CN112407310B - Unmanned aerial vehicle with small wind resistance and strong cruising ability and control method thereof - Google Patents
Unmanned aerial vehicle with small wind resistance and strong cruising ability and control method thereof Download PDFInfo
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- CN112407310B CN112407310B CN202011212354.4A CN202011212354A CN112407310B CN 112407310 B CN112407310 B CN 112407310B CN 202011212354 A CN202011212354 A CN 202011212354A CN 112407310 B CN112407310 B CN 112407310B
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- aerial vehicle
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- wind resistance
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- 238000000034 method Methods 0.000 title abstract description 9
- 238000006243 chemical reaction Methods 0.000 claims description 24
- 230000005540 biological transmission Effects 0.000 claims description 22
- 230000007246 mechanism Effects 0.000 claims description 15
- 230000006698 induction Effects 0.000 claims description 7
- 230000017525 heat dissipation Effects 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 claims 1
- 241000883990 Flabellum Species 0.000 abstract description 4
- 230000000694 effects Effects 0.000 abstract description 4
- 230000007547 defect Effects 0.000 abstract description 2
- 230000009286 beneficial effect Effects 0.000 description 1
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Classifications
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- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses an unmanned aerial vehicle with small wind resistance and strong cruising ability and a control method thereof. According to the unmanned aerial vehicle, the four cameras are symmetrically arranged on the periphery of the unmanned aerial vehicle body, and the angles of the cameras can be adjusted through the electric push rod, so that the defect that in the prior art, the wind resistance is large due to the fact that the cameras are arranged at the bottom of the unmanned aerial vehicle body is overcome; through setting up solar cell panel, can effectually turn into the electric energy with solar energy to drive a plurality of flabellum through the motor and rotate, not only can increase unmanned aerial vehicle's duration, also can increase the radiating effect simultaneously.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with small wind resistance and strong cruising ability and a control method thereof.
Background
The unmanned plane is an unmanned plane which is operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and more families use the unmanned plane with the camera shooting function to shoot along with the improvement of living standard.
In the existing unmanned aerial vehicle with the photographing function, a photographing mechanism is usually installed right below the unmanned aerial vehicle, and the photographing mechanism has more mechanisms exposed outside a vehicle body, has larger wind resistance and has certain influence on the flight of the unmanned aerial vehicle; and, current unmanned aerial vehicle is because its self volume is difficult for setting up too big to the battery that leads to its to carry is limited, causes the poor condition of continuation of the journey ability.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle with small wind resistance and strong cruising ability and a control method thereof, which aim to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: an unmanned aerial vehicle with small wind resistance and strong cruising ability and a control method thereof comprise a shooting mechanism and an energy conversion mechanism.
Shoot the mechanism and include unmanned aerial vehicle body, branch, expansion joint, connecting rod and camera, four the same branches of bottom inner wall symmetry fixedly connected with of unmanned aerial vehicle body, four the same expansion joints have been seted up to the outer wall bottom symmetry of unmanned aerial vehicle body, four expansion joint and four one-to-one between the branch, branch is at the one side fixedly connected with connecting rod that is close to corresponding expansion joint with it, the end activity of connecting rod runs through the expansion joint and rotates the one side of connecting at the camera, branch is being close to one side fixedly connected with electric putter of corresponding expansion joint with it, electric putter's the output fixedly connected with body of rod, the end activity of the body of rod runs through the expansion joint and rotates and is connected with the slider, slider sliding connection is in the inside of slide rail, slide rail fixed connection is in one side of camera.
Energy conversion mechanism is including fixed frame, gas vent, induction port, dead lever and transmission shaft, the gas vent has been seted up to one side of fixed frame, the induction port has been seted up to one side of other of fixed frame, two the same dead levers of two of the top inner wall fixedly connected with of induction port, two the bottom of dead lever is rotated and is connected with the transmission shaft, a plurality of the same flabellums have been cup jointed to the right equidistance from a left side on the surface of transmission shaft, the transmission shaft is arranging the inside one end fixedly connected with driven gear of fixed frame in, the driven gear transmission is connected with the driving gear, driving gear fixed connection is at the output of motor, the motor passes through the top of frame fixed connection at the unmanned aerial vehicle body, solar cell panel has been cup jointed on the inner wall top of fixed frame.
