CN205311901U - Remote control aircraft - Google Patents
Remote control aircraft Download PDFInfo
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- CN205311901U CN205311901U CN201520939508.8U CN201520939508U CN205311901U CN 205311901 U CN205311901 U CN 205311901U CN 201520939508 U CN201520939508 U CN 201520939508U CN 205311901 U CN205311901 U CN 205311901U
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Abstract
The utility model provides a technical scheme that its technical problem adopted is: a remote control aircraft, includes: ultrasonic ranging appearance, high speed motor, transmission shaft, screw, gravity induction system, gyroscope, wind speed detector, vice servo motor, counter drive shaft, the interface that charges, battery, gyro wheel, voltage regulator device, signal reinforcing means, wireless communication device, PLC controller, data processing device, signal accumulator, signal encryption device, auxiliary propeller, the utility model provides a remote control aircraft, reasonable in design, has advantages such as function high efficiency, easy operation, practicality are strong at simple structure, has overcome present aircraft received external environment easily when flying influence, and wind is too big or interfering signal is too big, all can influence the problem of the flight situation of aircraft, and this device market potential is big, can promote on market.
Description
Technical field
This utility model relates to a kind of Remote aircraft, belongs to Flight Vehicle Design application.
Background technology
There are many remotely-piloted vehicle remote control distances very short now, so flying distance and highly all restricted. Existing stability of aircraft is not high, is susceptible to shake, and is not easily fixed on certain point during flight. Existing aircraft is easily subject to the impact of external environment when flight, and wind is excessive or interference signal is excessive, all can affect the flight condition of aircraft. Existing aircraft is not long for cruising time, must charge after work a period of time. The transmission of existing aircraft signal has delay, card situation easily occurs during for transmission mass data.
For this, a kind of Remote aircraft of design, solve and easily shake in use, the problem of impact flight. Solve the problem that aircraft falls short of cruising time in use. Solve the problem that external interference easily received by aircraft when flight. Solve the problem that the transmission of aircraft signal is unstable. Solve and can not be flown high problem when flight by distance limit. Solve the problem that existing aircraft is not humane in operating interactive.
Summary of the invention
The purpose of this utility model is to provide a kind of Remote aircraft.
This utility model solves its technical problem and be the technical scheme is that a kind of Remote aircraft, including: ultrasonic range finder, high-speed electric expreess locomotive, power transmission shaft, propeller, gravity sensing device, gyroscope, wind speed detector, secondary servomotor, counter drive shaft, charging inlet, battery, roller, stable-pressure device, signal intensifier, wireless communication apparatus, PLC, data processing equipment, signal bin, signal encryption device, auxiliary propeller, it is characterized in that: the charging inlet of Remote aircraft connects battery, battery connects manostat, it is that battery is charged by charging inlet external power source, by manostat, the electric energy of battery operated generation ensures that running voltage is constant, gravity sensing device connects data processing apparatus, data processing equipment connects PLC, first gravity sensing device detects the inclination angle of aircraft, pass data to data processing equipment, after data processing equipment calculates inclination angle, pass information to PLC and be analyzed processing,PLC connects high-speed electric expreess locomotive, high-speed electric expreess locomotive connects propeller by power transmission shaft, PLC sends instruction control high-speed electric expreess locomotive and is operated after information is processed, the power produced after high-speed electric expreess locomotive work is operated by the transmission carrying screws of power transmission shaft; Gyroscope and wind speed detector connect data processing apparatus, gyroscope monitor the shock conditions of aircraft, the resistance of wind speed detector monitoring aircraft, and data information transfer to data processing equipment carries out the process of data; Wireless communication apparatus connects signal intensifier, signal intensifier connects PLC, wireless communication apparatus transmits a signal to this device by wireless signal and carries out the enhancing of signal message, and the transmission of enhanced information is carried out the analyzing and processing of signal message by signal intensifier to PLC; Secondary servomotor connects auxiliary propeller by counter drive shaft, and the power that secondary servomotor work produces is transmitted to auxiliary propeller by counter drive shaft, thus driving auxiliary propeller to be operated; Device is installed signal encryption device, signal encryption device the data information transfer in device is encrypted; Bottom of device installs roller, roller work realize the stable landing of device. Device is installed ultrasonic range finder, is measured the height on device distance ground by the work of ultrasonic range finder.
