CN112173110A - Multifunctional inspection unmanned aerial vehicle - Google Patents
Multifunctional inspection unmanned aerial vehicle Download PDFInfo
- Publication number
- CN112173110A CN112173110A CN202011173096.3A CN202011173096A CN112173110A CN 112173110 A CN112173110 A CN 112173110A CN 202011173096 A CN202011173096 A CN 202011173096A CN 112173110 A CN112173110 A CN 112173110A
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- China
- Prior art keywords
- fixedly connected
- unmanned aerial
- aerial vehicle
- motors
- main body
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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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
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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
- 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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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
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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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- 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)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Length Measuring Devices By Optical Means (AREA)
Abstract
The invention provides a multifunctional inspection unmanned aerial vehicle which comprises a main body, wherein an inspection camera mechanism is arranged on the main body, four corners of the main body are fixedly connected with swing arms, three motors are fixedly connected to the swing arms, the three motors are arranged in a straight line on the swing arms, output shafts of the motors are fixedly connected with rotor wings, the bottoms of the rotor wings are fixedly connected with fixing frames, and fixing slide rods are fixedly connected to the fixing frames. The unmanned aerial vehicle provided by the invention has the advantages that the motor, the rotating gear, the first toothed plate and the second toothed plate are matched for use, the distance between the placing rods can be adjusted, the placing space can be further adjusted, articles with different sizes can be placed, the purpose of routing inspection can be timely achieved through the arrangement of the routing inspection camera mechanism, the load capacity of the unmanned aerial vehicle can be increased and the transportation efficiency of the unmanned aerial vehicle can be improved through the arrangement of the twelve motors and the rotor wings, and the unmanned aerial vehicle provided by the invention has the advantages of simple and reasonable structural design, convenience and quickness in use and very strong practicability.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to a multifunctional inspection unmanned aerial vehicle.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.
Along with unmanned aerial vehicle's popularization and usage are extensive day by day, utilize unmanned aerial vehicle to carry out transporting of smallclothes article also to become more and more common when patrolling and examining, can not place the space according to the control of the big or small rationality of article when current unmanned aerial vehicle places article, brought the inconvenience for the user.
Disclosure of Invention
The invention aims to provide a multifunctional inspection unmanned aerial vehicle which has the characteristics of inspection and convenience for a user to place articles.
In order to achieve the above purpose, the invention provides the following technical scheme: a multifunctional inspection unmanned aerial vehicle comprises a main body, wherein an inspection camera mechanism is arranged on the main body, four corners of the main body are fixedly connected with swing arms, three motors are fixedly connected to the swing arms, the three motors are arranged in a line on the swing arms, output shafts of the motors are fixedly connected with rotor wings, the bottoms of the rotor wings are fixedly connected with fixing frames, and fixing slide rods are fixedly connected to the fixing frames;
the bottom fixedly connected with motor of main part, the output shaft fixedly connected with swing pinion of motor, swing pinion's both sides mesh respectively has first pinion rack and second pinion rack, the equal fixedly connected with connecting plate of tip of first pinion rack and second pinion rack, fixedly connected with sliding sleeve on the connecting plate, fixed slide bar runs through the sliding sleeve, the pole is placed to the bottom fixedly connected with of connecting plate, the tip fixedly connected with connecting rod of placing the pole.
Further, in the invention, the connecting plate, the placing rod and the connecting rod are all made of carbon fiber.
Further, in the present invention, the number of the placing rods is six.
Further, in the invention, a support rod is fixedly connected to the fixing frame, and the top end of the support rod is fixedly connected with the swing arm.
Furthermore, in the invention, the inspection camera mechanism comprises two cameras, sound wave detection probes are arranged below the two cameras, infrared distance measurement probes are arranged above the two cameras, and illuminating lamps are arranged below the two cameras.
Further, in the present invention, a control system and a power system are provided in the main body.
The beneficial effects are that the technical scheme of this application possesses following technological effect: the unmanned aerial vehicle provided by the invention has the advantages that the motor, the rotating gear, the first toothed plate and the second toothed plate are matched for use, the distance between the placing rods can be adjusted, the placing space can be further adjusted, articles with different sizes can be placed, the purpose of routing inspection can be timely achieved through the arrangement of the routing inspection camera mechanism, the load capacity of the unmanned aerial vehicle can be increased and the transportation efficiency of the unmanned aerial vehicle can be improved through the arrangement of the twelve motors and the rotor wings, and the unmanned aerial vehicle provided by the invention has the advantages of simple and reasonable structural design, convenience and quickness in use and very strong practicability.
It should be understood that all combinations of the foregoing concepts and additional concepts described in greater detail below can be considered as part of the inventive subject matter of this disclosure unless such concepts are mutually inconsistent.
The foregoing and other aspects, embodiments and features of the present teachings can be more fully understood from the following description taken in conjunction with the accompanying drawings. Additional aspects of the present invention, such as features and/or advantages of exemplary embodiments, will be apparent from the description which follows, or may be learned by practice of specific embodiments in accordance with the teachings of the present invention.
