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 PDFInfo
- 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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- WO
- WIPO (PCT)
- Prior art keywords
- motor
- apron
- fuselage
- blade
- plate
- Prior art date
Links
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000001307 helium Substances 0.000 claims description 3
- 229910052734 helium Inorganic materials 0.000 claims description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 6
- 230000006872 improvement Effects 0.000 description 3
- 238000005265 energy consumption Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Images
Classifications
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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
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- 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)
- Toys (AREA)
- Photovoltaic Devices (AREA)
Abstract
Description
Claims (4)
- 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。
- 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。
- 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。
- 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。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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CN201910537047.4 | 2019-06-20 | ||
CN201910537047.4A CN110217373A (zh) | 2019-06-20 | 2019-06-20 | 一种太阳能浮空停机坪及配套单叶片无人机 |
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WO2020253614A1 true WO2020253614A1 (zh) | 2020-12-24 |
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PCT/CN2020/095624 WO2020253614A1 (zh) | 2019-06-20 | 2020-06-11 | 一种太阳能浮空停机坪及配套单叶片无人机 |
Country Status (3)
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CN (1) | CN110217373A (zh) |
BE (1) | BE1027331B1 (zh) |
WO (1) | WO2020253614A1 (zh) |
Cited By (2)
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CN114847064A (zh) * | 2022-05-26 | 2022-08-05 | 安徽科技学院 | 一种夜蛾黑卵蜂田间放蜂定位系统 |
WO2024056195A1 (en) * | 2022-09-16 | 2024-03-21 | Kji Dronelab Bv | Propulsion system for multicopters and related aircrafts |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102018116169B4 (de) * | 2018-07-04 | 2022-02-24 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Luftfahrzeug |
CN110217373A (zh) * | 2019-06-20 | 2019-09-10 | 金陵科技学院 | 一种太阳能浮空停机坪及配套单叶片无人机 |
CN114919741B (zh) * | 2022-05-17 | 2024-03-12 | 西安电子科技大学 | 一种可倾转四旋翼浮空器组阵 |
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- 2019-06-20 CN CN201910537047.4A patent/CN110217373A/zh active Pending
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2020
- 2020-06-11 WO PCT/CN2020/095624 patent/WO2020253614A1/zh active Application Filing
- 2020-06-18 BE BE20205444A patent/BE1027331B1/de active IP Right Grant
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CN110217373A (zh) | 2019-09-10 |
BE1027331A1 (de) | 2021-01-06 |
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