WO2020253614A1 - 一种太阳能浮空停机坪及配套单叶片无人机 - Google Patents

一种太阳能浮空停机坪及配套单叶片无人机 Download PDF

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Publication number
WO2020253614A1
WO2020253614A1 PCT/CN2020/095624 CN2020095624W WO2020253614A1 WO 2020253614 A1 WO2020253614 A1 WO 2020253614A1 CN 2020095624 W CN2020095624 W CN 2020095624W WO 2020253614 A1 WO2020253614 A1 WO 2020253614A1
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WIPO (PCT)
Prior art keywords
motor
apron
fuselage
blade
plate
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PCT/CN2020/095624
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English (en)
French (fr)
Inventor
杨忠
吴有龙
余振中
唐玉娟
田小敏
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金陵科技学院
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Publication of WO2020253614A1 publication Critical patent/WO2020253614A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/30—Launching, take-off or landing arrangements for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/24—Arrangement of propulsion plant
    • B64B1/30—Arrangement of propellers
    • B64B1/32—Arrangement of propellers surrounding hull
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/30—Lighter-than-air aircraft, e.g. aerostatic aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/34—In-flight charging
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/20—Launching, take-off or landing arrangements for releasing or capturing UAVs in flight by another aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/60—UAVs characterised by the material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
    • B64U2101/64—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for parcel delivery or retrieval