Preferably, the top of unmanned aerial vehicle body is being located the inside fixed surface of fixed frame and is being connected with PCB, PCB top is fixedly connected with wireless receiving module, MCU control module, dc-to-ac converter conversion unit and temperature control sensor from a left side to the right side in proper order.
Preferably, the PCB is electrically connected with the wireless receiving module, the MCU control module, the inverter conversion unit and the temperature control sensor, and the MCU control module is electrically connected with the four electric push rods and the motor.
Preferably, the fixing frame is of a hollow circular truncated cone structure.
Preferably, the solar cell panel is electrically connected with the inverter conversion unit, and the inverter conversion unit is electrically connected with the storage battery in the unmanned aerial vehicle body.
Preferably, the motor passes through this internal battery of wire electric connection unmanned aerial vehicle.
Preferably, the exhaust port corresponds to the suction port one by one, and the inner diameters of the exhaust port and the suction port are equal.
Preferably, the unmanned aerial vehicle control method with small wind resistance and strong cruising ability comprises the following steps:
(1) the angle adjustment device comprises a remote controller, a wireless receiving module, an MCU control module, an electric push rod and a camera, wherein the remote controller is used for sending an instruction, the wireless receiving module is used for receiving the instruction and then sending the instruction to the MCU control module, and the MCU control module is used for receiving the instruction and then controlling the electric push rod to act to drive the camera to change the angle under the action of the electric push rod, so that the angle adjustment is completed.
(2) Increase continuation of the journey, after solar cell panel turned into the electric energy with light energy, carry the electric energy to dc-to-ac converter conversion unit department, dc-to-ac converter conversion unit carries to the storage battery of unmanned aerial vehicle body inside after converting the electric energy in, and then accomplishes and charge.
(3) Automatic heat dissipation, after the air temperature in fixed frame reached the appointed temperature of temperature control sensor, temperature control sensor turned into the signal of telecommunication and carried to MCU control module department with thermal signal, MCU control module through calculating the back, control motor work, and the motor passes through the driving gear and drives the transmission shaft with driven gear and rotate, the transmission shaft drives a plurality of driven gear and rotates, and a plurality of pivoted driven gear passes through the induction port with the outside air of fixed frame and carries to the inside of fixed frame, and the inside hot-air of fixed frame passes through the gas vent and discharges to realize automatic heat dissipation.
Compared with the prior art, the invention has the beneficial effects that:
(1) according to the unmanned aerial vehicle, the four cameras are symmetrically arranged on the periphery of the unmanned aerial vehicle body, and the angles of the cameras can be adjusted through the electric push rod, so that the defect that in the prior art, the wind resistance is large due to the fact that the cameras are arranged at the bottom of the unmanned aerial vehicle body is overcome;
(2) through setting up solar cell panel, can effectually turn into the electric energy with solar energy to drive a plurality of flabellum through the motor and rotate, not only can increase unmanned aerial vehicle's duration, also can increase the radiating effect simultaneously.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic front sectional view of the present invention;
FIG. 3 is an enlarged view of a portion of the structure at A in FIG. 2 according to the present invention;
fig. 4 is an enlarged view of a portion of the structure at B in fig. 2 according to the present invention.
In the figure: 1. unmanned aerial vehicle body, 2, branch, 3, the expansion gap, 4, the connecting rod, 5, the camera, 6, electric putter, 7, the body of rod, 8, the slider, 9, the slide rail, 10, fixed frame, 11, the gas vent, 12, the induction port, 13, the dead lever, 14, the transmission shaft, 15, the flabellum, 16, driven gear, 17, the driving gear, 18, the motor, 19, the frame, 20, solar cell panel, 21, PCB, 22, wireless receiving module, 23, MCU control module, 24, inverter conversion unit, 25, the control by temperature change sensor.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, an embodiment of the present invention is shown: an unmanned aerial vehicle with small wind resistance and strong cruising ability and a control method thereof comprise a shooting mechanism and an energy conversion mechanism.
