• 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:
    A levitating solar aircraft parking lot and an associated single-bladed unmanned aerial vehicle include an aircraft parking lot and a single-bladed unmanned aerial vehicle. The aircraft parking area floats in the air by means of the buoyancy of a float ball. The single-blade unmanned aerial vehicle is only equipped with a single main propeller and has few drive units. Compared to conventional unmanned aerial vehicles with multiple propellers, the flight is more stable and there is less turbulence and vibration. The invention provides a levitating solar aircraft parking space and an associated single-bladed unmanned aerial vehicle. The aircraft parking area floats in the air, does not take up any floor space and does not require any special staff to assist. With stable operation, the unmanned aerial vehicle can ensure safe transportation of the packages.
    公开号:BE1027331B1
    申请号:E20205444
    申请日:2020-06-18
    公开日:2021-03-12
    发明作者:Zhong Yang；Yulong Wu；Zhenzhong Yu；Yujuan Tang；Xiaomin Tian
    申请人:Jinling Inst Technology；
    IPC主号:
    专利说明:

    Hovering solar aircraft parking area and associated single-blade unmanned aerial vehicle
    FIELD OF THE INVENTION The present invention enters the field of transportation by means of an unmanned aerial vehicle, in particular a floating solar aircraft parking area and an associated single-bladed unmanned aerial vehicle.
    BACKGROUND ART When transported by unmanned aerial vehicle, packages are transported by unmanned aerial vehicles at low altitude, which are operated with radio remote control devices and provided program control devices, and are automatically delivered to the destination. Thus, advantages such as solving the delivery problem in remote areas, improving delivery efficiency, and lowering labor costs are achieved. Existing unmanned aerial vehicle transport devices are based on conventional unmanned aerial vehicles. In this case, due to an existing unmanned aircraft, a carrier for receiving packages is also provided. During the operation of the unmanned aerial vehicle, the packages easily fall off due to strong turbulence. Drop the package. In addition, an unmanned aerial vehicle has to travel a long distance from a parcel distribution point to the destination and there is no suitable transit platform. In fully populated residential areas, there is a lack of large open space for the construction of a transit aircraft parking area for unmanned aircraft. In addition, a ground transit aircraft parking area requires special personnel care, thereby wasting manpower.
    > BE2020 / 5444
    DISCLOSURE OF THE INVENTION To solve the above problem, the present invention is based on the object of providing a floating solar aircraft parking space and an associated single-blade unmanned aerial vehicle, the aircraft parking space floating in the air, taking up no floor space and not requiring any special staff. With stable operation, the unmanned aerial vehicle can ensure safe transportation of the packages. According to the invention, the object is achieved by a floating solar aircraft parking space and an associated single-blade unmanned aircraft, which include an aircraft parking area and a single-blade unmanned aircraft, the aircraft parking area being designed as a centrally symmetrical panel body, an aircraft parking platform being provided in the middle of the panel body, whereby on the plate body, a solar panel is arranged evenly around the aircraft parking platform, a float ball that is evenly arranged on the edge of the plate body and filled with helium on the inside, the aircraft parking area being able to float in the air under the action of a buoyancy force of the float ball, with the surrounding area Edge of the plate body further at least three horizontally arranged horizontal alignment motors are centrally symmetrically arranged, the output end of which is connected to a horizontal drive propeller, wherein the central axis of each of the horizontal drive propellers runs through the center line of the plate body, a support plate being provided on the underside of the plate body, the single-bladed unmanned aerial vehicle comprising a hollow cylindrical fuselage in which a main drive motor is provided, the output end of which is designed as a main propeller, An air inlet screen plate is provided on the upper side of the fuselage, with air outside the fuselage entering the fuselage via the air inlet screen plate by turning the main propeller, with at least three drive force air outlets circumferentially on the outer surface of the fuselage, the air outlet direction of which is vertically downwards directed, are arranged evenly, with at least three torque compensation air outlets running around the circumferential surface of the fuselage, the air outlet direction of which is horizontal,
    are evenly arranged, the air outlet direction of the torque compensation air outlets corresponds to the direction of rotation of the main propeller, a support beam is provided on the underside of the fuselage, the lower end of which is provided with a support foot and on which a mounting plate is provided, on which mounting plate a main control board and a battery and an attitude sensor, which are connected to the main control board, are provided, wherein a camera is further provided on the mounting plate, which is connected to an output end of a first motor, the first motor is connected to an output end of a second motor, the Axes of the first motor and the second motor are perpendicular to each other, the second motor being arranged vertically, the camera being able to rotate through 360 degrees under the drive of the first motor and the second motor, wherein in the center of the underside of the mounting plate also a On it Vision camera is provided, the lens of which is directed vertically downwards, the battery being used to supply power to the main drive motor, the first motor, the second motor, the attitude sensor and the top view camera. In a further development of the invention it is provided that at the exit of both the drive force air outlet and the torque compensation air outlet, an adjusting device is provided in each case, which comprises an adjusting plate arranged on the central axis of the respective air outlet, one end of the adjusting plate having an outlet end one Adjustment plate drive motor is connected and can pivot under drive from the motor, the adjustment plate drive motor is fixedly connected to the inner wall of the air outlet via an adjustment plate motor mounting bracket, while the other end of the adjustment plate is connected to a hinge holder which is fixed to the inner wall of the air outlet is connected. In a further development of the invention it is provided that the adjusting plate is arranged vertically within the torque compensation air outlet and the axis of rotation of the adjusting plate intersects with the center line of the plate body of the aircraft parking area within the driving force air outlet.
