CN110949668A - Unmanned aerial vehicle with folding crashproof support function and monitored control system thereof - Google Patents
Unmanned aerial vehicle with folding crashproof support function and monitored control system thereof Download PDFInfo
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- CN110949668A CN110949668A CN201911301555.9A CN201911301555A CN110949668A CN 110949668 A CN110949668 A CN 110949668A CN 201911301555 A CN201911301555 A CN 201911301555A CN 110949668 A CN110949668 A CN 110949668A
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- unmanned aerial
- aerial vehicle
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K1/00—Details of thermometers not specially adapted for particular types of thermometer
- G01K1/14—Supports; Fastening devices; Arrangements for mounting thermometers in particular locations
- G01K1/146—Supports; Fastening devices; Arrangements for mounting thermometers in particular locations arrangements for moving thermometers to or from a measuring position
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
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- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention is suitable for the technical field of unmanned aerial vehicles, and provides an unmanned aerial vehicle with a function of a folding anti-collision support and a monitoring system thereof, wherein the unmanned aerial vehicle comprises a main body, wings, a power part and hinges, the power part is fixedly connected to the main body, the wings are fixed on the outer wall of the main body, and the hinges are fixedly connected to the outer wall of the wings; in the in-process that uses, unmanned aerial vehicle is when carrying out the measuring of temperature data, carry out the transmission of instruction to control module through controlling the module, control module sends control command to the cylinder afterwards and makes it begin to work, make the telescopic shaft of cylinder begin to lengthen, because temperature sensor is located the telescopic shaft of cylinder, and then temperature sensor just can be along with the stretching of cylinder telescopic shaft and then the change and the removal of position, thereby make temperature sensor keep away from the main part, avoid the heat that the main part gived off to influence the measuring of temperature sensor to temperature data, and then just can be abundant assurance temperature data acquisition's accuracy.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle with a function of folding an anti-collision support and a monitoring system thereof.
Background
Unmanned aircraft, also known as "drones," are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, or are operated autonomously, either completely or intermittently, by an onboard computer, and are often more suited to tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
At present, the unmanned aerial vehicle is used for collecting data mostly, and the temperature sensor is directly installed on the unmanned aerial vehicle, and the unmanned aerial vehicle can emit a large amount of heat at the in-process self of flying, and then the data acquisition of the temperature sensor can be influenced, and the temperature difference is indirectly increased.
Disclosure of Invention
The invention provides an unmanned aerial vehicle with a function of a folding anti-collision support and a monitoring system thereof, and aims to solve the problems that the unmanned aerial vehicle can emit a large amount of heat in the flying process, so that the data acquisition of a temperature sensor is influenced, and the temperature difference is indirectly increased.
The invention provides an unmanned aerial vehicle with a function of a folding anti-collision support, which comprises a main body, wings, a power part and hinges, wherein the power part is fixedly connected to the main body, the wings are fixed on the outer wall of the main body, the hinges are fixedly connected to the outer wall of the wings, inserting rods are accommodated in the wings, and the inserting rods penetrate through the wings and are inserted into the wings.
Preferably, the power portion comprises motor and rotor, the output transmission of motor connect in the rotor, just motor and built-in power supply electric connection.
Preferably, the motor further comprises a support frame, and two ends of the support frame are respectively and fixedly connected to the outer walls of the main body and the motor.
Preferably, the wings are arranged in a four-section mode, and each section of the wings are hinged through the hinges.
Preferably, holes along the length direction of the wing are formed in each section of the wing, the holes correspond to each other, and the inserted bar penetrates through the wing through the holes.
The utility model provides an unmanned aerial vehicle monitored control system with folding crashproof support function, includes detection module, shoots the module, controls module and control module, control module with control module is connected for control command's sending and execution, detection module with shoot the module all with control module wireless connection for the data that will detect and the video data who shoots are sent to control module inside, detection module includes temperature sensor and cylinder, temperature sensor is fixed in on the telescopic shaft of cylinder, just the cylinder with control module is connected for control command's execution.
Preferably, the cylinder is fixed in the bottom of the main body, a sleeve body with an opening at the bottom is arranged on a telescopic shaft of the detection module, and the temperature sensor is fixed in the sleeve body.
Preferably, the device further comprises a transmission module and a wireless module, wherein the transmission module is connected with the control module through the wireless module, and the detection module and the shooting module are connected with the transmission module and used for wirelessly transmitting the video and temperature data acquired by the detection module and the shooting module to the inside of the control module.