The shooting mechanism comprises an unmanned aerial vehicle body 1, support rods 2, a movable port 3, a connecting rod 4 and a camera 5, wherein four same support rods 2 are symmetrically and fixedly connected to the inner wall of the bottom of the unmanned aerial vehicle body 1, four same movable ports 3 are symmetrically arranged at the bottom end of the outer wall of the unmanned aerial vehicle body 1, the four movable ports 3 correspond to the four support rods 2 one by one, the connecting rod 4 is fixedly connected to one side of each support rod 2 close to the corresponding movable port 3, the tail end of each connecting rod 4 movably penetrates through the corresponding movable port 3 and is rotatably connected to one side of the camera 5, an electric push rod 6 is fixedly connected to one side of each support rod 2 close to the corresponding movable port 3, a rod body 7 is fixedly connected to the output end of each electric push rod 6, the tail end of each rod body 7 movably penetrates through the corresponding movable port 3 and is rotatably connected with a slide block 8, and the slide block 8 is slidably connected to the inside of a slide rail 9, the slide rail 9 is fixedly connected to one side of the camera 5.
The energy conversion mechanism comprises a fixed frame 10, an exhaust port 11, an air suction port 12, a fixed rod 13 and a transmission shaft 14, an exhaust port 11 is opened at one side of the fixing frame 10, an intake port 12 is opened at the other side of the fixing frame 10, two identical fixing rods 13 are fixedly connected to the inner wall of the top of the air suction port 12, the bottom ends of the two fixing rods 13 are rotatably connected with a transmission shaft 14, a plurality of same fan blades 15 are sleeved on the surface of the transmission shaft 14 from left to right at equal intervals, a driven gear 16 is fixedly connected to one end of the transmission shaft 14 arranged in the fixed frame 10, the driven gear 16 is connected with a driving gear 17 in a transmission way, the driving gear 17 is fixedly connected with the output end of a motor 18, the motor 18 passes through frame 19 fixed connection at the top of unmanned aerial vehicle body 1, the inner wall top of fixed frame 10 has cup jointed solar cell panel 20.
The top of unmanned aerial vehicle body 1 is being located the inside fixed surface of fixed frame 10 and is being connected with PCB21, PCB21 top is from a left side to the right fixedly connected with wireless receiving module 22, MCU control module 23, inverter conversion unit 24 and temperature control sensor 25 in proper order.
The PCB21 is electrically connected to the wireless receiving module 22, the MCU control module 23, the inverter conversion unit 24 and the temperature control sensor 25, and the MCU control module 23 is electrically connected to the four electric push rods 6 and the motor 18.
The fixing frame 10 is a hollow round table structure.
The solar cell panel 20 is electrically connected with the inverter conversion unit 24, and the inverter conversion unit 24 is electrically connected with a storage battery in the unmanned aerial vehicle body 1.
The motor 18 is electrically connected with the storage battery in the unmanned aerial vehicle body 1 through a conducting wire.
The exhaust port 11 corresponds to the suction port 12 one by one, and the inner diameters of the exhaust port 11 and the suction port 12 are equal.
A control method of an unmanned aerial vehicle with small wind resistance and strong cruising ability comprises the following steps:
(1) the angle adjustment is performed by sending an instruction through a remote controller, the wireless receiving module 22 sends the instruction to the MCU control module 23 after receiving the instruction, and the MCU control module 23 controls the electric push rod 6 to act after receiving the instruction, and drives the camera 5 to change the angle under the action of the electric push rod 6, so that the angle adjustment is completed.
(2) Increase continuation of the journey, after solar cell panel 20 turned into the electric energy with light energy, carry the electric energy to inverter conversion unit 24 department, inverter conversion unit 24 carries to the storage battery of unmanned aerial vehicle body 1 inside after converting the electric energy in, and then accomplishes and charge.
(3) Automatic heat dissipation, after the air temperature in fixed frame 10 reached the appointed temperature of temperature control sensor 25, temperature control sensor 25 turned into the signal of telecommunication with thermal signal and carried to MCU control module 23 department, and MCU control module 23 is through calculating the back, and control motor 18 work, motor 18 drive transmission shaft 14 rotation through driving gear 17 and driven gear 16, transmission shaft 14 drives a plurality of driven gear 16 and rotates, and a plurality of pivoted driven gear 16 passes through induction port 12 with the outside air of fixed frame 10 and carries to the inside of fixed frame 10, and the inside hot-air of fixed frame 10 passes through exhaust port 11 and discharges to realize automatic heat dissipation.