    In a further development of the invention it is provided that both the panel body of the aircraft parking area and the fuselage of the unmanned aircraft are made from one
    Aluminum alloy material or a hard plastic are made. The floating solar aircraft parking area and the associated single-blade unmanned aerial vehicle are distinguished by the following features: 1) The present application comprises a floating solar aircraft parking area. The aircraft parking space floats in the air under the action of the float ball and its underside can be connected to the floor via a pull rope and thus does not take up any floor space. The aircraft parking space has a horizontally arranged horizontal drive propeller, the rotation of which ensures the stability of the aircraft parking space in the air. The electrical energy consumed by the aircraft parking area is provided by a solar panel, with which environmental friendliness and low energy consumption are achieved. 2) The present application comprises a single-bladed unmanned aerial vehicle. The unmanned aerial vehicle is provided with only a single blade for drawing in air. The unmanned aerial vehicle can fly by ejecting air downward through the propulsion air outlet. Due to the small number of drive units, more stable flight and less turbulence and vibration are achieved compared to conventional unmanned aircraft. At the same time, a torque compensation air outlet is provided to counteract the torque generated by the rotation of the main propeller and thus prevent the fuselage from turning during flight. At the same time, the drive force air outlet and the torque compensation air outlet are also provided with an adjusting device in order to adjust the air outlet direction of the air outlet and thus to realize an adjustment of the flight direction of the unmanned aircraft.
    DESCRIPTION OF THE INVENTION FIG. 1 shows a floating solar aircraft parking area and an associated single-blade unmanned aircraft according to the present invention in a schematic structural illustration,
    FIG. 2 shows the single-bladed unmanned aircraft according to the present invention in a schematic representation, FIG. 3 shows the single-bladed unmanned aerial vehicle according to the present invention in a first schematic detail view, FIG. 4 shows the single-blade unmanned aircraft according to the present invention in a second schematic detail view, FIG the single-bladed unmanned aerial vehicle according to the present invention in a third schematic detail view, FIG. 6 the setting device of the single-bladed unmanned aerial vehicle according to the present invention in a schematic representation. Description of the reference symbols:
    1. Torque compensation air outlet, 2. Air inlet sieve plate, 3. Driving force air outlet, 4. Support bracket, 5. Support foot, 6. Main control board, 7. Battery, 8. Camera, 9. First motor, 10. Second motor, 11. Attitude sensor, 12th top view camera,
    13. main propeller, 14. main propulsion motor, 15. adjustment plate motor mounting bracket,
    16. Adjustment Plate Drive Motor, 17. Adjustment Plate, 18 Hinge Bracket, 19. Float Ball, 20. Solar Panel, 21. Aircraft Parking Platform, 22. Horizontal Alignment Motor, 23. Horizontal Drive Propeller, 24. Support Plate. Concrete Embodiments The following is a closer look at the present invention with reference to the drawings based on specific embodiments: The floating solar aircraft parking area and the associated single-blade unmanned aircraft according to FIG. 1 include an aircraft parking area and a single-blade unmanned aircraft. The aircraft parking area is designed as a regular hexagonal plate body. An aircraft parking platform 21 is provided in the middle of the plate body. A solar panel 20 is arranged uniformly around the aircraft parking platform 21 on the plate body. Six float balls 19 are evenly arranged around the edge of the plate body. Everyone who
    Float ball 19 is filled with helium on the inside.