Definitions

  • the invention relates to the field of unmanned aerial vehicle distribution, in particular to a solar floating apron and a supporting single-blade unmanned aerial vehicle.
  • Unmanned aerial vehicle distribution that is, unmanned low-altitude aircraft operated by radio remote control equipment and self-provided program control devices to carry packages and automatically deliver them to their destinations. Its advantages are mainly to solve the distribution problems in remote areas and improve the efficiency of distribution. At the same time reduce labor costs.
  • the existing UAV delivery equipment is based on the traditional UAV design, and most of the existing UAVs are equipped with brackets for placing the packages.
  • the drones are bumpy during the operation, which may easily cause the packages to fall over.
  • the distance between drones transported from the parcel collection and distribution point to the destination is long, there is no suitable transfer platform, and the residential area with concentrated residents lacks a large area of open space for the construction of drone transfer and stopping points, and the ground stopping points require special care, which is wasteful Manpower.
  • the present invention provides a solar floating apron and a supporting single-blade drone.
  • the apron is suspended in the air, does not occupy ground space and does not require special personnel for care, and the drone runs smoothly to ensure the safety of the package. transport.
  • the present invention provides a solar floating apron and a supporting single-blade drone, including the apron and the single-blade drone.
  • the apron is a plate with a central symmetrical shape, and the center of the plate is the apron.
  • Platform Solar panels are evenly arranged around the parking platform on the board.
  • Floating balls are evenly arranged around the edge of the board.
  • the floats are filled with helium.
  • the apron can float in the air under the buoyancy of the floating balls.
  • At least three horizontally arranged horizontally oriented motors are arranged symmetrically in the center, the output end of which is connected with horizontal driving propellers, the central axis of each horizontal driving propeller passes through the center line of the plate body, and the bottom of the plate body is provided with a support plate; the single blade has no
  • the man-machine includes a hollow cylindrical fuselage.
  • the fuselage is equipped with a main drive motor.
  • the output end of the main drive motor is a main propeller.
  • the top of the fuselage is equipped with an intake screen.
  • the main propeller rotates to make the outside air of the fuselage pass the intake screen.
  • the board enters the fuselage, and the side of the fuselage is evenly provided with no less than three vertical downward power outlets in the air outlet direction, and the side of the fuselage is evenly provided with no less than three horizontal torque offset air outlets in the air outlet direction.
  • the direction of the torque offset air outlet is the same as the rotation direction of the main propeller.
  • the bottom of the fuselage is provided with a support frame, the lower end of the support frame is provided with support feet, the support frame is provided with a fixed plate, and the fixed plate is provided with a main control board and connected to it.
  • the battery, and the attitude sensor, the fixed board is also provided with a camera, which is connected to the output end of the first motor, the first motor is connected to the second output end of the motor, the first motor is perpendicular to the second axis of the motor, and the second motor is arranged vertically.
  • the camera is located between the first motor and the motor A 360° rotation can be achieved under the driving of the second plate; the bottom center of the fixed plate is also provided with a top view camera, the top view camera lens is vertically downward, and the battery is used to supply power to the main driving motor, motor one, motor two, attitude sensor and top view camera.
  • an adjustment device is provided at the outlet of the power outlet and the torque offset outlet, and the adjustment device includes an adjustment plate located at the central axis of the outlet.
  • One end of the adjustment plate is connected to the output end of the adjustment plate drive motor.
  • the adjusting plate driving motor is fixedly connected to the inner wall of the air outlet by the adjusting plate motor fixing seat, the other end of the adjusting plate is connected to the hinge support, and the hinge support is fixedly connected to the inner wall of the air outlet.
  • the adjusting plate in the torque counteracting air outlet is arranged vertically, and the rotation axis of the adjusting plate in the power air outlet intersects at the center line of the apron plate body.
  • the apron board body and the drone body are both made of aluminum alloy material or hard plastic.
  • the application is a solar floating apron and supporting single-blade drone, which has the following characteristics:
  • This application includes a solar floating apron.
  • the apron can be controlled by the floating ball.
  • the bottom of the apron can be connected to the ground by a pull rope, which does not occupy ground space.
  • the apron has a horizontally set horizontal drive propeller, which drives the propeller to rotate horizontally. It can ensure that the apron is stable in the control position, and the power consumed by the apron is provided by solar panels, which is clean and environmentally friendly, with low energy consumption;
  • This application includes single-blade drones.