In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are therefore not to be considered limiting of the invention.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (7)
1. The utility model provides an unmanned aerial vehicle that little duration of wind resistance is strong which characterized in that: comprises a shooting mechanism and an energy conversion mechanism;
the shooting mechanism comprises an unmanned aerial vehicle body (1), four same supporting rods (2), a movable opening (3), a connecting rod (4) and a camera (5), wherein the bottom inner wall of the unmanned aerial vehicle body (1) is symmetrically and fixedly connected with the four same supporting rods (2), the bottom end of the outer wall of the unmanned aerial vehicle body (1) is symmetrically provided with the four same movable openings (3), the four movable openings (3) correspond to the four supporting rods (2) one by one, the connecting rod (4) is fixedly connected to one side of each supporting rod (2) close to the corresponding movable opening (3), the tail end of each connecting rod (4) movably penetrates through the corresponding movable opening (3) and is rotatably connected to one side of the camera (5), one side of each supporting rod (2) close to the corresponding movable opening (3) is fixedly connected with an electric push rod (6), and the output end of each electric push rod (6) is fixedly connected with a rod body (7), the tail end of the rod body (7) movably penetrates through the movable opening (3) and is rotatably connected with a sliding block (8), the sliding block (8) is connected inside a sliding rail (9) in a sliding mode, and the sliding rail (9) is fixedly connected to one side of the camera (5);
the energy conversion mechanism comprises a fixed frame (10), an exhaust port (11), an air suction port (12), fixing rods (13) and a transmission shaft (14), wherein the exhaust port (11) is formed in one side of the fixed frame (10), the air suction port (12) is formed in the other side of the fixed frame (10), two same fixing rods (13) are fixedly connected to the inner wall of the top of the air suction port (12), the transmission shaft (14) is connected to the bottom end of the two fixing rods (13) in a rotating mode, a plurality of same fan blades (15) are sleeved on the surface of the transmission shaft (14) from left to right at equal intervals, a driven gear (16) is fixedly connected to one end of the transmission shaft (14) inside the fixed frame (10), a driving gear (17) is connected to the driven gear (16) in a transmission mode, the driving gear (17) is fixedly connected to the output end of a motor (18), and the motor (18) is fixedly connected to the top of an unmanned aerial vehicle body (1) through a rack (19), the top end of the inner wall of the fixing frame (10) is sleeved with a solar panel (20);
(1) the angle is adjusted, an instruction is sent out through a remote controller, the wireless receiving module (22) sends the instruction to the MCU control module (23) after receiving the instruction, the MCU control module (23) controls the electric push rod (6) to act after receiving the instruction, and the camera (5) is driven to change the angle under the action of the electric push rod (6), so that the angle adjustment is completed;
(2) increasing endurance, namely after the solar panel (20) converts light energy into electric energy, transmitting the electric energy to an inverter conversion unit (24), converting the electric energy by the inverter conversion unit (24), and transmitting the electric energy into a storage battery in the unmanned aerial vehicle body (1) so as to complete charging;
(3) automatic heat dissipation, after the air temperature in fixed frame (10) reached the appointed temperature of control by temperature change sensor (25), control by temperature change sensor (25) turned into the signal of telecommunication with heating power signal and carried to MCU control module (23) department, MCU control module (23) are through calculating the back, control motor (18) work, and motor (18) drive transmission shaft (14) through driving gear (17) and driven gear (16) and rotate, transmission shaft (14) drive a plurality of driven gear (16) and rotate, and a plurality of pivoted driven gear (16) carry the inside of fixed frame (10) through induction port (12) with fixed frame (10) outside air, and the inside hot-air of fixed frame (10) passes through gas vent (11) and discharges to realize automatic heat dissipation.
2. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle has a low wind resistance and a high cruising ability, and comprises: the top of unmanned aerial vehicle body (1) is being located fixed frame (10) inside fixed surface be connected with PCB (21), PCB (21) top is fixedly connected with wireless receiving module (22), MCU control module (23), dc-to-ac converter converting unit (24) and control by temperature change sensor (25) from a left side to the right side in proper order.
3. The unmanned aerial vehicle of claim 2, wherein the unmanned aerial vehicle has a low wind resistance and a high cruising ability, and the unmanned aerial vehicle comprises: the PCB (21) is electrically connected with the wireless receiving module (22), the MCU control module (23), the inverter conversion unit (24) and the temperature control sensor (25), and the MCU control module (23) is electrically connected with the four electric push rods (6) and the motor (18).
4. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle has a low wind resistance and a high cruising ability, and comprises: the fixing frame (10) is of a hollow round table body structure.
5. The unmanned aerial vehicle of claim 2, wherein the unmanned aerial vehicle has a low wind resistance and a high cruising ability, and the unmanned aerial vehicle comprises: the solar cell panel (20) is electrically connected with the inverter conversion unit (24), and the inverter conversion unit (24) is electrically connected with the storage battery in the unmanned aerial vehicle body (1).
6. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle has a low wind resistance and a high cruising ability, and comprises: the motor (18) is electrically connected with a storage battery in the unmanned aerial vehicle body (1) through a lead.
7. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle has a low wind resistance and a high cruising ability, and comprises: the exhaust port (11) and the air suction port (12) are in one-to-one correspondence, and the inner diameters of the exhaust port (11) and the air suction port (12) are equal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011212354.4A CN112407310B (en) | 2020-11-03 | 2020-11-03 | Unmanned aerial vehicle with small wind resistance and strong cruising ability and control method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN202011212354.4A CN112407310B (en) | 2020-11-03 | 2020-11-03 | Unmanned aerial vehicle with small wind resistance and strong cruising ability and control method thereof |
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| Publication Number | Publication Date |
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| CN112407310A CN112407310A (en) | 2021-02-26 |
| CN112407310B true CN112407310B (en) | 2022-05-20 |
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| CN202011212354.4A Active CN112407310B (en) | 2020-11-03 | 2020-11-03 | Unmanned aerial vehicle with small wind resistance and strong cruising ability and control method thereof |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204368434U (en) * | 2015-01-04 | 2015-06-03 | 金陵科技学院 | A kind of unmanned plane of band Dual Action camera of upper laying solar panel |
| CN108263605A (en) * | 2018-01-31 | 2018-07-10 | 芜湖市海联机械设备有限公司 | A kind of high continuation of the journey multi-rotor unmanned aerial vehicle |
| CN208198816U (en) * | 2018-04-11 | 2018-12-07 | 刘岩 | A kind of unmanned plane with high altitude operation |
| CN110892612A (en) * | 2017-09-20 | 2020-03-17 | 信浓绢糸株式会社 | All-weather motor |
| CN210191839U (en) * | 2019-04-03 | 2020-03-27 | 薛宇涵 | Unmanned aerial vehicle device of taking photo by plane based on many cameras |
| CN211519835U (en) * | 2019-12-24 | 2020-09-18 | 企威(苏州)文化科技有限公司 | Aircraft detection equipment with high cruising ability |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275400A (en) * | 2016-08-29 | 2017-01-04 | 尚华军 | A kind of hybrid unmanned plane |
| CN108513740B (en) * | 2017-02-24 | 2020-04-07 | 深圳市大疆创新科技有限公司 | Frame and unmanned vehicles |
| CN107963209B (en) * | 2017-11-17 | 2020-03-20 | 沈阳无距科技有限公司 | Tandem wing rotor unmanned aerial vehicle that verts |
| CN208429235U (en) * | 2018-07-12 | 2019-01-25 | 中国人民解放军战略支援部队信息工程大学 | It is a kind of can VTOL and long continuation of the journey unmanned plane |
-
2020
- 2020-11-03 CN CN202011212354.4A patent/CN112407310B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204368434U (en) * | 2015-01-04 | 2015-06-03 | 金陵科技学院 | A kind of unmanned plane of band Dual Action camera of upper laying solar panel |
| CN110892612A (en) * | 2017-09-20 | 2020-03-17 | 信浓绢糸株式会社 | All-weather motor |
| CN108263605A (en) * | 2018-01-31 | 2018-07-10 | 芜湖市海联机械设备有限公司 | A kind of high continuation of the journey multi-rotor unmanned aerial vehicle |
| CN208198816U (en) * | 2018-04-11 | 2018-12-07 | 刘岩 | A kind of unmanned plane with high altitude operation |
| CN210191839U (en) * | 2019-04-03 | 2020-03-27 | 薛宇涵 | Unmanned aerial vehicle device of taking photo by plane based on many cameras |
| CN211519835U (en) * | 2019-12-24 | 2020-09-18 | 企威(苏州)文化科技有限公司 | Aircraft detection equipment with high cruising ability |
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| CN112407310A (en) | 2021-02-26 |
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