Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
  • B64U70/00—Launching, take-off or landing arrangements
  • B64U70/90—Launching from or landing on platforms
  • B64U70/99—Means for retaining the UAV on the platform, e.g. dogs or magnets
• • 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
  • B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
  • B64F1/222—Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
  • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
  • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
  • B60L53/14—Conductive energy transfer
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
  • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
  • B60L53/80—Exchanging energy storage elements, e.g. removable batteries
• • 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
  • B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
• • 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
  • B64F1/362—Installations for supplying conditioned air to parked aircraft
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
  • B64U70/00—Launching, take-off or landing arrangements
  • B64U70/90—Launching from or landing on platforms
  • B64U70/92—Portable platforms
  • B64U70/93—Portable platforms for use on a land or nautical vehicle
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
  • B64U70/00—Launching, take-off or landing arrangements
  • B64U70/90—Launching from or landing on platforms
  • B64U70/97—Means for guiding the UAV to a specific location on the platform, e.g. platform structures preventing landing off-centre
• • 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
  • B60—VEHICLES IN GENERAL
  • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
  • B60L2200/00—Type of vehicles
  • B60L2200/10—Air crafts
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
  • B64U2201/00—UAVs characterised by their flight controls
  • B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
• • 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
  • Y02T10/00—Road transport of goods or passengers
  • Y02T10/60—Other road transportation technologies with climate change mitigation effect
  • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
• • 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
  • Y02T10/00—Road transport of goods or passengers
  • Y02T10/60—Other road transportation technologies with climate change mitigation effect
  • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
• • 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
  • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
  • Y02T90/10—Technologies relating to charging of electric vehicles
  • Y02T90/14—Plug-in electric vehicles

Definitions

• the present invention relates to a station, preferably a mobile station, and the elements of such a station capable of accommodating several types of drones and performing several functions/actions on the drone and parts of the drone.
• the system is notably capable of placing the drones in a defined position, of locking the drone in the station, of extracting the battery or batteries from the drone, of inserting a full battery or batteries in the drone and of charging the batteries extracted from independently.
• the system makes it possible to load and/or unload various loads such as parcels, seeds, treatment liquids or any other load from the drone.
• the station is preferably equipped with an intelligent battery charging system optimizing battery life and a programmable robot capable of handling any type of payload.
• the invention also relates to a universal battery shell/cage system, easy to insert/uninsert, connect/disconnect, thus making the handling of the batteries possible by a robot and consequently an automated management and handling of said batteries.
• the station can be used as an intermediate station in a network of several drones or in a system comprising one station per drone.
• the station can be fixed or mobile, for example mounted on a vehicle.
• the station can adapt to different drones, for example of different construction and/or of different size.
• An object of the present invention is to improve the systems known from the state of the art.
• Another object of the present invention is to propose a system and means allowing automated management of drones of several types, shapes and sizes.
• Another object of the present invention is to propose means of production which are simple and reliable.
• FIG. 1 illustrates an embodiment of the invention.
• FIGS 2 to 6 illustrate parts of an embodiment of the invention.
• Figure 7 illustrates a sensor used in embodiments of the invention.
• Figure 8 illustrates a dome used in embodiments of the invention.
• FIGS 8 to 15 illustrate batteries and their mounting in one embodiment of the invention.
• Figure 16 illustrates a general view of the invention.
• Figures 17 and 18 illustrate another embodiment of the invention.
• FIGS. 19 to 23 illustrate an embodiment of batteries with a support and fixing means.
• FIGS 24A to 24D illustrate one embodiment of fastening means according to the invention.
• FIGS 25 and 26 illustrate centering means according to embodiments of the invention.
• FIGS. 27A to 27F illustrate an embodiment according to the invention of means for retaining a drone.
• FIGS. 28A to 28K illustrate an embodiment according to the invention of means allowing the orientation of a drone, for example to maintain its horizontality.
• Figures 29 to 33 illustrate an embodiment according to the invention of means for refilling liquid in a drone.