  • the drones are only equipped with separate blades for air intake, and the power outlet is used to exhaust the air downward to realize the drone flight. Because of its fewer power units, it is different from the traditional multi-propeller. Compared with drones, the flight is more stable, with less turbulence and jitter. At the same time, it is equipped with a torque cancellation air outlet to offset the torque generated by the rotation of the main propeller and prevent the fuselage from rotating during flight. At the same time, the power air outlet and torque offset the output The air port is also provided with an adjusting device to adjust the air outlet direction, so as to adjust the flying direction of the drone.
  • Figure 1 is a schematic diagram of the apron and supporting single-blade UAV of the present invention
  • FIG. 2 is a schematic diagram of the single-blade UAV of the present invention.
  • FIG. 3 is a partial schematic diagram 1 of the single-blade UAV of the present invention.
  • Figure 4 is the second partial schematic diagram of the single-blade UAV of the present invention.
  • Figure 5 is the third partial schematic diagram of the single-blade UAV of the present invention.
  • Fig. 6 is a schematic diagram of a single-blade UAV direction adjusting device of the present invention.
  • the apron is a regular hexagonal board.
  • the center of the board is the parking platform 21.
  • the solar panels 20 are evenly arranged around the parking platform 21 on the board.
  • Six floating balls 19 are evenly arranged on the edge of the board.
  • Each floating ball 19 is filled with helium gas, and the apron can float in the air under the buoyancy of the float 19.
  • Three horizontally arranged horizontally oriented motors 22 are arranged symmetrically around the edge of the board.
  • the output end is connected with a horizontal drive propeller 23, each The central axis of the horizontal driving propeller 23 passes through the center line of the plate body, and a support plate 24 is provided at the bottom of the plate body.
  • the board body can be connected to the ground by a draw rope, and the board body floats in the air under the action of the floating ball 19, which is larger than the total weight of the apron and the package carried by the drone.
  • the apron has a horizontally set horizontal driving propeller 23.
  • the rotation of the horizontal driving propeller 23 can ensure that the apron is stable in a controlled position.
  • the power consumption of the apron is provided by the solar panel 20, which is clean and environmentally friendly, and has low energy consumption.
  • the single-blade UAV shown in Figures 2, 3, 4 and 5 includes a hollow cylindrical fuselage, a main drive motor 14 is arranged in the fuselage, and the output end of the main drive motor 14 is a main propeller 13, and the top of the fuselage is arranged There is an intake screen 2, the main propeller 13 rotates to make the outside air of the fuselage enter the fuselage from the intake screen 2.
  • the side of the fuselage is evenly provided with three power outlets 3 with the air outlet direction vertically downward.
  • the outlet direction of the torque offset outlet 1 is the same as the rotation direction of the main propeller 13.
  • the bottom of the fuselage is provided with a support frame 4, and the lower end of the support frame 4 is provided with a support foot 5.
  • the support frame 4 is provided with a fixed plate, the fixed plate is provided with the main control board 6 and the battery 7 connected with it, and the attitude sensor 11, and the fixed plate is also provided with a camera 8 connected to the output terminal of the motor 9 and the motor 9 Connected to the output terminal of motor two 10, motor one 9 is perpendicular to the axis of motor two 10, motor two 10 is arranged vertically, camera 8 can realize 360° rotation under the drive of motor one 9 and motor two 10; the bottom center of the fixed plate is also set There is a top view camera 12, and the top view camera 12 has a lens vertically downward.
  • the battery 7 is used to supply power to the main drive motor 14, motor one 9, motor two 10, attitude sensor 11 and top view camera 12.
  • the outlet of the power outlet 3 and the torque offset outlet 1 is provided with an adjusting device.
  • Figure 6 takes the power outlet 3 as an example.
  • the adjustment device includes an adjustment plate 17 located at the central axis of the outlet. One end of the adjustment plate 17 is connected to the output end of the adjustment plate 17 driving motor 16 and can swing under the drive of the motor.
  • the adjustment plate 17 drives the motor 16
  • the motor fixing base 15 of the adjusting plate 17 is fixedly connected to the inner wall of the air outlet, the other end of the adjusting plate 17 is connected to a hinge support 18, and the hinge support 18 is fixedly connected to the inner wall of the air outlet.
  • the adjusting plate 17 in the torque offset air outlet 1 is vertically arranged, and the rotation axis of the adjusting plate 17 in the power air outlet 3 intersects at the center line of the apron plate.
  • the power outlet 3 and the torque offset outlet 1 are also provided with an adjusting device to adjust the air outlet direction, so as to adjust the flight direction of the drone.
  • Both the apron board and the drone body are made of aluminum alloy to reduce their own weight as much as possible.
  • the drone flight environment can be observed in real time through the camera 8 above the fixed plate and the top-view camera 12 at the bottom, and equipment such as a package basket can be set on the outside of the support frame 4 to place packages.
  • equipment such as a package basket can be set on the outside of the support frame 4 to place packages.
  • the apron can be set at every other end, and the battery 7 and wireless charging equipment can also be set on the apron.
  • the solar panel 20 continuously charges the battery 7. When the drone is parked on the apron, it can also charge itself through the wireless charging device .

