CN110217373A - A kind of solar energy floating airplane parking area and mating single blade unmanned plane - Google Patents

Abstract

A kind of solar energy floating airplane parking area and mating single blade unmanned plane; including airplane parking area and single blade unmanned plane; airplane parking area is suspended in the air by floating buoyancy; single blade unmanned plane is provided only with single main screw; power unit is few; compared with traditional multiple propeller unmanned plane, flies more steady, jolt and shake smaller.The present invention provides a kind of solar energy floating airplane parking area and mating single blade unmanned plane, airplane parking area and is suspended in the air, is not take up ground space and does not need special messenger and nurses, and unmanned plane runs smoothly, and guarantees that package can transport safely.

Description

A solar-powered floating apron and supporting single-blade UAV

technical field

The invention relates to the field of unmanned aerial vehicle distribution, in particular to a solar-powered floating apron and a supporting single-blade unmanned aerial vehicle.

Background technique

Unmanned aerial vehicle distribution, that is, the unmanned low-altitude aircraft operated by radio remote control equipment and its own program control device is used to carry packages and automatically deliver them to the destination. Its advantages mainly lie in solving the distribution problems in remote areas and improving distribution efficiency. At the same time reduce labor costs.

The existing UAV distribution equipment is based on the traditional UAV design, and most of them are based on the existing UAV. The bracket for placing the package is added. The UAV is bumpy during the operation process, which may easily cause the package to fall. , and the UAV is transported from the parcel distribution point to the destination for a long distance, lacks a suitable transfer platform, and the residential area with concentrated residents lacks a large area of open space for the construction of the UAV transfer stop point, and the ground stop point needs special care, which is wasteful. manpower.

Contents of the invention

In order to solve the above problems, the present invention provides a solar floating apron and a supporting single-blade UAV. The apron is suspended in the air, does not occupy the ground space and does not require special personnel to take care of it. The UAV runs smoothly and ensures the safety of parcels. transportation.

In order to achieve this purpose, the present invention provides a solar floating apron and a supporting single-blade UAV, including the apron and the single-blade UAV. On the platform, solar panels are evenly arranged around the parking platform on the board body, and floating balls are evenly arranged around the edge of the board body, and the floating balls are filled with helium. The center is symmetrically provided with at least three horizontally oriented motors arranged horizontally, the output end of which is connected to a horizontally driven propeller, the central axis of each horizontally driven propeller passes through the centerline of the plate body, and a support plate is provided at the bottom of the plate body; the single blade has no The man-machine consists of a hollow cylindrical fuselage. The main drive motor is arranged inside the fuselage. The output end of the main drive motor is the main propeller. The top of the fuselage is provided with an air intake sieve plate. The board enters the fuselage, and the side of the fuselage is evenly provided with no less than three power outlets with air outlet directions vertically downward, and the side of the fuselage is evenly provided with no less than three horizontal torque offset outlets with air outlet directions. , the torque counteracts the air outlet direction to be 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 a support foot, the support frame is provided with a fixed plate, and the fixed plate is provided with a main control board and connected to it Storage battery, and attitude sensor, also be provided with camera on the fixed plate, be connected to motor one output end, motor one is connected to motor two output ends, motor one and motor two axis vertical, motor two vertical setting, camera is connected between motor one and motor two. Can realize 360 ° rotation under the drive of two; Described fixed plate bottom center is also provided with overlooking camera, and overlooking camera lens vertically downwards, battery is used for main drive motor, motor one, motor two, attitude sensor and overlooking camera power supply.

As a further improvement of the present invention, an adjustment device is provided at the outlet of the power air outlet and the torque offset air outlet, and the adjustment device includes an adjustment plate located at the central axis of the air outlet, and one end of the adjustment plate is connected to the output end of the drive motor of the adjustment plate, which can Driven by the motor to swing, the adjusting plate drive motor is fixedly connected to the inner wall of the air outlet by the adjusting plate motor fixing seat, and 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.

As a further improvement of the present invention, the adjustment plate in the torque offset air outlet is arranged vertically, and the rotation axis of the adjustment plate in the power air outlet intersects at the center line of the apron body.

As a further improvement of the present invention, both the apron board body and the UAV fuselage are made of aluminum alloy or hard plastic.