• the logistics station according to the invention is provided for flying electric vehicles, such as a drone, with at least one battery, the station being adaptable to different flying vehicles and comprising at least one landing zone having means for maintaining the flying vehicle, a robot intended to exchange the batteries of the flying vehicle and/or a charge of the flying vehicle and a tank/battery charger.
• flying electric vehicles such as a drone
• the station being adaptable to different flying vehicles and comprising at least one landing zone having means for maintaining the flying vehicle, a robot intended to exchange the batteries of the flying vehicle and/or a charge of the flying vehicle and a tank/battery charger.
• the station includes a portion in the form of a circle to support the flying vehicle in the landing and take-off area.
• the holding means comprise at least three locking systems. In some embodiments, the holding means comprise two plates that are movable relative to each other.
• said circle and the holding means are fixed in the station or can move along one or more axes actuated by orientation means.
• the orientation means comprise actuators or motors coupled to supports.
• the locking means are moved according to the position of the circle.
• the locking means when the hoop is in a high position, the locking means are in an open position and when the hoop is in a low position, the locking means are in a locked position.
• the station comprises at least one battery storage and charging zone.
• batteries are mounted in a cage with a universal attachment system.
• the station includes a robot with at least one finger to move the batteries in the station.
• the station comprises means for centering the flying vehicle.
• the station includes a motion detection sensor.
• the station includes a dome to maintain constant flight conditions during takeoff and landing.
• the locking of the batteries is ensured by a guide and a locking system by spring and by a clip cooperating with the guide.
• the station is mounted on a vehicle.
• the station includes at least one station reservoir.
• the station tank comprises at least one mixer and one pump associated with a gun.
• the station includes a recuperator.
• the station is combined with at least one drone or other equivalent vehicle.
• the system according to the present invention comprises a logistics station 1 capable of accommodating several types of drones 12 or other equivalent flying vehicles as described and illustrated in detail in the present application.
• the system is capable, by appropriate means, of placing said drones in a defined position, of locking the drones 12 in the station once said position has been reached, of extracting used and/or empty batteries (or accumulators), of insert the full batteries and charge the empty batteries that have been removed.
• the system makes it possible to load and unload parcels, seeds, treatment liquids or any other load.
• the station is equipped with an intelligent battery charging system that optimizes battery life and a programmable robot capable of handling any type of payload.
• a universal battery shell/cage system easy to insert/uninsert, connect/disconnect thus making the manipulation of batteries possible by a robot.
• the landing zone 1 preferably comprises a circle 10 on which are fixed three locking systems 11 illustrated in FIG. 1.
• Each locking system 11 comprises for example guides (illustrated in the form of rollers) which can move and hold the arms of the drone.
• Figure 1 illustrates the circular landing zone 10 with three open locking systems.
• a drone 12 lands in the center of the circle 10 and on its arms 13, the systems 11 lock the arms 13 to hold the drone.
• the position of the locking systems 11 corresponding to the position of the arms 13 of the drone 12 which is variable and therefore adapts to several types of drones.
• the locking systems 11 are placed to receive a type of drone (for example with six arms as in FIG. 2) or having less than six arms or more than six arms.
• three locking systems are used
• the station is preferably adaptable to several drones (for example with three arms or more), the space under the drone is left free, the drone lands on its arms and is held stably in position, see figure 2 which illustrates the circular landing zone with a drone 12 locked.
• the landing zone comprises guides 14 in the form of rollers (circled in figure 3 which illustrates guides for precision landing) making it possible to steer the drone
• the guides 14 “pinch” the arm of the drone to be held.
• the guides 14 are preferably free to rotate to allow adjustment of the position of the drone when the three locking systems close on the arm of the drone (FIG. 2).
• Each of the locking systems 11 comprises for example 4 rollers 14 ensuring proper sliding of the drone 12 when it is locked, see in particular FIGS. 4 and 5. These rollers 14 are mobile and can approach each other to hold the arms of the drone, see Figures 1, 2, 4 and 5. In Figure 4 (or 1), they are "open” or far from each other while in Figures 2 and 5 they are “closed” or close to each other. each other.
