WO2002016203A1 - Aircraft support vehicle - Google Patents
Aircraft support vehicle Download PDFInfo
- Publication number
- WO2002016203A1 WO2002016203A1 PCT/GB2001/003794 GB0103794W WO0216203A1 WO 2002016203 A1 WO2002016203 A1 WO 2002016203A1 GB 0103794 W GB0103794 W GB 0103794W WO 0216203 A1 WO0216203 A1 WO 0216203A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- self
- vehicle according
- aircraft
- propelled
- services
- Prior art date
Links
- 238000001816 cooling Methods 0.000 claims description 8
- 239000000446 fuel Substances 0.000 claims description 4
- 238000011084 recovery Methods 0.000 claims description 3
- 238000002485 combustion reaction Methods 0.000 claims description 2
- 239000002283 diesel fuel Substances 0.000 claims description 2
- 230000009977 dual effect Effects 0.000 claims description 2
- 238000010276 construction Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- 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
- B64F1/36—Other airport installations
Definitions
- This invention relates to aircraft support vehicles for providing support services for aircraft and in particular, but not exclusively, to self-propelled multipurpose support vehicles capable of operating in a wide range of terrains .
- the present invention is therefore concerned with reducing the logistics burden or logistics "footprint" by combining functions previously provided in separate towed items of aerospace ground equipment .
- this invention provides a self-propelled ground support vehicle for an aircraft, said vehicle comprising: - a wheeled main body portion; a cab portion containing driver controls for the vehicle; a main power unit; a ground wheel drive train connected to the power unit for transmitting drive from the power unit to at least two of the vehicle wheels; an aircraft services gearbox connected to the power unit and supplying drive to at least two aircraft service devices.
- the aircraft service devices include one or more of the following service devices :- a hydraulic pump; an electrical generator; a low pressure air compressor; a high pressure air compressor, and a cooling device.
- the construction of the support vehicle may be modular to enable it readily to be configured during manufacture for one of several different uses.
- the vehicle includes respective independent clutch means between the power unit and the ground wheel drive train, and between the power unit and said aircraft services gearbox respectively.
- the control means for selecting and controlling the services driven by the aircraft services gearbox is preferably provided within the cab portion although auxiliary controls may be provided elsewhere in the vehicle at an externally accessible location.
- the power unit preferably comprises a dual fuel internal combustion engine capable of running on aviation fuel (AVTUR) or diesel fuel.
- AVTUR aviation fuel
- the ground wheel drive train transmits drive to four or more vehicle wheels.
- said main body portion includes externally accessible inlet/outlet connections for at least some of the services driven by said aircraft services gearbox.
- the main body portion may include externally accessible duplicate inlet/outlet connections to opposite sides of the main body portion for at least some of said services.
- said main body portion includes a load space for carrying support equipment.
- the support equipment may comprise one or more of : - a towing arm; gas storage vessels; test equipment; crash recovery equipment; a fork lift device; a hoist, and tools .
- said main body portion includes shutter means for closing said load space.
- the load space is covered by a covered roof which is strengthened to serve as a work platform.
- One or more movable floodlights may be provided on the roof or elsewhere on the vehicle.
- the vehicle also preferably includes a towing point on the front and/or rear of the vehicle .
- the vehicle preferably includes a winch means on the front and/or rear of the vehicle.
- Figure 1 is a front perspective view of a multi- purpose ground support vehicle in accordance with this invention.
- Figure 2 is a section view looking down through the floor area of the multi-purpose support vehicle of Figure
- Figure 3 is a side view of the multi-purpose support vehicle of Figure 1
- Figure 4 is a perspective view from the rear showing the equipment load space of the multi-purpose support vehicle of Figure 1.
- Figures combines several aerospace ground equipment functions into a single, self-propelled vehicle with rough terrain capability and the ability to be tailored in terms of the on-board features through a modular build concept.
- the vehicle illustrated is intended to be built on the basis of an existing four wheel drive all-terrain vehicle.
- the vehicle 10 comprises a cab portion 12, a load space 14 and, in this embodiment, four wheels.
- the load space 14 has a strengthened roof 16 which may be used as a work platform.
- Movable floodlights 18 are disposed at the upper four corners of the vehicle. At the front of the vehicle there is provided a winch 20 and a towing hitch 22. To the left and right hand sides of the vehicle is a connector bay 24.
- the strengthened roof 16 may be provided with retractable safety rails (not shown) , with the roof being accessible via an access ladder.
- the vehicle engine 26 is connected to the four road wheels 28 by a generally conventional four wheel drive power train indicated schematically by lines 29, via a clutch 31.
- the engine 26 is capable of running on either diesel or AVTUR.