The beneficial effects of the utility model are: new aircraft longer service life, when takeoff and landing all more stable, better protect aircraft, the Signal Booster being newly added strengthens communication signal, improve the stability of communication, external interference is reduced when high-altitude flight, control more stable, the wind speed detector being newly added can detect wind-force size in real time, it is easy to the power of regulation and control propeller, contribute to aircraft even running, the three-axis gyroscope being newly added can record the vibrations that aerial photography aircraft is small, can make up in real time, ensure aircraft even running, the wireless communication module added can realize remote control, get rid of pining down of signal distance, make aircraft can perform remote task, add ultrasonic range finder and can measure the height that aircraft distance ground is arrived when flight, to better control over aircraft, this aircraft is more outstanding in continuation of the journey, aircraft can be worked long hours.
Accompanying drawing explanation
Fig. 1 is Remote Flight Vehicle Structure schematic diagram.
Detailed description of the invention
Below in conjunction with accompanying drawing, this utility model Remote aircraft is described further.
In Fig. 1,1 ultrasonic range finder, 2 high-speed electric expreess locomotives, 3 power transmission shafts, 4 propellers, 5 gravity sensing devices, 6 gyroscopes, 7 wind speed detectors, 8 secondary servomotors, 9 counter drive shafts, 10 charging inlets, 11--battery, 12 rollers, 13 stable-pressure devices, 14 signal intensifiers, 15 wireless communication apparatus, 16 PLC, 17 data processing equipments, 18 signal bins, 19 signal encryption devices, 20 auxiliary propellers.
The ultrasonic range finder 1 of Remote aircraft can measure the height that aircraft distance ground is arrived when flight, in order to better controls over aircraft. High-speed electric expreess locomotive 2 can produce power by work. Roller 12 and auxiliary propeller 20 are all more stable when takeoff and landing, better protect aircraft. Signal Booster 14 strengthens communication signal, improves the stability of communication, reduces external interference when high-altitude flight, controls more stable.Wind speed detector 7 can detect wind-force size in real time, it is simple to the power of regulation and control propeller, contributes to aircraft even running. Gyroscope 6 can record the vibrations that aerial photography aircraft is small, it is possible to makes up in real time, it is ensured that aircraft even running. Wireless communication apparatus 15 can realize remote control, has got rid of pining down of signal distance so that aircraft can perform remote task. Charging inlet 10 and battery 11 make this aircraft more outstanding in continuation of the journey so that aircraft can work long hours. Power can be transmitted by power transmission shaft 3 and counter drive shaft 9. Propeller 4 makes the device mode of taking off accordingly take off. Gravity sensing device 5 detects the inclination angle of aircraft. Secondary servomotor 8 produces power by work. Stable-pressure device 13 makes the running voltage of aircraft constant, in order to avoid affecting aircraft smooth flight. PLC 16 information to the received signal sends instruction after carrying out integration process. Data processing equipment 17 can carry out the process of data message. Signal bin 18 can store receiving signal message. Data message can be encrypted by signal encryption device 19.
The charging inlet 10 of Remote aircraft connects battery 11, and battery 11 connects manostat 13. Gravity sensing device 5 connects data processing apparatus 17, and data processing equipment 17 connects PLC 16. PLC 16 connects high-speed electric expreess locomotive 2, and high-speed electric expreess locomotive 2 connects propeller 4 by power transmission shaft 3. Gyroscope 6 and wind speed detector 7 connect data processing apparatus 17. Wireless communication apparatus 15 connects signal intensifier 14, and signal intensifier 14 connects PLC 16. Secondary servomotor 8 connects auxiliary propeller 20 by counter drive shaft 9. Device is installed signal encryption device 19. Bottom of device installs roller 12. Device is installed ultrasonic range finder 1.
Its work is made in use by battery 11 power supply. A manostat 13 is had so that the running voltage of aircraft is constant, in order to avoid affecting aircraft smooth flight after battery. When taking off, gravity sensing device (5) first detects the inclination angle of aircraft, pass data to data processing equipment 17, after data processing equipment 17 calculates inclination angle, passing information to PLC 16, PLC controls high-speed electric expreess locomotive 2 carrying screws 4 and takes off by the mode of taking off accordingly. In flight course, the shock conditions of aircraft monitored by gyroscope 6, and wind speed detector 7 monitors the resistance of aircraft, data are processed again through data processor 17, feeding back to PLC 16, PLC is by regulating the rotating speed of high-speed electric expreess locomotive 2, thus reaching flight optimization smoothness. Control signal sends PLC to by wireless communication apparatus 15. Signal intensifier 14 makes signal more stable, reduces noise ripple. When aircraft lands, auxiliary propeller 20 can rotate, it is possible to quickly adjusts the direction of aircraft, adds the roller 12 bottom aircraft, it is possible to achieve stable landing.
