CN114162314A - Novel unmanned aerial vehicle able to programme - Google Patents
Novel unmanned aerial vehicle able to programme Download PDFInfo
- Publication number
- CN114162314A CN114162314A CN202111575242.XA CN202111575242A CN114162314A CN 114162314 A CN114162314 A CN 114162314A CN 202111575242 A CN202111575242 A CN 202111575242A CN 114162314 A CN114162314 A CN 114162314A
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- shell
- unmanned aerial
- aerial vehicle
- novel programmable
- novel
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- 239000006096 absorbing agent Substances 0.000 claims abstract description 4
- 230000035939 shock Effects 0.000 claims abstract description 4
- 230000005540 biological transmission Effects 0.000 claims description 4
- 239000004698 Polyethylene Substances 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 3
- -1 polyethylene Polymers 0.000 claims description 3
- 229920000573 polyethylene Polymers 0.000 claims description 3
- 229920001169 thermoplastic Polymers 0.000 claims description 3
- 239000004416 thermosoftening plastic Substances 0.000 claims description 3
- 230000000087 stabilizing effect Effects 0.000 claims 2
- 230000000694 effects Effects 0.000 abstract description 4
- 239000000463 material Substances 0.000 abstract description 3
- 230000002093 peripheral effect Effects 0.000 abstract description 3
- 238000012544 monitoring process Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 3
- 230000007613 environmental effect Effects 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
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- 239000002245 particle Substances 0.000 description 1
- 238000012549 training Methods 0.000 description 1
- 239000002912 waste gas Substances 0.000 description 1
- 238000003911 water pollution Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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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; ARRANGEMENT 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
- 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
- B64D47/02—Arrangements or adaptations of signal or lighting devices
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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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention is suitable for the technical field of robots, and provides a novel programmable unmanned aerial vehicle which comprises a shell, wherein propellers are arranged at the upper ends of four corners of the shell, a propeller protection ring is arranged on one side of the shell, supporting legs are arranged at the bottom end of the shell, shock absorbers are arranged on the supporting legs, and a motor for driving the propellers to rotate is arranged in the shell; the novel programmable unmanned aerial vehicle is an unmanned aerial vehicle developed for teenagers, can be programmed by a computer, automatically flies and controls, guides students to learn programming, is light in material, resistant to falling, stable and safe in flying, can hover, is externally provided with a wireless remote controller, a camera, an external hanging part, a colored LED lamp and other extensible peripheral devices, teaches in fun through lively activities, and enables flying to be more interesting.
Description
Technical Field
The invention belongs to the technical field of robots, and particularly relates to a novel programmable unmanned aerial vehicle.
Background
Unmanned aerial vehicle is the unmanned aircraft that utilizes radio remote control or self-contained program control device to control, and along with the continuous progress of science and technology, the development of unmanned aerial vehicle technique is more and more mature, and the application is more and more extensive. The application of unmanned aerial vehicles in civil fields such as homeland monitoring, logistics, environmental monitoring and the like is increasingly paid attention, and related technologies are mature day by day. At present, with the help of technologies such as video transmission and aerial photography, unmanned aerial vehicle is more and more wide in the application of environmental emergency monitoring field. The unmanned aerial vehicle environment monitoring mainly focuses on two aspects, namely, the unmanned aerial vehicle is adopted to investigate the water pollution range, the garbage distribution range, the chimney waste gas emission condition and the like; and secondly, monitoring the concentration of gas or particles by carrying an ambient air monitoring instrument.
Unmanned aerial vehicle products for teaching and training purposes are few in types in the market at present, and products with wheelbases (the length of the diagonal line of a four-axis aircraft) of 130mm or less are more scarce in the market at present, and still have more problems.
1. The unable DIY of education in the existing market is with unmanned aerial vehicle product, can't do all can't assemble the problem of carrying out the accessory upgrading. Related education products in the market mostly take flight experience and simple accessory replacement as the main.
2. The safety of the products in the market is poor, and the serious consequences can be caused when the operation is not standard for a novice.
3. The product on the market has poor flight stability and is not suitable for the beginner to fly.
Disclosure of Invention
The invention provides a novel programmable unmanned aerial vehicle, and aims to solve the problems that the robot has low flexibility and stiff steering and is easy to have accidents when the steering meets an obstacle because a complex program is needed to complete the steering work.