• FIG 4 illustrates the open rollers 14 seen from the side and Figure 5 illustrates the closed rollers seen from above.
• the center of the landing zone is preferably empty, this keeps the passage free for the on-board equipment (packages, camera, detection tools, etc.) as illustrated in figure 6 which shows the landing zone free in the center.
• the drone 12 can carry bulky payloads and still land on the station.
• the station is equipped with motion detection sensors 15 to stop landing or take-off in the event of intrusion by a third party into the zone.
• Figure 7 illustrates such a motion sensor 15.
• An advantage of this feature is increased safety around the station to avoid an accident to people, for example, or damage to the drone.
• a dome 16 may surround the station in order to maintain constant flight conditions during the descent of the drone 12.
• the dome 16 is preferably equipped with a retractable roof 17 which opens and closes only during the landing / take-off phases to protect the equipment from bad weather and, for example, from external influences such as wind.
• Figure 8 shows a diagram of a dome and a retractable roof. Advantages include the stabilization of wind disturbances during landing, protection against rain, protection against vandalism.
• the station coordinates the drones 12 during the approach and waiting phases. It prioritizes drone landings based on the flight states and battery states of each drone and/or UAV (Unmanned Aerial Vehicle) or other criteria. It is therefore preferably associated with electronic means 76, see figure 281, such as one or more computers and means of communication such as a wireless network which determine the position of the drones and can organize a landing and/or take-off order and /or other drone actions, such as a control tower at an airport. Different criteria can be used such as: the state of the batteries, the urgency in relation to a load transported or to be transported, the weather and the conditions of the environment, etc.
• UAV Unmanned Aerial Vehicle
• the drones preferably communicate permanently with these electronic means to transmit status information (for example the position of the drone, the state of charge of the batteries etc.) and to receive commands (for example movement, landing, waiting etc. ).
• This management can be automated and/or programmed and/or controlled by an operator, for example depending on the mission of the drone(s) and/or the action to be taken.
• the management can be mixed, either partially automated, partially programmed and partially carried out by an operator.
• the distribution of management can vary over time or circumstances: for example an operator can "take over" in the event of a problem or choose automated actions (for example for a take-off or landing etc.) or act by remote control.
• An advantage of this realization is the centralization of flight data (battery status, %) of each drone and management of the UAV network by communicating with all the drones and vehicles concerned.
• the battery charging system is intelligent and allows longer battery life.
• the system optimizes the charge in particular in relation to the temperature and the state of the battery.
• Other parameters can be implemented, for example the age of the battery, the number of charge cycles it has undergone.
• An advantage of this way of doing things is an optimization of the battery life using an intelligent management system.
• the zone for charging the batteries is made up of a “cartridge” 20 of batteries 21 that is entirely modular. If the customer wants to increase the capacity of the station because several drones 12 must be replenished, it suffices to add a “cartridge” itself comprising several batteries.
• Batteries 21 can be attached to a hull/cage 22 forming a universal attachment system as shown in Figures 10-11 which show battery cages, batteries, fixed mounts and robot finger 31, Figure 12 which shows a fixed rack in a drone with batteries and cages and Figure 13 which shows storage with batteries and cages. It is these shells 22 which are placed in the drone 12 and in the battery storage 20. These shells 22 allow the fixing of batteries of different capacities available on the market.
• This universal system easy to insert/uninsert, connect/disconnect, makes handling of the batteries 21 possible by a robot 30 for example (see FIG. 16).
• An advantage of this system is that it is adaptable to all types of batteries, makes handling possible by a robot.
• FIG. 14 which shows fixed reception plates 25 for a hull 22 with connectors 26 on the drone 12 for mounting the batteries
• the locking of the hulls is ensured by guides and a locking system by spring as well as by the friction of the power connectors and by a clip which presses the male guide of the hull on the female guide of the battery reception module positioned under the drone.