Drawings
The drawings are not intended to be drawn to scale. In the drawings, each identical or nearly identical component that is illustrated in various figures may be represented by a like numeral. For purposes of clarity, not every component may be labeled in every drawing. Embodiments of various aspects of the present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1 is a schematic view of the structure of the present invention.
FIG. 2 is a schematic diagram of a partial structure of the present invention.
In the figures, the meaning of the reference numerals is as follows: 1. a main body; 2. a swing arm; 3. a motor; 4. a rotor; 5. a fixed mount; 6. a support rod; 7. fixing the sliding rod; 8. a sliding sleeve; 9. a connecting plate; 10. placing a rod; 11. a connecting rod; 12. a motor; 13. a rotating gear; 14. a first toothed plate; 15. a second toothed plate.
Detailed Description
In order to better understand the technical content of the present invention, specific embodiments are described below with reference to the accompanying drawings. In this disclosure, aspects of the present invention are described with reference to the accompanying drawings, in which a number of illustrative embodiments are shown. Embodiments of the present disclosure are not necessarily intended to include all aspects of the invention. It should be appreciated that the various concepts and embodiments described above, as well as those described in greater detail below, may be implemented in any of numerous ways, as the disclosed concepts and embodiments are not limited to any one implementation. In addition, some aspects of the present disclosure may be used alone, or in any suitable combination with other aspects of the present disclosure.
As shown in fig. 1-2, a multi-functional unmanned aerial vehicle that patrols and examines includes main part 1, is provided with control system and electric power system in the main part 1, and control system includes wireless signal transceiver, control box, flight control system, and electric power system includes power supply unit. Be provided with on the main part 1 and patrol and examine camera mechanism, patrol and examine camera mechanism and include two cameras, be provided with sound wave probe below two cameras, be provided with infrared distance measuring probe above two cameras, be provided with the light below two cameras.
Four corners of the main body 1 are fixedly connected with radial arms 2, the radial arms 2 are fixedly connected with three motors 3, the three motors 3 are arranged in a straight line on the radial arms 2, output shafts of the motors 3 are fixedly connected with rotor wings 4, the bottoms of the rotor wings 4 are fixedly connected with fixing frames 5, and the fixing frames 5 are fixedly connected with fixed sliding rods 7;
the bottom fixedly connected with motor 12 of main part 1, the output shaft fixedly connected with rotary gear 13 of motor 12, rotary gear 13's both sides have meshing respectively first pinion rack 14 and second pinion rack 15, the equal fixedly connected with connecting plate 9 of tip of first pinion rack 14 and second pinion rack 15, fixedly connected with sliding sleeve 8 on the connecting plate 9, fixed slide bar 7 runs through sliding sleeve 8, the bottom fixedly connected with of connecting plate 9 places pole 10, place the tip fixedly connected with connecting rod 11 of pole 10. During the specific use, the user sends the signal of taking off through the remote controller, in the radio signal transceiver receives the flight control system of signal transmission in the control box behind the signal, the electronic 3 circular telegram of flight control system control starts, motor 3 drives the rotatory buoyancy that produces of rotor 4 and makes unmanned aerial vehicle take off, direction and the height through the flight of remote controller control unmanned aerial vehicle, when unmanned aerial vehicle reachs the appointed place, two cameras are to being shot by the detection zone, high definition image and the temperature image transmission that two cameras were shot are to the flight control system in, the flight control system utilizes the radio signal transceiver to transmit the picture to the remote controller on, make things convenient for ground personnel to look over, infrared range finder can detect the distance that unmanned aerial vehicle apart from being detected the object simultaneously, conveniently adjust unmanned aerial vehicle's position, sound wave detecting probe can detect being detected object inner structure. Further, the motor 12 is started, the output shaft of the motor 12 drives the rotating gear 13 to rotate, the rotating gear 13 drives the first toothed plate 14 and the second toothed plate 15 to move, the first toothed plate 14 and the second toothed plate 15 drive the opposite placing rods 10 to move, the distance between the placing rods 10 is adjusted, and then the placing space of an article is adjusted.
This embodiment is preferred, and connecting plate 9, the material of placing pole 10 and connecting rod 11 are the carbon fiber, can reduce unmanned aerial vehicle's weight.
In the present embodiment, it is preferable that the number of the placing rods 10 is six, and the placing rods 10 and the connecting rods 11 form a placing space for placing the article.
This embodiment is preferred, fixedly connected with cradling piece 6 on the mount 5, and the top and the spiral arm 2 fixed connection of cradling piece 6 through the setting of cradling piece 6, can increase the stability of unmanned aerial vehicle structure.
To sum up, the space between the placing rods 10 can be adjusted through the matching use of the motor 12, the rotating gear 13, the first toothed plate 14 and the second toothed plate 15, so that the placing space can be adjusted, articles with different sizes can be placed, the purpose of routing inspection can be achieved in time through the arrangement of the routing inspection camera mechanism, the load capacity of the unmanned aerial vehicle can be increased through the arrangement of the twelve motors 3 and the rotor wings 4, and the transportation efficiency of the unmanned aerial vehicle is improved.
