WO2002062663A1 - Rpv transport vehicle - Google Patents
Rpv transport vehicle Download PDFInfo
- Publication number
- WO2002062663A1 WO2002062663A1 PCT/GB2001/005717 GB0105717W WO02062663A1 WO 2002062663 A1 WO2002062663 A1 WO 2002062663A1 GB 0105717 W GB0105717 W GB 0105717W WO 02062663 A1 WO02062663 A1 WO 02062663A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- uav
- transporter
- tractor
- deck
- trailer
- 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.)
- Ceased
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/10—Transport or storage specially adapted for UAVs with means for moving the UAV to a supply or launch location, e.g. robotic arms or carousels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/20—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV
- B64U80/25—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV for recharging batteries; for refuelling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/86—Land vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/50—Foldable or collapsible UAVs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/60—Take-off or landing of UAVs from a runway using their own power
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
Definitions
- This invention relates to a vehicle for use with aircraft, and particularly for use with unmanned aerial vehicles.
- vehicle may have command service and transport functions.
- Unmanned aerial vehicles have a relatively low cost compared with manned aircraft, and are typically used for data acquisition, for example aerial photography.
- UAVs Unmanned aerial vehicles
- airport facilities may not be available, especially in remote areas.
- the limited payload/range of a typical UAV also make it desirable to minimise transit time between the take-off and landing location, and the region of interest.
- the present invention provides a relatively inexpensive solution to this problem whilst also solving the associated requirements for transport of the UAV and servicing/replenishment of consumables.
- a transporter for a UAV comprising a trailer of an articulated tractor/trailer combination wherein the trailer comprises an upper deck adapted to carry a UAV and a lower deck adapted to carry consumables for a UAV, separate loading and unloading ramps being provided at the front and back of the upper deck in order to permit unidirectional movement of a UAV over the upper deck.
- This arrangement has the advantage that different operations on the UAV take place at different locations on the upper deck. For example fuelling of the
- UAV may be confined to one dedicated location on the upper deck which is provided with means for accommodating fuel spillages and for fighting fires.
- the most dangerous operations are preferably carried out close to the departure end of the upper deck, so as to avoid unnecessary risk at other upper deck locations.
- the trailer is preferably a double deck car transporter having upper deck loading/unloading ramp for the UAV, and one or more storage units on the lower deck. It is envisaged that a trailer according to the invention could be easily adapted from an open car transporter by the addition of runways for the UAV, and demountable containers for consumables such as fuel, spares and the like. A demountable container may also be provided for command and control of the UAV.
- a trailer according to the invention is adapted to carry a plurality of UAVs in series on the upper deck, and can be pulled by a conventional tractor to a launch and/or landing site, which may be a road.
- the trailer may further include a demountable container for road barriers, signs, cones and the like.
- a tractor for use with the trailer comprises a command and control centre.
- the tractor preferably has a rearwards cab extension, and is for example a sleeper cab.
- the cab extension contains command and control apparatus for a UAV which may be demountable.
- the tractor may have a rear facing window, and the tractor seats may be adapted to swivel so as to face the command and control equipment whilst permitting viewing through the rear cab window. This arrangement permits the tractor to be positioned away from the trailer, immediately adjacent a temporary take off/landing area.
- a trailer according to the invention can provide low cost, self-contained mobile support for a UAV close to the desired operating region, and that a tractor for use with the trailer can provide a mobile command and control unit.
- the UAV is adapted for support by two personnel, being the tractor driver and driver's mate.
- Fig.1 is a side elevation of a trailer according to the invention and carrying three UAVs;
- Fig.2 is a side elevation of an extended cab tractor; and
- Fig.3 is a schematic plan view of the tractor of Fig.2, illustrating the internal configuration.
- Fig.1 shows a conventional double deck car transporter 10 from which, for reasons of clarity, the upper deck supports and hydraulic rams have been omitted.
- the upper deck 11 supports three UAVs 12, shown schematically and having wings folded for transport. It will be observed that the overall vehicle height is substantially of the order for a conventional car transporter and thus the transporter 10 is adapted for travel on most roads.
- the lower deck 13 includes three demountable containers comprising a fuel tank and armaments bay 14, a service bay 15 and a spares container 16. More or less demountable units having other functions may be provided to suit particular circumstances.
- the upper deck is provided with a front ramp and a rear ramp, also contained in demountable units 17, 18 for respective extension to the front and to the rear. These ramps may be extended mechanically or with power assistance to the ground so as to give departure angles which can be accommodated by the design of the UAVs.
- the units 17,18 may also include winches of any suitable kind for assisting smooth loading and unloading, means also being provided for the UAVs to progress along the upper deck 11 as will be described below.
- another container 19 which may be integral with the tank or separate, contains fuel pumps, fire protection equipment and the like. It will be readily appreciated that the range and kind of demountable units is large.
- the demountable containers 14-16 are wheeled, and are loaded via the usual drop down rear ramp of the lower deck, and latched. These containers may be winched on, or pushed on by for example, a small vehicle. Such a small vehicle may also be carried on the lower deck at the back, and may be adapted to tow UAVs.
- the tractor 20 illustrated in Figs. 2 and 3 has two axles and the usual fifth wheel 21 for coupling to the trailer.
- An extended cab 22 contains a command and control station 23, the tractor seats 24 being pivotable through 180° to permit the driver and driver's mate to operate the station 23.
- a cab rear window (not illustrated) permits viewing of the UAV.
- tractor/trailer combination is largely conventional, it can operate over normal roads, be fuelled and serviced in an accepted manner, and be driven by any person having the required class of licence.
- the transporter will be driven to the predefined location having a surface suitable for take-off and/or landing of a UAV.