• a module 23 for receiving the battery 21 is used to accommodate the shells in the drones and in the storage and loading space.
• These modules 23 are once again adaptable to several types of drone.
• An advantage is the standardization of the position of the battery 21 of the drones 12.
• FIG. 16 is a general illustration of an embodiment of the station according to the present invention comprising the elements described above with reference to the preceding figures.
• the station notably comprises a landing zone with battery cartridges 20, a drone 12 and the robot 30 which is used to replace the batteries and load/unload the drone according to the principles of the present invention.
• Reference 32 schematically illustrates a vehicle used to carry the station. This vehicle can be for example a truck, a trailer, a tracked vehicle, a tank such as a military tank etc. The principle of this construction applies to all the embodiments of the present invention as described in the present application.
• FIG. 17 and 18 illustrate another embodiment of the invention with a
• the landing zone 1 which comprises a circle 10 on which are fixed four locking systems 11.
• the drone 12 lands in the center of the circle 10 and on its arms 13, the systems 11 lock the arms.
• the position of the locking systems 11 corresponding to the position of the arms of the drone which is variable and therefore adapts to several types of drones.
• FIGs 19 to 23 illustrate another embodiment of the batteries 21 and their support.
• the batteries are fixed on a 22' hull/cage. It is these shells that are placed in the drone and in the battery storage. These shells allow the battery to be attached to different capacities available in the market.
• This universal system easy to insert/uninsert, connect/disconnect, makes it possible to handle the batteries by a robot and horizontally.
• this system comprises a battery 21 which is mounted in a shell 22', the latter being standard but adapted to the battery 21.
• the wires 27 electrically connect the battery 21 to the contacts 27'.
• Figure 20 illustrates batteries 30 mounted in a drone 12.
• Figure 21 more specifically illustrates the shell 22' with the contact wires 27 to the battery 21.
• Figure 22 illustrates the means used on the drone or in the storage/charging system to receive the battery 21 and its shell 22'.
• These means comprise a support 28 and contacts 29' on a contact support 29 intended to come into contact with the contacts 27' of the shell 22' (illustrated in FIG. 21).
• the assembly of the shell 22 'on the support 28 is done for example by sliding from left to right in Figure 22 and once the sliding is complete the contacts 27' of the shell 22' are in contact with the contacts 29 'of the drone 12.
• the shell 22' comprises locking means illustrated in FIG. 23.
• These locking means comprise for example an "L” clip 40 comprising at one end of the ramps 41.
• These ramps 41 are intended to enter the openings 28' of the support 28 to lock the shell 22' in position.
• the ramps 41 are held in the openings 28' by pressure springs 43.
• the robot 30 will press the "L” 40 against the spring will move the ramps 41 into the openings 28'. As they have an inclined plane, everything will go up against the spring 43 and come out of the opening 28' which releases the lock and allows the extraction of the shell 22' by sliding (for example towards the left in figure 19).
• FIGS. 24A to 24D illustrate another mode of execution of the drone 12 blocking means.
• the blocking means do not block the arms of the drone but are located under the drone and hold and center the drone 12 by its feet and lock it in the good posture.
• These means use in particular two sliding plates 50 which are moved apart from each other when the drone 12 lands and approach each other after landing to "pinch" the feet 12' of the drone 12.
• FIGS. 24A and 24B illustrate plates 50 in the closed position and Figures 24C and 24D in the open position.
• These plates 50 can also be used with the embodiment of FIG. 1 (for example) of the station 1 and form an alternative or a complement to the blocking means 11 of the embodiments. They are moved laterally for example by means of actuators and/or slideways and/or endless screws.
• Elements are preferably added to the drone to allow complete locking and mooring, for example suitable supports or fasteners for their pinching by the plates 50.
• This system can be used for multicopter drones with arms that are too short or inaccessible, but also for other types of VTOL drones (eg fixed wings or helicopters) and other UAVs.
