 (en) 2001-09-10
US20030161707A1 (en) 2003-08-28
CA2396198C (en) 2008-12-23
WO2001051356A1 (en) 2001-07-19
DE60118043D1 (en) 2006-05-11
MXPA02006757A (en) 2004-09-10
DE60104280T2 (en) 2005-07-28
JP2003519594A (en) 2003-06-24
ES2259064T3 (en) 2006-09-16
US7156604B2 (en) 2007-01-02
EP1666357B1 (en) 2008-03-19
EP1248726B1 (en) 2004-07-14
CA2640645C (en) 2010-12-21
ZA200205298B (en) 2003-10-02
EP1273517A2 (en) 2003-01-08
US20030091415A1 (en) 2003-05-15
EP1273517B1 (en) 2006-03-15
US20040105740A1 (en) 2004-06-03

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Effective date: 20190110