- the tractor 20 will be unhitched, and the unloading ramp 17 extended. If the runway area is a road, suitable road blocking measures will be taken, perhaps using equipment carried on the transporter 10.
- the tractor will be parked at about the mid-point of the runway area so as to permit supervision of the UAV.
- the UAV will be guided off the transporter 10 to the take-off area, and launched in a conventional manner. At the conclusion of the flight the UAV lands in the same or another area, and is guided onto the rear ramp 18 for loading on the top deck of the transporter 10.
- the UAV is subjected to any necessary servicing and maintenance, with any necessary spare parts or other consumables provided from container 16.
- the UAV is then rolled along the top deck on its undercarriage, either by hand or by a suitable winch (not shown) or the like, towards the front of the transporter (the left hand side of Figure 1 ) and it is refuelled and then re-armed when it is ready to be demounted from the top deck via front ramp 17 for redeployment.
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Robotics (AREA)
- Mechanical Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB0103202.8A GB0103202D0 (en) | 2001-02-08 | 2001-02-08 | Vehicle |
| GB0103202.8 | 2001-02-08 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2002062663A1 true WO2002062663A1 (en) | 2002-08-15 |
Family
ID=9908408
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/GB2001/005717 Ceased WO2002062663A1 (en) | 2001-02-08 | 2001-12-21 | Rpv transport vehicle |
Country Status (2)
| Country | Link |
|---|---|
| GB (1) | GB0103202D0 (en) |
| WO (1) | WO2002062663A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1884463A1 (en) * | 2006-07-25 | 2008-02-06 | Honeywell Inc. | Micro air-vehicle transport container and launch system |
| CN106560398A (en) * | 2015-10-02 | 2017-04-12 | 波音公司 | Aerial Agricultural Management System |
| US9841757B2 (en) | 2015-12-03 | 2017-12-12 | At&T Intellectual Property I, L.P. | Drone piggybacking on vehicles |
| CN109436364A (en) * | 2018-10-22 | 2019-03-08 | 南京航空航天大学 | A kind of device and method continuously emitted for unmanned plane |
| US20220396421A1 (en) * | 2021-06-07 | 2022-12-15 | Shanghai Autoflight Co., Ltd. | UAV Transport Box |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4730793A (en) * | 1981-08-12 | 1988-03-15 | E-Systems, Inc. | Ordnance delivery system and method including remotely piloted or programmable aircraft with yaw-to-turn guidance system |
| US5695153A (en) * | 1995-11-16 | 1997-12-09 | Northrop Grumman Corporation | Launcher system for an unmanned aerial vehicle |
-
2001
- 2001-02-08 GB GBGB0103202.8A patent/GB0103202D0/en not_active Ceased
- 2001-12-21 WO PCT/GB2001/005717 patent/WO2002062663A1/en not_active Ceased
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4730793A (en) * | 1981-08-12 | 1988-03-15 | E-Systems, Inc. | Ordnance delivery system and method including remotely piloted or programmable aircraft with yaw-to-turn guidance system |
| US5695153A (en) * | 1995-11-16 | 1997-12-09 | Northrop Grumman Corporation | Launcher system for an unmanned aerial vehicle |
Non-Patent Citations (2)
| Title |
|---|
| BENJAMIN N ELSON: "Mini-RPV being Developed for Army", AVIATION WEEK AND SPACE TECHNOLOGY,MCGRAW-HILL INC. NEW YORK,US, vol. 112, no. 4, 7 January 1980 (1980-01-07), pages 54 - 63, XP002160708, ISSN: 0005-2175 * |
| HEWISH M: "BUILDING A BIRD'S-EYE VIEW OF THE BATTLEFIELD. UNMANNED AERIAL VEHICLES ADDRESS NEW REQUIREMENTS", JANE'S INTERNATIONAL DEFENSE REVIEW,GB,JANE'S INFORMATION GROUP, vol. 30, 1 February 1997 (1997-02-01), pages 55 - 56,58-59, XP000679198, ISSN: 0020-6512 * |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1884463A1 (en) * | 2006-07-25 | 2008-02-06 | Honeywell Inc. | Micro air-vehicle transport container and launch system |
| US7658347B2 (en) | 2006-07-25 | 2010-02-09 | Honeywell International, Inc. | Micro air-vehicle transport container and launch system |
| CN106560398A (en) * | 2015-10-02 | 2017-04-12 | 波音公司 | Aerial Agricultural Management System |
| EP3156328A1 (en) * | 2015-10-02 | 2017-04-19 | The Boeing Company | Aerial agricultural management system |
| US9776717B2 (en) | 2015-10-02 | 2017-10-03 | The Boeing Company | Aerial agricultural management system |
| CN106560398B (en) * | 2015-10-02 | 2022-01-14 | 波音公司 | Aviation agricultural management system |
| US9841757B2 (en) | 2015-12-03 | 2017-12-12 | At&T Intellectual Property I, L.P. | Drone piggybacking on vehicles |
| US10134290B2 (en) | 2015-12-03 | 2018-11-20 | At&T Intellectual Property I, L.P. | Drone piggybacking on vehicles |
| CN109436364A (en) * | 2018-10-22 | 2019-03-08 | 南京航空航天大学 | A kind of device and method continuously emitted for unmanned plane |
| CN109436364B (en) * | 2018-10-22 | 2021-10-15 | 南京航空航天大学 | A device and method for continuous launch of unmanned aerial vehicles |
| US20220396421A1 (en) * | 2021-06-07 | 2022-12-15 | Shanghai Autoflight Co., Ltd. | UAV Transport Box |
| US11814241B2 (en) * | 2021-06-07 | 2023-11-14 | Shanghai Autoflight Co., Ltd. | UAV transport box |
Also Published As
| Publication number | Publication date |
|---|---|
| GB0103202D0 (en) | 2001-03-28 |
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