This utility model provides a kind of Remote aircraft, reasonable in design, simple in construction, there is the running advantage such as efficient, simple to operate, practical, overcome existing aircraft and be easily subject to the impact of external environment when flight, wind is excessive or interference signal is excessive, capital affects the problem of the flight condition of aircraft, and this device market potential is big, it is possible to commercially promote.
Claims (1)
1. a Remote aircraft, including: ultrasonic range finder, high-speed electric expreess locomotive, power transmission shaft, propeller, gravity sensing device, gyroscope, wind speed detector, secondary servomotor, counter drive shaft, charging inlet, battery, roller, stable-pressure device, signal intensifier, wireless communication apparatus, PLC, data processing equipment, signal bin, signal encryption device, auxiliary propeller, it is characterized in that: the charging inlet of Remote aircraft connects battery, battery connects manostat, it is that battery is charged by charging inlet external power source, by manostat, the electric energy of battery operated generation ensures that running voltage is constant,Gravity sensing device connects data processing apparatus, data processing equipment connects PLC, first gravity sensing device detects the inclination angle of aircraft, pass data to data processing equipment, after data processing equipment calculates inclination angle, pass information to PLC and be analyzed processing; PLC connects high-speed electric expreess locomotive, high-speed electric expreess locomotive connects propeller by power transmission shaft, PLC sends instruction control high-speed electric expreess locomotive and is operated after information is processed, the power produced after high-speed electric expreess locomotive work is operated by the transmission carrying screws of power transmission shaft; Gyroscope and wind speed detector connect data processing apparatus, gyroscope monitor the shock conditions of aircraft, the resistance of wind speed detector monitoring aircraft, and data information transfer to data processing equipment carries out the process of data; Wireless communication apparatus connects signal intensifier, signal intensifier connects PLC, wireless communication apparatus transmits a signal to this device by wireless signal and carries out the enhancing of signal message, and the transmission of enhanced information is carried out the analyzing and processing of signal message by signal intensifier to PLC; Secondary servomotor connects auxiliary propeller by counter drive shaft, and the power that secondary servomotor work produces is transmitted to auxiliary propeller by counter drive shaft, thus driving auxiliary propeller to be operated; Device is installed signal encryption device, signal encryption device the data information transfer in device is encrypted; Bottom of device installs roller, roller work realize the stable landing of device, installs ultrasonic range finder in device, is measured the height on device distance ground by the work of ultrasonic range finder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520939508.8U CN205311901U (en) | 2015-11-24 | 2015-11-24 | Remote control aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520939508.8U CN205311901U (en) | 2015-11-24 | 2015-11-24 | Remote control aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205311901U true CN205311901U (en) | 2016-06-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520939508.8U Expired - Fee Related CN205311901U (en) | 2015-11-24 | 2015-11-24 | Remote control aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN205311901U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106075765A (en) * | 2016-08-05 | 2016-11-09 | 杨勇 | A kind of hydrodynamic force fire-fighting aircraft |
| CN107031830A (en) * | 2017-05-12 | 2017-08-11 | 西华酷农无人机产业园运营有限公司 | It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance |
| CN108313291A (en) * | 2018-03-27 | 2018-07-24 | 郑州大学 | A kind of omnidirectional's aircraft |
| CN110362101A (en) * | 2019-07-22 | 2019-10-22 | 复汉海志(江苏)科技有限公司 | A kind of monitoring system of taking photo by plane based on unmanned plane |
-
2015
- 2015-11-24 CN CN201520939508.8U patent/CN205311901U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106075765A (en) * | 2016-08-05 | 2016-11-09 | 杨勇 | A kind of hydrodynamic force fire-fighting aircraft |
| CN107031830A (en) * | 2017-05-12 | 2017-08-11 | 西华酷农无人机产业园运营有限公司 | It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance |
| CN108313291A (en) * | 2018-03-27 | 2018-07-24 | 郑州大学 | A kind of omnidirectional's aircraft |
| CN110362101A (en) * | 2019-07-22 | 2019-10-22 | 复汉海志(江苏)科技有限公司 | A kind of monitoring system of taking photo by plane based on unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160615 Termination date: 20161124 |
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| CF01 | Termination of patent right due to non-payment of annual fee |