- a power offtake shaft 30 from the engine supplies power to an aircraft services gearbox or aircraft accessory drive 32. This may be based on an existing aircraft gearbox and modified to suit requirements .
- the aircraft services gearbox has a single input drive. However if a specialised input drive is required (e.g. airflow or pressure) it may be necessary to drive the aircraft services gearbox from a separate power source e.g. a small gas turbine.
- the aircraft services gearbox 32 in this embodiment supplies power to a system cooling device 34, a low pressure air compressor 36, a high pressure air compressor 38, an electrical generator 40, and a hydraulic pump 42.
- the system cooling device 34 provides additional cooling for the aircraft avionic systems if the onboard aircraft cooling system is not capable of maintaining the avionics system within the required temperature range - for example if the external air temperature is very high.
- the system cooling device may therefore comprise the components found on a conventional towed ground cooling trolley.
- the number of output drives and aircraft services so provided will vary in number and configuration depending on the aircraft type for which the multi-purpose support vehicle is being configured. In many instances, the aircraft services gearbox will be the same item, or modified from the same item, as is fitted to the aircraft for which the multipurpose support vehicle is being configured.
- the services (34 to 42) are supplied to respective connectors (only two of which are shown) in the connector bays 24 to either side of the vehicle (only one of which is shown in Figure 2) .
- the connector bays are each accessible via a closeable door 44.
- a clutch 46 allows the power to the aircraft services gearbox to be disengaged.
- the load space 14 may house test equipment, crash recovery equipment, tools or other items such as a forklift and a hoist, as required.
- the load space may be closed by means of a roller shutter or the like (not shown) .
- the load space may also include lockers 48 and 50 for storing a towing arm (in dismantled form) and one or more gas bottles 54.
- At the rear of the vehicle is provided a further towing hitch 56 and a further winch 58.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Body Structure For Vehicles (AREA)
- Hybrid Electric Vehicles (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE60126622T DE60126622T2 (en) | 2000-08-25 | 2001-08-24 | AIR SUPPLY VEHICLE |
EP01963134A EP1311427B1 (en) | 2000-08-25 | 2001-08-24 | Aircraft support vehicle |
AU2001284168A AU2001284168A1 (en) | 2000-08-25 | 2001-08-24 | Aircraft support vehicle |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0020970.0 | 2000-08-25 | ||
GBGB0020970.0A GB0020970D0 (en) | 2000-08-25 | 2000-08-25 | Aircraft support vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002016203A1 true WO2002016203A1 (en) | 2002-02-28 |
Family
ID=9898295
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB2001/003794 WO2002016203A1 (en) | 2000-08-25 | 2001-08-24 | Aircraft support vehicle |
Country Status (7)
Country | Link |
---|---|
US (1) | US20030164256A1 (en) |
EP (1) | EP1311427B1 (en) |
AU (1) | AU2001284168A1 (en) |
DE (1) | DE60126622T2 (en) |
ES (1) | ES2281436T3 (en) |
GB (1) | GB0020970D0 (en) |
WO (1) | WO2002016203A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011066891A1 (en) * | 2009-12-02 | 2011-06-09 | Diehl Aerospace Gmbh | Multi-function aircraft tractor |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DK200400445A (en) * | 2004-03-19 | 2005-09-20 | Falck Schmidt S Maskinfabrik A | Self-propelled vehicle, for support or service of aircraft |
US7311298B2 (en) * | 2005-06-09 | 2007-12-25 | Warn Industries, Inc. | Integrated air compressor and winch |
US7559534B2 (en) | 2005-06-09 | 2009-07-14 | Warn Industries, Inc. | Integrated air compressor and winch |
US7635921B2 (en) * | 2007-04-06 | 2009-12-22 | Northrop Grumman Space & Mission Systems Corporation | Self-powered mobile electrical power hub |
CN101898499A (en) * | 2010-08-26 | 2010-12-01 | 威海广泰空港设备股份有限公司 | Double power air-conditioned car for aircraft |
NL2011931C2 (en) | 2013-12-10 | 2015-06-11 | Duinmaaijer B V | Ground support system for an aircraft having a turbine engine. |