The invention discloses a novel programmable unmanned aerial vehicle which comprises a shell, wherein propellers are arranged at the upper ends of four corners of the shell, a propeller protection ring is arranged on one side of the shell, supporting legs are arranged at the bottom end of the shell, shock absorbers are arranged on the supporting legs, and a motor for driving the propellers to rotate is arranged in the shell.
Preferably, a single chip microcomputer control system is arranged in the shell and comprises a wireless receiver.
Preferably, the lower end of the shell is provided with a camera and a color LED lamp.
Preferably, the single chip microcomputer control system further comprises a camera image transmission module and a sensor which are matched with the camera.
Preferably, the sensor includes the gyroscope and the barometer, barometer one end is connected with the output of the steady voltage chip that sets up, and the one end of gyroscope is connected with the output of steady voltage chip, and barometer and gyroscope connect jointly on same root bus and the mainboard that sets up and link to each other and connect and carry out the communication, detect the data of barometer and gyroscope in the mainboard.
Preferably, a battery compartment is arranged in the shell, and a detachable rechargeable battery is correspondingly installed in the battery compartment.
Preferably, the lower end of the shell is provided with a bin door convenient for replacing the battery.
Preferably, the shell is made of light and drop-resistant thermoplastic polyethylene.
Advantageous effects
Compared with the prior art, the invention has the beneficial effects that: the novel programmable unmanned aerial vehicle is an unmanned aerial vehicle developed for teenagers, can be programmed by a computer, automatically flies and controls, guides students to learn programming, is light in material, resistant to falling, stable and safe in flying, can hover, is externally provided with a wireless remote controller, a camera, an external hanging part, a colored LED lamp and other extensible peripheral devices, teaches in fun through lively activities, and enables flying to be more interesting.
Drawings
FIG. 1 is a schematic side sectional view of the structure of the chassis of the present invention;
in the figure: the propeller protection device comprises a shell 1, a propeller 2 and a propeller protection ring 3.
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.
Referring to the attached drawings of the specification, the invention provides a technical scheme that: the utility model provides a novel unmanned aerial vehicle able to programme, includes casing 1, 1 four corners upper end of casing all is equipped with screw 2, 1 one side of casing is equipped with screw guard circle 3, 1 bottom of casing is equipped with the landing leg, be equipped with the bumper shock absorber on the landing leg, be equipped with 2 pivoted motors of drive screw in the casing 1.
Further, a single chip microcomputer control system is arranged in the shell 1 and comprises a wireless receiver.
Furthermore, the lower end of the shell 1 is provided with a camera and a color LED lamp.
Furthermore, the single chip microcomputer control system also comprises a camera image transmission module and a sensor which are matched with the camera.
Further, the sensor includes the gyroscope and the barometer, barometer one end is connected with the output of the steady voltage chip that sets up, and the one end of gyroscope is connected with the output of steady voltage chip, and barometer and gyroscope connect jointly on same root bus and the mainboard that sets up and link to each other and connect and carry out the communication, detect the data of barometer and gyroscope in the mainboard.
Furthermore, a battery compartment is arranged in the shell 1, and a detachable rechargeable battery is correspondingly installed in the battery compartment.
Furthermore, the lower end of the shell 1 is provided with a bin door convenient for replacing the battery.
Further, the housing 1 is made of light and shatter-resistant thermoplastic polyethylene.
The novel programmable unmanned aerial vehicle is an unmanned aerial vehicle developed for teenagers, can be programmed by a computer, automatically flies and controls, guides students to learn programming, is light in material, resistant to falling, stable and safe in flying, can hover, is externally provided with a wireless remote controller, a camera, an external hanging part, a colored LED lamp and other extensible peripheral devices, teaches in fun through lively activities, and enables flying to be more interesting.
The above embodiments are provided to further explain the objects, technical solutions and advantages of the present invention in detail, it should be understood that the above embodiments are only examples of the present invention and are not intended to limit the present invention, and any modifications, equivalents, improvements and the like made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms indicating an orientation or positional relationship are based on the orientation or positional relationship shown in the drawings only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings or the orientations or positional relationships that the products of the present invention are conventionally placed in use, and are only used for convenience in describing the present invention and simplifying the description, but do not indicate or imply that the devices or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the present invention, unless otherwise expressly stated or limited, the first feature may be present on or under the second feature in direct contact with the first and second feature, or may be present in the first and second feature not in direct contact but in contact with another feature between them. Also, the first feature being above, on or above the second feature includes the first feature being directly above and obliquely above the second feature, or merely means that the first feature is at a higher level than the second feature. A first feature that underlies, and underlies a second feature includes a first feature that is directly under and obliquely under a second feature, or simply means that the first feature is at a lesser level than the second feature.