• VTOL drones eg fixed wings or helicopters
• UAVs UAVs
• Figures 25 and 26 illustrate drone centering means. They include in particular a centering bar 51 mounted on an actuator 52 able to move it to the right in figure 26. As the station illustrated in figure 25 comprises three of them distributed at 120° (for example), the movement of the bars 51 towards the center of the station will have the effect of centering the drone that is landed.
• figure 25 it is the mode of execution of figures 27A to 27F which is illustrated with the rollers 64, the tie rods 61 and the actuators 62.
• FIGS. 27, 27A to 27F illustrate one embodiment of a station according to the present invention.
• This station has the characteristic in particular of an automatic raising and lowering of the level of the landing zone 1, namely of the circle 10, for the landing and takeoff of a drone for example.
• the locking/docking systems 60 (for example in the form of rollers) close and correct the position of the drone when the area landing zone descends and opens as the landing zone rises to release the drone for takeoff.
• FIGS. 27A to 27C illustrate the system in the closed state when the landing zone 1 is in the low position: in this position, the drone 12 is held by locking means 60 according to the principles of the present invention.
• FIGS. 25, 27D to 27F illustrate the landing zone 1 in the high position, ie open: in this position the drone 12 is no longer maintained and can take off or land.
• the passage from the high position to the low position and vice versa is carried out by actuators, such as cylinders as shown (three locking systems 60 have been shown, but there may be more).
• the locking means 60 can be actuated directly by the movement of the landing zone, for example by tie rods 61 which cause the rollers 64 of the locking means 60 to move from an open position (FIG. 27F) to a closed position (FIG. 27C).
• tie rods 61 which cause the rollers 64 of the locking means 60 to move from an open position (FIG. 27F) to a closed position (FIG. 27C).
• FIGS. 27A, B, D, E illustrate the movement of the locking means.
• the vertical movement of zone 1 can be achieved for example by mechanical, fluidic actuators 62, with guidance (for example on slides) or not.
• Each of the locking systems 60 comprises for example three rollers 64 ensuring proper sliding of the drone 12 when it is locked, see in particular FIGS. 27A, B, D, E. These rollers 64 are mobile and can tilt to hold the arms drone, see Figures 27C and 27F. In Figures 27D, E and F they are "open” i.e. away from each other while in Figures 27A, B and C they are "closed” i.e. close together and holding the drone (Figure 27B).
• FIGs 28A to 28K illustrate embodiments of a landing zone 1 whose level (or "attitude") relative to the terrain is controlled, preferably automatically, and can be modified as illustrated in the figures (leaning forward, backward, right or left etc., see Figures 28A to 28H).
• a zone 1 is useful, for example, if the system is mounted on a vehicle 32 which moves over terrain that is not flat. It is thus possible to correct the position of zone 1 (circle 10) so that it remains permanently horizontal or essentially horizontal (or in another desired position) independently of the position and orientation of the carrier vehicle 32.
• the adjustment can be made static (vehicle 32 stopped) or dynamic (vehicle 32 moving).
• the setting can be done manually or automatically.
• the means implemented are in particular two supports 70 of the zone (preferably with shock absorbers 71) linked to motors 72 and a support 73 attached to a fixed point 74 through a joint 75.
• this construction makes it possible to move the landing zone in several directions relative to the support.
• Figures 28J and 28K show construction details of the system (support 70, damper 71 and motor 72).
• These adjustable supports 70 are also visible in FIGS. 1 and 6 and can be manually or automatically adjusted (for example with a controlled jack). Dampers may or may not be present.
• a fixed point and an articulation similar to those of Figures 28A to 28K are also preferably present in the embodiment of Figures 1 to 6.
• known means are used to determine the horizontal position or that desired (for example sensors) and the control can be done for example by electronic means (computer, calculator etc.), for example placed in a case (preferably waterproof).