Preferably, the device comprises a power module, wherein the power module is connected with the detection module, the shooting module, the transmission module, the wireless module and the control module and used for supplying power.
Preferably, the shooting module is a camera and is fixed at the bottom of the main body.
Compared with the prior art, the invention has the beneficial effects that: according to the unmanned aerial vehicle with the function of the folding anti-collision support and the monitoring system thereof, the temperature sensor, the cylinder, the control module and the control module are arranged, in the using process, when the unmanned aerial vehicle detects temperature data, the control module sends instructions to the control module, then the control module sends control instructions to the cylinder to enable the cylinder to start working, the telescopic shaft of the cylinder starts to be elongated, the temperature sensor is located on the telescopic shaft of the cylinder, and the temperature sensor can change and move along with the stretching of the telescopic shaft of the cylinder, so that the temperature sensor is far away from the main body, the heat emitted by the main body is prevented from influencing the detection of the temperature sensor on the temperature data, and the accuracy of temperature data acquisition can be fully ensured.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle according to the present invention;
FIG. 2 is a schematic view of a wing structure according to the present invention;
FIG. 3 is a schematic structural view of the present invention;
in the figure: 11. a main body; 12. an airfoil; 13. a support frame; 14. a motor; 15. a rotor; 16. a hinge; 17. inserting a rod; 21. a detection module; 211. a temperature sensor; 212. a cylinder; 22. a shooting module; 23. a transmission module; 24. a wireless module; 25. a control module; 26. a control module; 27. and a power supply module.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
The first embodiment is as follows: referring to fig. 1-2, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle with folding crashproof support function, includes main part 11, wing 12, power portion and hinge 16, power portion fixed connection in main part 11, and wing 12 is fixed in the outer wall of main part 11, and hinge 16 fixed connection in the outer wall of wing 12, and inserted bar 17 has been acceptd to the inside of wing 12, and inserted bar 17 runs through wing 12, and the plug-in connects in wing 12.
In the embodiment, when the unmanned aerial vehicle is not in use, a user can pull out the insertion rod 17 inside the wing 12, due to the four-section arrangement of the wing 12, when the user pulls out the insertion rod 17 from the inside of the wing 12, the wing 12 loses connection and support, and under the action of the hinge 16, the user can fold each two sections of wings 12, so that the wing 12 can be folded in a folding manner when the unmanned aerial vehicle is boxed and transported, and the boxing and transportation of the unmanned aerial vehicle are more convenient, when the unmanned aerial vehicle is in use, the user can insert the insertion rod 17 into the hole inside the wing 12, the shape of the wing 12 is fixed through the insertion rod 17, the folding condition of the wing 12 in use is avoided, then, the motor 14 starts to work, the rotor 15 is driven by the motor 14 to rotate, and the four rotors 15 synchronously rotate, the main body 11 is lifted, so that the flight of the unmanned aerial vehicle can be realized, and the length of the wing 12 is smaller than that of the support frame 13, so that the phenomenon that the wing 12 collides in the flight process of the unmanned aerial vehicle can be avoided.
Further, the power portion comprises motor 14 and rotor 15, and the output transmission of motor 14 is connected in rotor 15, and motor 14 and built-in power electrical connection.
In this embodiment, at the in-process that uses, when unmanned aerial vehicle is flying, motor 14 begins work, drives rotor 15 through motor 14 and rotates, and four rotors 15 rotate in step, carry out the lifting to main part 11, and then alright realize unmanned aerial vehicle's flight.
Further, the electric vehicle further comprises a support frame 13, and two ends of the support frame 13 are respectively and fixedly connected to the outer walls of the main body 11 and the motor 14.
In this embodiment, in the use process, the support frame 13 plays a linked role, and then under the effect of the support frame 13, the motor 14 and the rotor 15 can be smoothly fixed on the main body 11, and then the main body 11 can be smoothly driven to lift through the rotation of the rotor 15.
Further, the wings 12 are arranged in four sections, and each section of wing 12 is hinged through a hinge 16.
In this embodiment, due to the four-segment arrangement of the wings 12, when the user pulls out the insertion rod 17 from the inside of the wings 12, the wings 12 lose connection and support, and under the action of the hinges 16, the user can fold each two segments of wings 12 with each other, thereby reducing the space occupation of the wings 12.
Furthermore, holes along the length direction of each section of wing 12 are formed in the inner part of each section of wing 12, the holes correspond to each other, and the inserted rod 17 penetrates through the wing 12 through the holes.