Claims (8)
1. A novel unmanned aerial vehicle able to programme, its characterized in that: the improved multifunctional shell comprises a shell, wherein propellers are arranged at the upper ends of four corners of the shell, a propeller protection ring is arranged on one side of the shell, supporting legs are arranged at the bottom end of the shell, shock absorbers are arranged on the supporting legs, and a motor for driving the propellers to rotate is arranged in the shell.
2. A novel programmable drone according to claim 1, characterised in that: a single chip microcomputer control system is arranged in the shell and comprises a wireless receiver.
3. A novel programmable drone according to claim 2, characterised in that: the lower end of the shell is provided with a camera and a colorful LED lamp.
4. A novel programmable drone according to claim 3, characterised in that: the single chip microcomputer control system further comprises a camera image transmission module and a sensor which are matched with the camera.
5. The novel programmable drone of claim 4, characterized in that: the sensor comprises a gyroscope and a barometer, one end of the barometer is connected with the output end of a voltage stabilizing chip, one end of the gyroscope is connected with the output end of the voltage stabilizing chip, the barometer and the gyroscope are jointly connected on the same bus and connected with a set mainboard for communication, and data of the barometer and the gyroscope are detected in the mainboard.
6. The novel programmable drone of claim 5, characterized in that: a battery bin is arranged in the shell, and a detachable rechargeable battery is correspondingly arranged in the battery bin.
7. The novel programmable drone of claim 6, characterized in that: the lower end of the shell is provided with a bin door convenient for replacing the battery.
8. A novel programmable drone according to claim 7, characterised in that: the shell is made of light and anti-falling thermoplastic polyethylene.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202111575242.XA CN114162314A (en) | 2021-12-21 | 2021-12-21 | Novel unmanned aerial vehicle able to programme |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202111575242.XA CN114162314A (en) | 2021-12-21 | 2021-12-21 | Novel unmanned aerial vehicle able to programme |
Publications (1)
Publication Number | Publication Date |
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CN114162314A true CN114162314A (en) | 2022-03-11 |
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CN202111575242.XA Pending CN114162314A (en) | 2021-12-21 | 2021-12-21 | Novel unmanned aerial vehicle able to programme |
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CN (1) | CN114162314A (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100661618B1 (en) * | 2005-12-21 | 2006-12-26 | 한국생산기술연구원 | Quad-rotor type electric organic aerial vehicle |
CN106178528A (en) * | 2016-08-31 | 2016-12-07 | 北京趣智阿尔法科技有限公司 | Education unmanned plane able to programme |
CN111137466A (en) * | 2020-01-13 | 2020-05-12 | 深圳市星图智控科技有限公司 | Unmanned aerial vehicle capable of being monitored and monitoring shooting method of unmanned aerial vehicle |
JP2020080853A (en) * | 2018-11-22 | 2020-06-04 | ハングク サムゴン カンパニー・リミテッドHankooksamgong Co.,Ltd. | Agricultural drone having conveyor type discharger |
-
2021
- 2021-12-21 CN CN202111575242.XA patent/CN114162314A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100661618B1 (en) * | 2005-12-21 | 2006-12-26 | 한국생산기술연구원 | Quad-rotor type electric organic aerial vehicle |
CN106178528A (en) * | 2016-08-31 | 2016-12-07 | 北京趣智阿尔法科技有限公司 | Education unmanned plane able to programme |
JP2020080853A (en) * | 2018-11-22 | 2020-06-04 | ハングク サムゴン カンパニー・リミテッドHankooksamgong Co.,Ltd. | Agricultural drone having conveyor type discharger |
CN111137466A (en) * | 2020-01-13 | 2020-05-12 | 深圳市星图智控科技有限公司 | Unmanned aerial vehicle capable of being monitored and monitoring shooting method of unmanned aerial vehicle |
Non-Patent Citations (1)
Title |
---|
龙顺宇、杨伟、钟鹏飞, 北京工业大学出版社 * |
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Application publication date: 20220311 |
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