This application is a solar floating parking pad and supporting single-blade unmanned aerial vehicle, which has the following characteristics:

1) This application includes a solar floating apron. The apron is controlled by floating balls. The bottom of the apron can be connected to the ground by a pull rope, which does not occupy the ground space. The apron has a horizontal drive propeller that is set horizontally, and the horizontal drive propeller rotates It can ensure that the apron is stable at the control position, and the power consumed by the apron is provided by solar panels, which is clean and environmentally friendly, and has low energy consumption;

2) This application includes a single-blade drone, which only has a single blade for air intake, and the drone is exhausted downward through the power outlet to realize the flight of the drone. Due to its small power unit, it is different from the traditional multi-propeller Compared with drones, the flight is more stable, with less bumps and jitters. At the same time, a torque offset air outlet is set to offset the torque generated by the rotation of the main propeller, preventing the fuselage from rotating during flight. At the same time, the power air outlet and the torque offset outlet The air port is also equipped with an adjustment device to adjust the direction of the air outlet, so as to realize the adjustment of the flight direction of the drone.

Description of drawings

Fig. 1 is the schematic diagram of apron of the present invention and supporting single-blade unmanned aerial vehicle;

Fig. 2 is a schematic diagram of a single-blade unmanned aerial vehicle of the present invention;

Fig. 3 is a partial schematic diagram 1 of the single-blade UAV of the present invention;

Fig. 4 is a partial schematic diagram II of the single-blade UAV of the present invention;

Fig. 5 is a partial schematic diagram three of the single-blade UAV of the present invention;

Fig. 6 is a schematic diagram of a single-blade UAV direction adjustment device of the present invention;

Description of drawings:

1. Torque offset air outlet; 2. Intake sieve plate; 3. Power outlet; 4. Support frame; 5. Support foot; 6. Main control board; 7. Battery; 8. Camera; 9. Motor one; 10 1. Motor two; 11. Attitude sensor; 12. Overlooking camera; 13. Main propeller; 14. Main driving motor; 15. Adjusting plate motor fixing seat; 16. Adjusting plate driving motor; ; 19, floating ball; 20, solar panel; 21, parking platform; 22, horizontal orientation motor; 23, horizontal drive propeller; 24, support plate.

Detailed ways

Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

As shown in Figure 1, a solar floating apron and a supporting single-blade UAV include the apron and the single-blade UAV. The apron is a regular hexagonal plate, the center of the plate is the parking platform 21, the solar panel 20 is evenly arranged around the parking platform 21 on the plate body, and six floating balls 19 are evenly arranged around the edge of the plate body. 19 is filled with helium, and the apron can float in the air under the buoyancy of the buoyancy ball 19. The edge of the board body is also center-symmetrically arranged with three horizontally arranged horizontally oriented motors 22, and its output end is connected with a horizontally driven propeller 23, each The central axes of the horizontally driven propellers 23 all pass through the centerline of the plate body, and a support plate 24 is arranged at the bottom of the plate body. The board body can be connected with the ground by a stay rope, and the board body floats in the air under the action of the floating ball 19, which is greater than the sum of the weight of the apron and the package carried by the drone.

The apron has a horizontally driven propeller 23 arranged horizontally, and the rotation of the horizontally driven propeller 23 can ensure that the apron is stable at the control position. The power consumed by the apron is provided by the solar panel 20, which is clean and environmentally friendly, and has low energy consumption.

The single-blade unmanned aerial vehicle shown in Figure 2, 3, 4 and 5 comprises the fuselage of hollow tube shape, is provided with main drive motor 14 in the fuselage, and main propeller 13 is arranged at the output end of main drive motor 14, and fuselage top is provided with There is an air intake sieve plate 2, and the main propeller 13 rotates so that the air outside the fuselage enters the fuselage through the air intake sieve plate 2. Three power outlets 3 with air outlet directions vertically downward are evenly arranged on the side of the fuselage. Three horizontal torque offset air outlets 1 in the direction of air outlet are evenly arranged around the head. The air outlet direction of the torque offset air outlet 1 is the same as the rotation direction of the main propeller 13. A support frame 4 is provided at the bottom of the fuselage, and a support foot 5 is provided at the lower end of the support frame 4. The support frame 4 is provided with a fixed plate, the fixed plate is provided with a main control board 6 and a storage battery 7 connected thereto, and an attitude sensor 11, and a camera 8 is also arranged on the fixed plate, which is connected to the output terminal of the motor one 9, and the motor one 9 Connected to the output end of motor two 10, motor one 9 is perpendicular to the axis of motor two 10, motor two 10 is vertically arranged, camera 8 can realize 360 ° rotation under the drive of motor one 9 and motor two 10; the center of the bottom of the fixed plate is also set There is a bird's eye view camera 12, and the bird's eye view camera 12 lenses are vertically downward, and the storage battery 7 is used to supply power to the main drive motor 14, motor one 9, motor two 10, attitude sensor 11 and bird's eye view camera 12.