In the embodiment, during the use process, a user can insert the insertion rod 17 into the hole inside the wing 12, and the shape of the wing 12 is fixed through the insertion rod 17, so that the wing 12 is prevented from being folded during the use process.
Example two: referring to fig. 3, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle monitored control system with folding crashproof support function, including detection module 21, shoot module 22, control module 25 and control module 26, control module 25 is connected with control module 26, a sending and execution for control command, detection module 21 and shooting module 22 all with control module 25 wireless connection, a video data send to control module 25 inside with the data that detect and shoot, detection module 21 includes temperature sensor 211 and cylinder 212, temperature sensor 211 is fixed in on the telescopic shaft of cylinder 212, and cylinder 212 is connected with control module 26, an execution for control command is in this embodiment.
In the embodiment, in the using process, when a user needs to monitor the temperature in a certain area, the control module 25 can send a start control instruction to the inside of the control module 26, the control module 25 can be a base station, an unmanned aerial vehicle remote controller and the like, the control module 26 sends the start control instruction to the motor 14, then the motor 14 is connected with the internal power module 27, the motor 14 works to drive the rotor 15 on the output shaft to rotate, and the unmanned aerial vehicle can fly under the rotation of the rotor 15, when the unmanned aerial vehicle flies, because the shooting module 22 is arranged at the bottom of the main body 11, the shooting module 22 is a camera, and the route of the unmanned aerial vehicle when flying can be shot through the camera and sent to the inside of the transmission module 23, because the transmission module 23 is connected with the control module 25 through the wireless module 24, then under the effect of the wireless module 24, the video image data received by the transmission module 23 can be sent to the inside of the control module 25 and displayed by the display in the control module 25 for the user to watch, when the unmanned aerial vehicle flies to the area of the temperature to be detected, the control module 25 controls the unmanned aerial vehicle to fly in place through the control module 26 and sends a control instruction to the cylinder 212, so that the telescopic shaft of the cylinder 212 starts to elongate, since the temperature sensor 211 is located on the telescopic shaft of the cylinder 212, the temperature sensor 211 can change and move along with the stretching of the telescopic shaft of the cylinder 212, so that the temperature sensor 211 is far away from the main body 11, the heat emitted by the main body 11 is prevented from influencing the detection of the temperature sensor 211 on the temperature data, and the accuracy of temperature data acquisition can be fully ensured, subsequently, the temperature sensor 211 can send the acquired data to the inside of the transmission module 23, and send the acquired temperature data to the inside of the control module 25 through the wireless module 24, and the temperature data is watched and recorded by a user, after the temperature data is acquired, the control module 26 controls the cylinder 212 again to drive the temperature sensor 211 to reset, the control module 26 and the power module 27 are installed inside the main body 11, the control module 26 is a controller of model STM32F103T8U6, and the model of the temperature sensor 211 is pt 100.
Further, the cylinder 212 is fixed at the bottom of the main body 11, a sleeve body with an opening at the bottom is arranged on the telescopic shaft of the detection module 21, and the temperature sensor 211 is fixed inside the sleeve body.
In this embodiment, in the using process, the telescopic shaft of the cylinder 212 starts to be elongated, and since the temperature sensor 211 is located on the telescopic shaft of the cylinder 212, the temperature sensor 211 can change and move along with the stretching of the telescopic shaft of the cylinder 212, so that the temperature sensor 211 is far away from the main body 11, the detection of the temperature sensor 211 on the temperature data is prevented from being affected by the heat emitted by the main body 11, and the temperature between the temperature sensor 211 and the main body 11 can be further isolated by using the sleeve body.
Further, the device also comprises a transmission module 23 and a wireless module 24, wherein the transmission module 23 is connected with the control module 25 through the wireless module 24, and the detection module 21 and the shooting module 22 are connected to the transmission module 23 and used for wirelessly transmitting the video and temperature data collected by the detection module 21 and the shooting module 22 to the interior of the control module 25.
In this embodiment, in the using process, the temperature and the video image data collected by the temperature sensor 211 and the camera are sent to the inside of the transmission module 23, and since the transmission module 23 is connected to the control module 25 through the wireless module 24, the video image data received by the transmission module 23 can be sent to the inside of the control module 25 under the action of the wireless module 24, and the video image data is displayed by the display in the control module 25 for the user to watch.
Further, the device also comprises a power module 27, and the power module 27 is connected with the detection module 21, the shooting module 22, the transmission module 23, the wireless module 24 and the control module 26 and used for supplying power.
