• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Loading device coupled to a drone designed to transport small loads, in a fast and simple manner, comprising a structure (1) of carbon fiber or similar, which is coupled to the landing gear of a drone (20); and wherein said structure (1) incorporates a chassis (2) where a hoist or the like (3) is connected, connected with an electric motor (8) that drives it, and where said hoist (3) has a kevlar thread (4). ), joined with magnets (5) that are attached to a carabiner (6) in charge of joining and holding the load (10) to be transported. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2627308A1
    申请号:ES201630094
    申请日:2016-01-26
    公开日:2017-07-27
    发明作者:Juan Francisco CAÑADILLAS SANCHEZ
    申请人:Juan Francisco CAÑADILLAS SANCHEZ；
    IPC主号:
    专利说明:

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    DESCRIPTION
    DRON COUPLABLE LOAD DEVICE
    Object of the invention
    The object of the present report is a charging device that can be attached to a drone, specially designed to transport small loads, in a quick and simple way. This makes this device an ideal means for transporting small loads, such as medical kits or small messaging packages.
    Background of the invention
    Currently, a drone is an unmanned aerial vehicle, used in both military and civilian applications. These drones are small planes that can be controlled from a remote location, or carry elements that allow autonomous handling, through sophisticated navigation elements included in it, which allow you total autonomy in your flight.
    The technological advance that these drones have supposed, has meant that they have gradually gone down in price (due to multiple factors, such as, for example, the increase in actors in said technical sector, who apply a competition that causes a price drop, between others) and its use has been standardized at a particular level.
    Therefore, the use of drones in various commercial applications, such as aerial photography, is becoming increasingly common. This has caused, that from other commercial sectors (such as transport) are designing solutions for the application of these drones in their commercial activity (thanks to the cost savings that would entail), but have the main drawback, which Drones are not capable of transporting loads, which makes it difficult to use so far.
    Description of the invention
    The technical problem that solves the present invention is to achieve a means attachable to a drone, capable of transporting small loads safely. For this, the charging device attachable to a drone, object of the present specification, is characterized by
    comprise carbon fiber structure or the like, which attaches to the landing gear of
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    a drone, and incorporates a chassis where a hoist is housed that has a kevlar thread wrapped, joined with magnets and a carabiner responsible for joining and holding the load to be transported.
    Thanks to its design, the device recommended here can be attached to a drone safely, facilitating the transport of its cargo, thanks to its low weight and consumption, the drone will hardly lose efficiency in its flight.
    This device will be controlled by radio control, in the same way that the aircraft is controlled, simply assigning one or more channels for the electronic control of said device, which in turn controls the electric motor to raise or lower the wire with the load, This load can be very different, from medical kits with defibrillators, to any other object with a volume appropriate to the load capacity of the device.
    The cargo will travel safely during the flight, since the device presented here takes advantage of the drone's own landing gear, attaching a structure with anchors that secure the suspended load ah during the trip. To lower the load, you would just have to open the landing gear and it would be suspended at that moment from the hoist and its thread.
    To remove the load, it can be done through two options, the first option is by means of a carabiner that the user receiving the payment load opens to unpin the bag or suitcase. The second option, is by means of an electronic in the bag or suitcase with electromagnets, this system can be unpinned the bag or suitcase automatically when touching land or at the distance that is programmed with proximity sensors in the bag or suitcase, besides being able to undo by means of manual carabiner and / or safety mushroom in the bag or suitcase.
    In the case where the user does not disengage the carabiners and pull the package, and in order to avoid a possible "demolition" of the drone by the tiron received if it were of a high intensity, the system has anti-tension magnets.
    Throughout the description and claims the word "comprises" and its variants are not intended to exclude other technical characteristics, additives, components or steps. For those skilled in the art, other objects, advantages and characteristics of the invention will be derived partly from the description and partly from the practice of the invention. The
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    The following examples and drawings are provided by way of illustration, and are not intended to restrict the present invention. In addition, the present invention covers all possible combinations of particular and preferred embodiments indicated herein.
    Brief description of the figures
    A series of drawings that help to better understand the invention and that expressly relate to an embodiment of said invention that is presented as a non-limiting example of this is described very briefly below.
    FIG 1. Shows a perspective view of the loading device that can be attached to a drone, coupled to the aircraft or drone.
    FIG 2. Shows a schematic view of the charging device attachable to a drone, object of the present specification.
    FIG 3. Shows a schematic view in detail of the elements that facilitate the unloading of the cargo transported in the charge device attachable to a drone.