    The aircraft parking area can float in the air under the action of a buoyancy force of the float ball 19.
    Furthermore, three horizontally arranged horizontal alignment motors 22 are arranged centrally symmetrically around the edge of the plate body, the output end of which is connected to a horizontal drive propeller 23.
    The central axis of each of the horizontal drive propellers 23 passes through the center line of the plate body.
    A support plate 24 is provided on the underside of the plate body.
    The panel body can be connected to the floor via a pull rope.
    Under the action of the float ball 19, the plate body floats in the air.
    The buoyancy force of the float ball 19 is greater than the sum of the weights of the aircraft parking area and the unmanned aircraft loaded with packages.
    The aircraft parking space has a horizontally arranged horizontal drive propeller 23, the rotation of which ensures the stability of the aircraft parking space in the air.
    The electrical energy consumed by the aircraft parking area is provided by the solar panel 20, whereby environmental friendliness and low energy consumption are achieved.
    As can be seen from FIGS. 2, 3, 4 and 5, the single-bladed unmanned aerial vehicle comprises a hollow cylindrical fuselage in which a main drive motor 14 is provided, the output end of which is designed as a main propeller 13.
    An air inlet screen plate 2 is provided on the top of the fuselage.
    By turning the main propeller 13, air outside the fuselage enters the fuselage via the air inlet screen plate 2.
    Circumferentially on the lateral surface of the fuselage, three driving force air outlets 3, the air outlet direction of which is directed vertically downwards, are arranged uniformly.
    Three torque compensation air outlets 1, the air outlet direction of which runs horizontally, are arranged uniformly around the circumferential surface of the fuselage.
    The air outlet direction of the torque compensation air outlets 1 corresponds to the direction of rotation of the main propeller 13. On the underside of the fuselage a support beam 4 is provided, the lower end of which is provided with a support foot 5 and on which a mounting plate is provided, on which mounting plate a main control board 6 and a Battery 7 and a
    Attitude sensor 11, which are connected to the main control board, are provided. A camera 8 is also provided on the mounting plate and is connected to an output end of a first motor 9, which first motor 9 is connected to an output end of a second motor 10. The axes of the first motor 9 and the second motor 10 are perpendicular to one another. The second motor 10 is arranged vertically. The camera 8 can rotate 360 degrees under the drive of the first motor 9 and the second motor. In the middle of the underside of the mounting plate, a top view camera 12 is also provided, the lens of which is directed vertically downwards. The battery 7 is used to supply power to the main drive motor 14, the first motor 9, the second motor 10, the attitude sensor 11 and the top view camera 12. An adjustment device is provided at the exit of the driving force air outlet 3 and the torque compensation air outlet 1. 6 shows the driving force air outlet 3 as an example. The adjusting device comprises an adjusting plate arranged on the central axis of the respective air outlet
    17. One end of the adjusting plate 17 is connected to an output end of a drive motor 16 of the adjusting plate 17 and can pivot under drive from the motor. The drive motor 16 of the adjusting plate 17 is fixedly connected to the inner wall of the air outlet via a motor mounting bracket 15 of the adjusting plate 17, while the other end of the adjusting plate 17 is connected to a hinge holder 18 which is fixedly connected to the inner wall of the air outlet. Within the torque compensation air outlet 1, the adjusting plate 17 is arranged vertically and within the driving force air outlet 3, the axis of rotation of the adjusting plate 17 intersects with the center line of the plate body of the aircraft parking area. An adjusting device for adjusting the air outlet direction is also provided on the drive force air outlet 3 and the torque compensation air outlet 1, in order to thus implement an adjustment of the flight direction of the unmanned aircraft. Both the panel body of the aircraft parking area and the fuselage of the unmanned aerial vehicle are made of an aluminum alloy material in order to minimize their own weight. In practical use, the flight environment of the unmanned aerial vehicle can be viewed in real time by the camera 8 above the mounting plate and the one below
    Top view camera 12 can be observed.
    A package basket or the like for receiving packages is provided on the outside of the support carrier 4.
    The aircraft parking spaces can be arranged at a certain distance from one another.
    The aircraft parking area can also be provided with a battery 7 and a wireless charger.
    The solar panel 20 charges the battery 7 continuously.
    When the unmanned aircraft is parked in the aircraft parking area, it can also be charged using the wireless charger.