In the present embodiment, during the use process, the power supply is provided for supplying power to the detection module 21, the shooting module 22, the transmission module 23, the wireless module 24, the control module 26 and the motor 14, so that the detection module 21, the shooting module 22, the transmission module 23, the wireless module 24, the control module 26 and the motor 14 can be smoothly supplied with power.
Further, the photographing module 22 is a camera and is fixed to the bottom of the main body 11.
In this embodiment, at the in-process that uses, the camera is fixed in the bottom of main part 11, and unmanned aerial vehicle just can drive the camera and remove when flying, and then through the camera alright shoot the route when unmanned aerial vehicle flies.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle with folding crashproof support function which characterized in that: including main part (11), wing (12), power portion and hinge (16), power portion fixed connection in main part (11), wing (12) are fixed in the outer wall of main part (11), just hinge (16) fixed connection in the outer wall of wing (12), inserted bar (17) have been acceptd to the inside of wing (12), inserted bar (17) run through wing (12), and plug in wing (12).
2. An unmanned aerial vehicle with folding crashproof support function of claim 1, characterized in that: the power portion comprises motor (14) and rotor (15), the output transmission of motor (14) connect in rotor (15), just motor (14) and built-in power supply electric connection.
3. An unmanned aerial vehicle with folding crashproof support function of claim 2, characterized in that: the motor is characterized by further comprising a support frame (13), wherein two ends of the support frame (13) are fixedly connected to the outer walls of the main body (11) and the motor (14) respectively.
4. An unmanned aerial vehicle with folding crashproof support function of claim 1, characterized in that: the wings (12) are arranged in a four-section mode, and each section of the wings (12) are hinged through the hinges (16).
5. An unmanned aerial vehicle with folding crashproof support function of claim 4, characterized in that: each section of the wing (12) is internally provided with holes along the length direction of the wing (12), each hole corresponds to each other, and the inserted bar (17) penetrates through the wing (12) through the holes.
6. The utility model provides an unmanned aerial vehicle monitored control system with folding crashproof support function which characterized in that: including detection module (21), shoot module (22), control module (25) and control module (26), control module (25) with control module (26) are connected for control command's sending and execution, detection module (21) and shooting module (22) all with control module (25) wireless connection for send the data that detect and the video data who shoots to inside control module (25), detection module (21) include temperature sensor (211) and cylinder (212), temperature sensor (211) are fixed in on the telescopic shaft of cylinder (212), just cylinder (212) with control module (26) are connected for control command's execution.
7. The unmanned aerial vehicle monitoring system with function of folding crashproof support of claim 6, characterized in that: the cylinder (212) is fixed at the bottom of the main body (11), a sleeve body with an opening at the bottom is arranged on a telescopic shaft of the detection module (21), and the temperature sensor (211) is fixed inside the sleeve body.
8. The unmanned aerial vehicle monitoring system with function of folding crashproof support of claim 6, characterized in that: the intelligent temperature control system is characterized by further comprising a transmission module (23) and a wireless module (24), wherein the transmission module (23) is connected with the control module (25) through the wireless module (24), and the detection module (21) and the shooting module (22) are connected to the transmission module (23) and used for wirelessly transmitting the video and temperature data collected by the detection module (21) and the shooting module (22) to the inside of the control module (25).
9. The unmanned aerial vehicle monitoring system with function of folding crashproof support of claim 8, characterized in that: the device also comprises a power supply module (27), wherein the power supply module (27) is connected with the detection module (21), the shooting module (22), the transmission module (23), the wireless module (24) and the control module (26) and is used for supplying power.
10. The unmanned aerial vehicle monitoring system with function of folding crashproof support of claim 6, characterized in that: the shooting module (22) is a camera and is fixed at the bottom of the main body (11).
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| Application Number | Priority Date | Filing Date | Title |
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| CN201911301555.9A CN110949668B (en) | 2019-12-17 | 2019-12-17 | Unmanned aerial vehicle with folding crashproof support function and monitored control system thereof |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201911301555.9A CN110949668B (en) | 2019-12-17 | 2019-12-17 | Unmanned aerial vehicle with folding crashproof support function and monitored control system thereof |
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| CN110949668A true CN110949668A (en) | 2020-04-03 |
| CN110949668B CN110949668B (en) | 2021-10-29 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113212732A (en) * | 2021-06-16 | 2021-08-06 | 桂林电子科技大学 | A scalable foldable unmanned aerial vehicle for pipeline monitoring |
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| CN110949668B (en) | 2021-10-29 |
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