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
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Abstract

本发明公开了一种太阳能浮空停机坪及配套单叶片无人机，包括停机坪和单叶片无人机，停机坪通过浮球浮力悬浮于空中，单叶片无人机仅设置有单个主螺旋桨，动力单元少，与传统的多螺旋桨无人机相比，飞行更加平稳，颠簸和抖动更小。本发明提供一种太阳能浮空停机坪及配套单叶片无人机，停机坪悬浮于空中，不占用地面空间且不需要专人进行看护，无人机运行平稳，保证包裹能安全运输。

Description

一种太阳能浮空停机坪及配套单叶片无人机 技术领域
本发明涉及无人机配送领域，特别是涉及一种太阳能浮空停机坪及配套单叶片无人机。
背景技术
无人机配送，即通过利用无线电遥控设备和自备的程序控制装置操纵的无人驾驶的低空飞行器运载包裹，自动送达目的地，其优点主要在于解决偏远地区的配送问题，提高配送效率，同时减少人力成本。
现有的无人机配送设备基于传统的无人机设计，多是在现有无人机基础上加装用于放置包裹的支架，无人机运行过程中颠簸较大，容易导致包裹翻落，且无人机由包裹集散点运送至目的地距离较长，缺少合适的中转平台，居民集中的住宅区缺少大片空地用于建设无人机中转停机点，且地面停机点需要专人看护，浪费人力。
发明内容
为了解决以上问题，本发明提供一种太阳能浮空停机坪及配套单叶片无人机，停机坪悬浮于空中，不占用地面空间且不需要专人进行看护，无人机运行平稳，保证包裹能安全运输。
为达此目的，本发明提供一种太阳能浮空停机坪及配套单叶片无人机，包括停机坪和单叶片无人机，所述停机坪为中心对称形状的板体，板体中心为停机平台，板体上围绕停机平台一周均 匀设置有太阳能板，板体边缘一周均匀设置有浮球，浮球内充满氦气，停机坪可在浮球浮力作用下漂浮于空中，板体边缘一周还中心对称设置有至少三个水平设置的水平定向电机，其输出端连接有水平驱动螺旋桨，每个水平驱动螺旋桨中轴线均通过板体中心线，板体底部设置有支撑板；所述单叶片无人机包括中空筒状的机身，机身内设置有主驱动电机，主驱动电机输出端为主螺旋桨，机身顶部设置有进气筛板，主螺旋桨转动使机身外部空气由进气筛板进入机身内，机身侧部一周均匀设置有不少于三个出气方向垂直向下的动力出气口，机身侧部一周均匀设置有不少于三个出气方向水平的扭矩抵消出气口，扭矩抵消出气口出气方向与主螺旋桨旋转方向相同，机身底部设置有支撑架，支撑架下端设置有支撑足，支撑架上设置有固定板，固定板上设置有主控板和与其相连的蓄电池、和姿态传感器，固定板上还设置有摄像头，连接于电机一输出端，电机一连接于电机二输出端，电机一与电机二轴线垂直，电机二竖直设置，摄像头在电机一和电机二的带动下可实现360°旋转；所述固定板底部中心还设置有俯视摄像头，俯视摄像头镜头垂直向下，蓄电池用于对主驱动电机、电机一、电机二、姿态传感器和俯视摄像头供电。
本发明的进一步改进，所述动力出气口和扭矩抵消出气口的出口处设置有调节装置，所述调节装置包括位于出气口中轴线处的调节板，调节板一端连接调节板驱动电机输出端，可在电机带动下摆动，调节板驱动电机由调节板电机固定座固定连接于出气 口的内壁，调节板另一端连接铰链支座，铰链支座固定连接于出气口的内壁。
本发明的进一步改进，所述扭矩抵消出气口内调节板竖直设置，所述动力出气口内调节板旋转轴线相交于停机坪板体中心线处。
本发明的进一步改进，所述停机坪板体和无人机机身均采用铝合金材料或者硬质塑料制成。
本申请一种太阳能浮空停机坪及配套单叶片无人机，具有如下特征：
1)本申请包括太阳能浮空停机坪，停机坪在浮球作用小漂浮于控制，其底部可通过拉绳连接地面，不占用地面空间，停机坪具有水平设置的水平驱动螺旋桨，水平驱动螺旋桨转动可保证停机坪在控制位置稳定，停机坪所消耗电能均通过太阳能板提供，清洁环保，能源消耗低；
2)本申请包括单叶片无人机，所述无人机仅设置单独叶片用于进风，通过动力出气口向下方排气实现无人机飞行，由于其动力单元少，与传统的多螺旋桨无人机相比，飞行更加平稳，颠簸和抖动更小，同时设置有扭矩抵消出气口用于抵消主螺旋桨旋转产生的扭矩，防止机身在飞行过程中旋转，同时动力出气口和扭矩抵消出气口还设置有调节装置进行出气风向调节，实现无人机飞行方向的调节。
附图说明
图1为本发明停机坪及配套单叶片无人机示意图；
图2为本发明单叶片无人机示意图；
图3为本发明单叶片无人机局部示意图一；
图4为本发明单叶片无人机局部示意图二；
图5为本发明单叶片无人机局部示意图三；
图6为本发明单叶片无人机方向调节装置示意图；
附图说明：
1、扭矩抵消出气口；2、进气筛板；3、动力出气口；4、支撑架；5、支撑足；6、主控板；7、蓄电池；8、摄像头；9、电机一；10、电机二；11、姿态传感器；12、俯视摄像头；13、主螺旋桨；14、主驱动电机；15、调节板电机固定座；16、调节板驱动电机；17、调节板；18、铰链支座；19、浮球；20、太阳能板；21、停机平台；22、水平定向电机；23、水平驱动螺旋桨；24、支撑板。
具体实施方式
下面结合附图与具体实施方式对本发明作进一步详细描述：
如图1所示的一种太阳能浮空停机坪及配套单叶片无人机，包括停机坪和单叶片无人机。停机坪为正六边形的板体，板体中心为停机平台21，板体上围绕停机平台21一周均匀设置有太阳能板20，板体边缘一周均匀设置有六个浮球19，每个浮球19内充满氦气，停机坪可在浮球19浮力作用下漂浮于空中，板体边缘一周还中心对称设置有三个水平设置的水平定向电机22，其输出 端连接有水平驱动螺旋桨23，每个水平驱动螺旋桨23中轴线均通过板体中心线，板体底部设置有支撑板24。板体可通过拉绳与地面连接，板体在浮球19作用下漂浮于空中，浮球19大于停机坪及无人机携带包裹重量之和。
停机坪具有水平设置的水平驱动螺旋桨23，水平驱动螺旋桨23转动可保证停机坪在控制位置稳定，停机坪所消耗电能均通过太阳能板20提供，清洁环保，能源消耗低。
如图2、3、4和5所示的单叶片无人机包括中空筒状的机身，机身内设置有主驱动电机14，主驱动电机14输出端为主螺旋桨13，机身顶部设置有进气筛板2，主螺旋桨13转动使机身外部空气由进气筛板2进入机身内，机身侧部一周均匀设置有三个出气方向垂直向下的动力出气口3，机身侧部一周均匀设置有三个出气方向水平的扭矩抵消出气口1，扭矩抵消出气口1出气方向与主螺旋桨13旋转方向相同，机身底部设置有支撑架4，支撑架4下端设置有支撑足5，支撑架4上设置有固定板，固定板上设置有主控板6和与其相连的蓄电池7、和姿态传感器11，固定板上还设置有摄像头8，连接于电机一9输出端，电机一9连接于电机二10输出端，电机一9与电机二10轴线垂直，电机二10竖直设置，摄像头8在电机一9和电机二10的带动下可实现360°旋转；固定板底部中心还设置有俯视摄像头12，俯视摄像头12镜头垂直向下，蓄电池7用于对主驱动电机14、电机一9、电机二10、姿态传感器11和俯视摄像头12供电。
动力出气口3和扭矩抵消出气口1的出口处设置有调节装置。图6以动力出气口3为示例，调节装置包括位于出气口中轴线处的调节板17，调节板17一端连接调节板17驱动电机16输出端，可在电机带动下摆动，调节板17驱动电机16由调节板17电机固定座15固定连接于出气口的内壁，调节板17另一端连接铰链支座18，铰链支座18固定连接于出气口的内壁。
扭矩抵消出气口1内调节板17竖直设置，动力出气口3内调节板17旋转轴线相交于停机坪板体中心线处。动力出气口3和扭矩抵消出气口1还设置有调节装置进行出气风向调节，实现无人机飞行方向的调节。
停机坪板体和无人机机身均采用铝合金材料，尽可能减少自身重量。
在实际使用过程中，可通过固定板上方的摄像头8和底部的俯视摄像头12实时观察无人机飞行环境，可在支撑架4外侧设置包裹篮等设备用于放置包裹。停机坪可每隔一端距离设置，停机坪上还可设置蓄电池7与无线充电设备，太阳能板20持续为蓄电池7充电，无人机停在停机坪时，也可通过无线充电设备对自身进行充电。
以上所述，仅是本发明的较佳实施例而已，并非是对本发明作任何其他形式的限制，而依据本发明的技术实质所作的任何修改或等同变化，仍属于本发明所要求保护的范围。