Adjusting devices are provided at the outlets of the power air outlet 3 and the torque offset air outlet 1 . Figure 6 takes the power air outlet 3 as an example, the adjustment device includes an adjustment plate 17 located at the central axis of the air outlet, one end of the adjustment plate 17 is connected to the output end of the adjustment plate 17 to drive the motor 16, and can swing under the drive of the motor, and the adjustment plate 17 drives the motor 16 The motor fixing seat 15 of the adjusting plate 17 is fixedly connected to the inner wall of the air outlet, and the other end of the adjusting plate 17 is connected to the hinge support 18, and the hinge support 18 is fixedly connected to the inner wall of the air outlet.

The adjustment plate 17 in the torque offset air outlet 1 is vertically arranged, and the rotation axis of the adjustment plate 17 in the power air outlet 3 intersects at the center line of the apron body. The power air outlet 3 and the torque offset air outlet 1 are also provided with adjustment devices to adjust the air outlet direction, so as to realize the adjustment of the flight direction of the drone.

Both the apron board body and the UAV fuselage are made of aluminum alloy to reduce its own weight as much as possible.

In actual use, 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 outside the support frame 4 for placing packages. The apron can be set at every other distance, and the battery 7 and wireless charging equipment can also be installed on the apron. The solar panel 20 can continuously charge the battery 7. When the drone is parked on the apron, it can also charge itself through the wireless charging equipment. .

The above is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any other form, and any modification or equivalent change made according to the technical essence of the present invention still belongs to the scope of protection required by the present invention .

Claims (4)

1. a kind of solar energy floating airplane parking area and mating single blade unmanned plane, which is characterized in that including airplane parking area and single blade without Man-machine, the airplane parking area is the plate body of center symmetric shape, and plate body center is to shut down platform, around shutdown platform one week on plate body Solar panels are evenly arranged with, plate body edge is evenly arranged with floating ball for one week, and helium is full of in floating ball, and airplane parking area can be floating in floating ball It is floated under power effect in the air, the one week also center symmetric setting in plate body edge has at least three horizontally disposed horizontal orientations electricity Machine, output end are connected with horizontal drive propeller, and each horizontal drive propeller central axes pass through plate body center line, plate body Bottom is provided with support plate；The single blade unmanned plane includes the fuselage of hollow tube-shape, and main drive motor is provided in fuselage, main Driving motor output end is main screw, and fuselage roof is provided with air inlet sieve plate, main screw rotation make external fuselage air by Air inlet sieve plate enters in fuselage, is evenly arranged within side-of-body one week the power outlet of no less than three outgassing directions vertically downward Mouthful, the torque for being evenly arranged with no less than three outgassing direction levels for side-of-body one week offsets gas outlet, and torque offsets outlet Mouth outgassing direction is identical as main screw direction of rotation, and fuselage bottom is provided with support frame, and support frame lower end is provided with support foot, It is provided with fixed plate on support frame, master control borad and coupled battery and attitude transducer are provided in fixed plate, it is fixed It is additionally provided with camera on plate, is connected to one output end of motor, motor one is connected to two output end of motor, motor one and motor two Axis is vertical, and motor two is vertically arranged, and 360 ° of rotations can be achieved in camera under the drive of motor one and motor two；The fixation Plate bottom centre is additionally provided with vertical view camera, overlooks cam lens vertically downward, and battery is used for main drive motor, electricity Machine one, motor two, attitude transducer and vertical view camera power supply.

2. a kind of solar energy floating airplane parking area according to claim 1 and mating single blade unmanned plane, it is characterised in that: institute The exit for stating power gas outlet and torque counteracting gas outlet is provided with regulating device, and the regulating device includes being located at gas outlet Adjustable plate at central axes, adjustable plate one end connect adjustable plate driving motor output end, can drive lower swing, adjustable plate in motor Driving motor is fixedly connected on the inner wall of gas outlet, adjustable plate other end connects hinge support, hinge by adjustable plate motor fixing seat Chain support is fixedly connected on the inner wall of gas outlet.

3. a kind of solar energy floating airplane parking area according to claim 2 and mating single blade unmanned plane, it is characterised in that: institute It states adjustable plate in torque counteracting gas outlet to be vertically arranged, adjustable plate jante et perpendiculaire is in airplane parking area plate in the power gas outlet Body centerline.

4. a kind of solar energy floating airplane parking area according to claim 1 to 3 and mating single blade unmanned plane, feature It is: the airplane parking area plate body and unmanned aerial vehicle body is all made of aluminum alloy materials or rigid plastics is made.