• FIG. 281, reference 76 These electronic means and their housing are for example illustrated in FIG. 281, reference 76. Although not specifically illustrated in all the figures, these means 76 are preferably present in all the embodiments of the present invention. More generally, all the elements of the station can be controlled (position, movement, etc.) by these electronic means, computers, computers, appropriate sensors in order to allow remote-controlled, semi-automatic or automatic operation of the station and of these parts and elements (cylinders, actuators etc.). Appropriate means of transmitting commands, information (data, measured values, etc.) are implemented: cables, transmission by waves, etc.
• the robot 30 is for example formed of an arm comprising several degrees of freedom in rotation and allows so-called "pick and place” movements: grabbing a battery, extracting it from its support (on the drone 12 or in the tank 20 ) and replace it at its intended destination (for example in the reservoir 20 for its recharging if it comes from the drone 12, or the reverse if it comes from the reservoir 20).
• Figures 29 to 33 illustrate an embodiment of the means for filling the tank of a drone, for example with a liquid.
• These means illustrated in figure 29 comprise in particular a station tank 80 with a filler cap 81, a mixer 82 (which makes it possible to maintain movement in the liquid if necessary) and a pump 83.
• This figure also shows wheels 84 which allow the tank to be moved to fill it.
• the means further comprise a pipe 85 connected at one end to the pump 83 and at the other end to a gun 86. 86 pistol as described below.
• the reservoir 80 is preferably located in the lower part 1' of the station 1 (see FIG. 30) and this part comprises for example doors 88, 88' which make it possible to bring out the reservoir 80 on its rollers 84 in order to fill it.
• FIG 31 the filling of a tank 90 of a drone 12 is illustrated.
• the gun 86 is brought by the robot 30 and introduced into the chute 91 of the reservoir 90 and the liquid from the reservoir of the station 80 introduced into the reservoir 90 of the drone 12.
• Figure 32 illustrates station 1 of figure 30 to which a liquid recuperator 92 has been added which is useful for recovering liquids which would flow out during filling.
• the recuperator 92 preferably surrounds the drone and seals the loading area.
• FIG. 33 illustrates in detail an embodiment of the filling gun 86 of station 1.
• the gun 86 is held in a support 93 which allows it to be manipulated by the robot 30 and the support further comprises actuating means.
• actuating means are for example a motor 94 linked to a worm screw 95 which acts on an actuating means 96 articulated on an axis 97.
• the rotation of the screw 95 will cause the actuating means 96 to tilt to the left or the right (depending on the direction of rotation of the screw) and the actuating means by tilting it to the right (in Figure 33) will press the trigger 98 of the gun 86 and allow the flow of liquid in the tank 90 of the drone 12.
• One rotation in the other sense will release the trigger and interrupt the feed.
• the materials used to manufacture the parts of the present invention are any suitable materials: metal, synthetic materials or combinations of materials. Everything is preferably managed by computer means such as one or more computers, information transmission means and wire or wireless controls (Wifi, Bluetooth® etc.).
• the system for example as illustrated in FIG. 16 in all its embodiments can be mounted on a vehicle 32 (for example an all-terrain vehicle) or a trailer.
• the use of the system can be military and/or civilian. It is also possible to envisage a system with several stations as described in the present application, identical or different (for example according to different embodiments).

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• Engineering & Computer Science (AREA)
• Aviation & Aerospace Engineering (AREA)
• Remote Sensing (AREA)
• Mechanical Engineering (AREA)
• Transportation (AREA)
• Power Engineering (AREA)
• Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
• Loading Or Unloading Of Vehicles (AREA)
• Window Of Vehicle (AREA)

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• 2021
  • 2021-09-15 WO PCT/IB2021/058399 patent/WO2022058903A1/fr unknown
  • 2021-09-15 CN CN202180068403.8A patent/CN116348379A/zh active Pending
  • 2021-09-15 US US18/026,366 patent/US20230348121A1/en active Pending
  • 2021-09-15 EP EP21786261.4A patent/EP4214122A1/de active Pending
  • 2021-09-15 IL IL301398A patent/IL301398A/en unknown

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