    Preferred Embodiment of the Invention
    A preferred embodiment of the invention is shown in the attached figures. More specifically, the charging device attachable to a drone, object of the present utility model, which is characterized in that it comprises a structure (1) of carbon fiber or the like, which is coupled to the landing gear of a drone (20) and where said structure (1) incorporates a chassis (2) where a hoist or similar (3) is connected connected to an electric motor (8) that drives it, and where said hoist (3) has a kevlar wire wound (4). or a material with equivalent mechanical characteristics, together with magnets (5) that prevent the drone from falling, in case the load (10) gets stuck or has not been released correctly by the user; and a carabiner (6) responsible for joining and securing the load (10) to be transported.
    The chassis (2) incorporates two lateral structures (2a, 2b), composed of a steel bar (21), a bearing (22) and a prisoner (23), which serve as a means of joining the chassis (2) with the hoist (3).
    The motor (8) is connected to electronic control means (7), composed of an "encoder" or encoder (7a) responsible for adapting the energy consumption of the device, electronic control means (7b) to activate the different functionalities of the device, and a radio control transmitter (7c) to remotely control the device, simply assigning it one or more channels for the control of the drone electronics (20).
    In a practical embodiment, the device incorporates a servomotor (9) coupled to the chassis (2), as an auxiliary motor to automatically increase the available energy when it is convenient.
    In a particular embodiment, the load (10) will have a fixed structure or shape, and will incorporate electromagnets (11) that will be released once the load (10) touches or is next to it, thanks to the presence of at least a proximity sensor (12) located at said load (10).
    In addition, in said embodiment, a second electronic means (13) with battery, and a manual actuation means (14) will also be included, which allow to control how the load is released (10) avoiding possible drone accidents (20).
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    In a practical embodiment, the chassis (2) will incorporate a cover that completely covers it to avoid possible damage.
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    权利要求:
    Claims (6)
    [1]
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    1. - Loading device coupled to a drone that is characterized in that it comprises a structure (1) of carbon fiber or the like, which is coupled to the landing gear of a drone (20); and where said structure (1) incorporates a chassis (2) where a hoist or similar (3) is connected connected to an electric motor (8) that drives it, and where said hoist (3) has a kevlar wire wound (4) ), together with magnets (5) that are attached to a carabiner (6) responsible for joining and holding the load (10) to be transported.
    [2]
    2. - Device according to claim 1 wherein the chassis (2) incorporates two lateral structures (2a, 2b), composed of a steel bar (21), a bearing (22) and a prisoner (23), which They serve as a means of joining the chassis (2) with the hoist (3).
    [3]
    3. - Device according to any of claims 1 - 2 wherein the motor (8) is connected with electronic control means (7), composed of an encoder (7a) responsible for adapting the energy consumption of the device; electronic control means (7b) to activate the different functionalities of the device; and a radio control transmitter (7c) to remotely control the device, simply assigning it one or more channels for the control of the drone electronics (20).
    [4]
    4. - Device according to any of claims 1 - 3 wherein the chassis (2) incorporates a servomotor (9).
    [5]
    5. - Device according to any of the preceding claims wherein the load (10) has a fixed structure or shape, and incorporates electromagnets (11) that are released once the load (10) touches ground or is close to this, thanks to the presence of at least one proximity sensor (12) located in said load (10); and where, in turn, it incorporates a second electronic means (13) with battery, and a manually operated means (14), which allow to control how the load is released (10) avoiding possible drone accidents (20).
    [6]
    6. - Device according to any of the preceding claims wherein the chassis (2) incorporates a cover that completely covers it to avoid possible damage.
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    同族专利:
    公开号 | 公开日
    ES2627308B1|2018-04-12|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US9174738B1|2013-04-14|2015-11-03|Google Inc.|Drag disk, small|
    US9205922B1|2013-07-17|2015-12-08|The Boeing Company|Systems and methods for implementing a payload distribution system|
    US20150158587A1|2013-08-26|2015-06-11|Google Inc.|Mechanisms for Lowering a Payload to the Ground from a UAV|
    US20150120094A1|2013-10-26|2015-04-30|Amazon Technologies, Inc.|Unmanned aerial vehicle delivery system|
    FR3017109A1|2014-02-04|2015-08-07|Christophe Pesenti|AERIAL DRONE FOR LAND RESCUE OR MARITIME|
    US9174733B1|2014-08-28|2015-11-03|Google Inc.|Payload-release device and operation thereof|
    DE202015105415U1|2015-09-15|2015-10-26|Thunder Tiger Corporation|Multicopter with the possibility to carry rescue equipment|
    法律状态:
    2018-04-12| FG2A| Definitive protection|Ref document number: 2627308 Country of ref document: ES Kind code of ref document: B1 Effective date: 20180412 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201630094A|ES2627308B1|2016-01-26|2016-01-26|DRON COUPLABLE LOAD DEVICE|ES201630094A| ES2627308B1|2016-01-26|2016-01-26|DRON COUPLABLE LOAD DEVICE|
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