FR3069853B1 (en) | 2017-08-03 | 2020-02-14 | Athena Pi | DEVICE FOR PROVIDING UTILITIES TO AN AIRCRAFT ON THE GROUND |
JP7233000B2 (en) * | 2019-02-19 | 2023-03-06 | シンフォニアテクノロジー株式会社 | aircraft ground support vehicle |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2448172A (en) * | 1946-05-11 | 1948-08-31 | Kibbey W Couse | Aircraft service power truck |
US2968923A (en) * | 1955-05-06 | 1961-01-24 | North American Aviation Inc | Mobile starter for jet aircraft engines |
US3866701A (en) * | 1973-05-21 | 1975-02-18 | Peter O E Bekker | Ground support unit |
US3886701A (en) | 1972-03-10 | 1975-06-03 | Bogaert P E E J | Top for a skylight side member |
US4171114A (en) * | 1976-09-02 | 1979-10-16 | Marden Jay W | Mobile aerial support system |
DE3423867A1 (en) * | 1984-06-28 | 1986-01-02 | Heinz 8132 Tutzing Schabmüller | Self-propelled on-board network supply system for aircraft |
EP0350615A2 (en) * | 1988-07-13 | 1990-01-17 | SIMAI S.p.A. | Self-propelled, electricity generating, hybrid tractor for airport services, for checking the on-board aircraft equipment and for starting-up the aircraft engines |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2016934A (en) * | 1934-01-25 | 1935-10-08 | Galion Metallic Vault Co | Power take-off mechanism |
US2337615A (en) * | 1940-05-18 | 1943-12-28 | Mclaren Chester | Mobile field packing plant |
DE1605985A1 (en) * | 1967-10-25 | 1971-02-04 | Walter Gutbrod | Self-propelled multi-gym |
US3667436A (en) * | 1970-01-14 | 1972-06-06 | Robert Reichhelm | Fuel gasification for internal combustion engines |
EP0081024B1 (en) * | 1981-11-12 | 1986-02-19 | Deere & Company | Mechanism for the selective driving of machines and devices by the power take-off shaft of an agricultural tractor |
US4683976A (en) * | 1984-05-18 | 1987-08-04 | Konrad Rosenbauer Kg | Service vehicle |
US4881864A (en) * | 1987-11-09 | 1989-11-21 | Hitch Lift, Inc. | Boom hoist for attachment to a trailer hitch drawbar |
CA2056236C (en) * | 1991-11-26 | 2001-08-21 | Gary D. Webster | Internal combustion engine with high temperature variable geometry pre-combustion chamber |
CA2146394A1 (en) * | 1995-04-05 | 1996-10-06 | Kazutoshi Furukawa | Power supply apparatus installed under a carrier of a vehicle |
-
2000
- 2000-08-25 GB GBGB0020970.0A patent/GB0020970D0/en not_active Ceased
-
2001
- 2001-08-24 DE DE60126622T patent/DE60126622T2/en not_active Expired - Fee Related
- 2001-08-24 EP EP01963134A patent/EP1311427B1/en not_active Expired - Lifetime
- 2001-08-24 ES ES01963134T patent/ES2281436T3/en not_active Expired - Lifetime
- 2001-08-24 WO PCT/GB2001/003794 patent/WO2002016203A1/en active IP Right Grant
- 2001-08-24 AU AU2001284168A patent/AU2001284168A1/en not_active Abandoned
- 2001-08-24 US US10/362,418 patent/US20030164256A1/en not_active Abandoned
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2448172A (en) * | 1946-05-11 | 1948-08-31 | Kibbey W Couse | Aircraft service power truck |
US2968923A (en) * | 1955-05-06 | 1961-01-24 | North American Aviation Inc | Mobile starter for jet aircraft engines |
US3886701A (en) | 1972-03-10 | 1975-06-03 | Bogaert P E E J | Top for a skylight side member |
US3866701A (en) * | 1973-05-21 | 1975-02-18 | Peter O E Bekker | Ground support unit |
US4171114A (en) * | 1976-09-02 | 1979-10-16 | Marden Jay W | Mobile aerial support system |
DE3423867A1 (en) * | 1984-06-28 | 1986-01-02 | Heinz 8132 Tutzing Schabmüller | Self-propelled on-board network supply system for aircraft |
EP0350615A2 (en) * | 1988-07-13 | 1990-01-17 | SIMAI S.p.A. | Self-propelled, electricity generating, hybrid tractor for airport services, for checking the on-board aircraft equipment and for starting-up the aircraft engines |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011066891A1 (en) * | 2009-12-02 | 2011-06-09 | Diehl Aerospace Gmbh | Multi-function aircraft tractor |
Also Published As
Publication number | Publication date |
---|---|
ES2281436T3 (en) | 2007-10-01 |
AU2001284168A1 (en) | 2002-03-04 |
US20030164256A1 (en) | 2003-09-04 |
DE60126622T2 (en) | 2007-10-31 |
GB0020970D0 (en) | 2000-10-11 |
EP1311427B1 (en) | 2007-02-14 |
EP1311427A1 (en) | 2003-05-21 |
DE60126622D1 (en) | 2007-03-29 |
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