    So far, only preferred exemplary embodiments of the present invention have been explained without restricting the invention in any way.
    Any modification and equivalent variant based on the basic technical idea of the invention is encompassed by the claimed scope of protection of the invention.
    权利要求:
    Claims (4)
    [1]
    1. Floating solar aircraft parking area and associated single-blade unmanned aircraft, characterized in that they comprise an aircraft parking area and a single-blade unmanned aircraft parking area, the aircraft parking area being designed as a centrally symmetrical panel body, an aircraft parking platform being provided in the middle of the panel body, on which Plate body, a solar panel is arranged evenly around the aircraft parking platform, with a float ball evenly arranged around the edge of the plate body, which is filled with helium on the inside, the aircraft parking area being able to float in the air under the action of a buoyancy force of the float ball, with the surrounding edge of the Plate body further at least three horizontally arranged horizontal alignment motors are centrally symmetrically arranged, the output end of which is connected to a horizontal drive propeller, the central axis of each de The horizontal drive propeller runs through the center line of the plate body, with a support plate being provided on the underside of the plate body, the single-bladed unmanned aerial vehicle comprising a hollow cylindrical fuselage in which a main drive motor is provided, the output end of which is designed as a main propeller Top of the fuselage an air inlet screen plate is provided, whereby by turning the main propeller, air outside the fuselage enters the fuselage via the air inlet screen plate, with at least three drive force air outlets circumferentially on the outer surface of the fuselage, the air outlet direction of which is vertically downwards, are arranged evenly, with at least three torque compensation air outlets, the air outlet direction of which runs horizontally, being arranged evenly on the circumferential surface of the fuselage, the air outlet direction of the torque compensation air outlets in the direction of rotation of the main propeller, with a support beam being provided on the underside of the fuselage, the lower end of which is provided with a support foot and on which a mounting plate is provided, on which mounting plate a main control board as well as a battery and an attitude sensor, which are connected to the main control board, are provided, wherein a camera is also provided on the mounting plate with a
    Output end of a first motor is connected, the first motor is connected to an output end of a second motor, the axes of the first motor and the second motor being perpendicular to each other, the second motor being arranged vertically, the camera being driven by the first Motor and the second motor can rotate 360 degrees, in the middle of the underside of the mounting plate also a top view camera is provided, the lens is directed vertically downwards, the battery for powering the main drive motor, the first motor, the second motor, the Attitude sensor and the top view camera is used.
    [2]
    2. Floating solar aircraft parking space and associated single-blade unmanned aircraft according to claim 1, characterized in that an adjusting device is provided at the exit of both the driving force air outlet and the torque compensation air outlet, which comprises an adjusting plate arranged on the central axis of the respective air outlet wherein one end of the adjustment plate is connected to an output end of an adjustment plate drive motor and can pivot under drive from the motor, the adjustment plate drive motor being fixedly connected to the inner wall of the air outlet via an adjustment plate motor mounting bracket, while the other end of the adjustment plate with a hinge holder is connected, which is firmly connected to the inner wall of the air outlet.
    [3]
    3. Floating solar aircraft parking space and associated single-blade unmanned aircraft according to claim 2, characterized in that the adjusting plate is arranged vertically within the torque compensation air outlet and the axis of rotation of the adjusting plate intersects with the center line of the plate body of the aircraft parking space within the driving force air outlet.
    [4]
    4. Floating solar aircraft parking area and associated single-blade unmanned aircraft according to one of claims 1 to 3, characterized in that both the plate body of the aircraft parking area and the fuselage of the unmanned aircraft are made of an aluminum alloy material or a hard plastic.
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    同族专利:
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    引用文献:
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    CN109733598A|2018-11-26|2019-05-10|顺丰科技有限公司|Aircraft duct and culvert type aircraft|
    CN110217373A|2019-06-20|2019-09-10|金陵科技学院|A kind of solar energy floating airplane parking area and mating single blade unmanned plane|CN110217373A|2019-06-20|2019-09-10|金陵科技学院|A kind of solar energy floating airplane parking area and mating single blade unmanned plane|
    法律状态:
    2021-03-19| FG| Patent granted|Effective date: 20210312 |
    优先权:
    申请号 | 申请日 | 专利标题
    CN201910537047.4A|CN110217373A|2019-06-20|2019-06-20|A kind of solar energy floating airplane parking area and mating single blade unmanned plane|
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