Claims (4)

  1. 一种太阳能浮空停机坪及配套单叶片无人机，其特征在于，包括停机坪和单叶片无人机，所述停机坪为中心对称形状的板体，板体中心为停机平台，板体上围绕停机平台一周均匀设置有太阳能板，板体边缘一周均匀设置有浮球，浮球内充满氦气，停机坪可在浮球浮力作用下漂浮于空中，板体边缘一周还中心对称设置有至少三个水平设置的水平定向电机，其输出端连接有水平驱动螺旋桨，每个水平驱动螺旋桨中轴线均通过板体中心线，板体底部设置有支撑板；所述单叶片无人机包括中空筒状的机身，机身内设置有主驱动电机，主驱动电机输出端为主螺旋桨，机身顶部设置有进气筛板，主螺旋桨转动使机身外部空气由进气筛板进入机身内，机身侧部一周均匀设置有不少于三个出气方向垂直向下的动力出气口，机身侧部一周均匀设置有不少于三个出气方向水平的扭矩抵消出气口，扭矩抵消出气口出气方向与主螺旋桨旋转方向相同，机身底部设置有支撑架，支撑架下端设置有支撑足，支撑架上设置有固定板，固定板上设置有主控板和与其相连的蓄电池、和姿态传感器，固定板上还设置有摄像头，连接于电机一输出端，电机一连接于电机二输出端，电机一与电机二轴线垂直，电机二竖直设置，摄像头在电机一和电机二的带动下可实现360°旋转；所述固定板底部中心还设置有俯视摄像头，俯视摄像头镜头垂直向下，蓄电池用于对主驱动电机、电机一、电机二、姿态传感器和俯视摄像头供电。
  2. 根据权利要求1所述的一种太阳能浮空停机坪及配套单叶片无人 机，其特征在于：所述动力出气口和扭矩抵消出气口的出口处设置有调节装置，所述调节装置包括位于出气口中轴线处的调节板，调节板一端连接调节板驱动电机输出端，可在电机带动下摆动，调节板驱动电机由调节板电机固定座固定连接于出气口的内壁，调节板另一端连接铰链支座，铰链支座固定连接于出气口的内壁。
  3. 根据权利要求2所述的一种太阳能浮空停机坪及配套单叶片无人机，其特征在于：所述扭矩抵消出气口内调节板竖直设置，所述动力出气口内调节板旋转轴线相交于停机坪板体中心线处。
  4. 根据权利要求1-3任一所述的一种太阳能浮空停机坪及配套单叶片无人机，其特征在于：所述停机坪板体和无人机机身均采用铝合金材料或者硬质塑料制成。
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