Although the present invention has been described with reference to the preferred embodiments, it is not intended to be limited thereto. Those skilled in the art can make various changes and modifications without departing from the spirit and scope of the invention. Therefore, the protection scope of the present invention should be determined by the appended claims.
Claims (6)
1. The utility model provides a multi-functional unmanned aerial vehicle that patrols and examines, includes main part (1), its characterized in that: the inspection camera shooting device is characterized in that an inspection camera shooting mechanism is arranged on the main body (1), four corners of the main body (1) are fixedly connected with swing arms (2), the swing arms (2) are fixedly connected with three motors (3), the three motors (3) are arranged in a line on the swing arms (2), output shafts of the motors (3) are fixedly connected with rotor wings (4), the bottoms of the rotor wings (4) are fixedly connected with fixing frames (5), and fixing slide rods (7) are fixedly connected to the fixing frames (5);
the bottom fixedly connected with motor (12) of main part (1), the output shaft fixedly connected with swing gear (13) of motor (12), the both sides of swing gear (13) mesh respectively has first pinion rack (14) and second pinion rack (15), the equal fixedly connected with connecting plate (9) of tip of first pinion rack (14) and second pinion rack (15), fixedly connected with sliding sleeve (8) on connecting plate (9), sliding sleeve (8) are run through in fixed slide bar (7), pole (10) are placed to the bottom fixedly connected with of connecting plate (9), place the tip fixedly connected with connecting rod (11) of pole (10).
2. The multifunctional inspection unmanned aerial vehicle of claim 1, wherein: the connecting plate (9), the placing rod (10) and the connecting rod (11) are made of carbon fibers.
3. The multifunctional inspection unmanned aerial vehicle of claim 1, wherein: the number of the placing rods (10) is six.
4. The multifunctional inspection unmanned aerial vehicle of claim 1, wherein: the support frame (5) is fixedly connected with a support rod (6), and the top end of the support rod (6) is fixedly connected with the spiral arm (2).
5. The multifunctional inspection unmanned aerial vehicle of claim 1, wherein: patrol and examine camera mechanism and include two cameras, two camera below are provided with sound wave probe, two camera tops are provided with infrared distance measuring probe, two camera below are provided with the light.
6. The multifunctional inspection unmanned aerial vehicle of claim 1, wherein: a control system and a power system are arranged in the main body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011173096.3A CN112173110A (en) | 2020-10-28 | 2020-10-28 | Multifunctional inspection unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011173096.3A CN112173110A (en) | 2020-10-28 | 2020-10-28 | Multifunctional inspection unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112173110A true CN112173110A (en) | 2021-01-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011173096.3A Pending CN112173110A (en) | 2020-10-28 | 2020-10-28 | Multifunctional inspection unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN112173110A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113212730A (en) * | 2021-05-28 | 2021-08-06 | 张小兵 | Double-body logistics unmanned aerial vehicle with detachable cargo compartment connecting wings |
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| CN205034334U (en) * | 2015-10-21 | 2016-02-17 | 浙江智天科技有限公司 | Multiaxis aircraft of screw dislocation dress |
| CN106347626A (en) * | 2016-11-16 | 2017-01-25 | 北京韦加无人机科技股份有限公司 | Foldable multi-rotor plant protection unmanned aerial vehicle |
| CN107298176A (en) * | 2017-06-21 | 2017-10-27 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being used to carry express delivery and the absorption that can hover |
| CN107315423A (en) * | 2017-08-23 | 2017-11-03 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of new patrol unmanned machine inspection device and method for inspecting |
| CN108357674A (en) * | 2018-04-17 | 2018-08-03 | 山东农业大学 | It can small more rotor unmanned aircrafts of paddle outside big paddle in tilted propeller |
-
2020
- 2020-10-28 CN CN202011173096.3A patent/CN112173110A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205034334U (en) * | 2015-10-21 | 2016-02-17 | 浙江智天科技有限公司 | Multiaxis aircraft of screw dislocation dress |
| CN106347626A (en) * | 2016-11-16 | 2017-01-25 | 北京韦加无人机科技股份有限公司 | Foldable multi-rotor plant protection unmanned aerial vehicle |
| CN107298176A (en) * | 2017-06-21 | 2017-10-27 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being used to carry express delivery and the absorption that can hover |
| CN107315423A (en) * | 2017-08-23 | 2017-11-03 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of new patrol unmanned machine inspection device and method for inspecting |
| CN108357674A (en) * | 2018-04-17 | 2018-08-03 | 山东农业大学 | It can small more rotor unmanned aircrafts of paddle outside big paddle in tilted propeller |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113212730A (en) * | 2021-05-28 | 2021-08-06 | 张小兵 | Double-body logistics unmanned aerial vehicle with detachable cargo compartment connecting wings |
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