CN204452931U - One follows four-axle aircraft - Google Patents
One follows four-axle aircraft Download PDFInfo
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- CN204452931U CN204452931U CN201520106371.8U CN201520106371U CN204452931U CN 204452931 U CN204452931 U CN 204452931U CN 201520106371 U CN201520106371 U CN 201520106371U CN 204452931 U CN204452931 U CN 204452931U
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Abstract
The utility model relates to one and to take photo by plane four-axle aircraft, particularly relate to one and follow four-axle aircraft, mainly comprise: aircraft and the telecommand equipment with four horns, aircraft interior is equipped with memory device, treater and engine installation, filming apparatus and The Cloud Terrace are housed bottom aircraft, the longitude and latitude data that second GPS locator is measured by the second dual-mode antenna by telecommand equipment are sent to aircraft, thus aircraft will monitor telecommand equipment position, treater can calculate the distance between aircraft and telecommand equipment, aircraft is respectively equipped with brushless motor at four horn ends, propeller and protective case, described aircraft interior is provided with height detecting device, barometric information is sent to treater by height detecting device, aircraft interior is provided with the ultrasonic transduter for detecting objects in front, telecommand equipment is provided with read out instrument, when flying at the rural atmosphere of complexity, aircraft can teaching display stand motion dynamic following, what solve aircraft follows the problem of taking photo by plane.
Description
Technical field
The utility model relates to one and to take photo by plane four-axle aircraft, particularly relates to one and follows four-axle aircraft.
Background technology
The modern fast development along with science and technology, people are increasingly deep for the research of aircraft, and all kinds of aircraft is applied in increasing occasion.Four rotor unmanned aircrafts are compared with other aircraft, and its physical construction is simply compact, and take action more flexible, landing environmental requirement is lower, has good operating characteristic, can realize among a small circle taking off, hover, landing.Due to these features, the numerous areas such as quadrotor has been widely used in taking photo by plane, monitor, investigate, search and rescue, control of agricultural pest.
Although four-axle aircraft has had various functions and expansion at present, as taking photo by plane in the air, still have larger deficiency, that can not realize track shot exactly in the process of taking photo by plane.Especially for taking photo by plane during outdoor sport, because can not realize following, thus miss a lot of excellent moments, complexity landform you cannot move on operation limit, limit, aircraft is taken photo by plane in the air quite inconvenient.
Summary of the invention
The purpose of this utility model is for the existing state of the art, provides a kind of and utilizes two GPS location to follow the four-axle aircraft of telecommand equipment.
For achieving the above object, the utility model adopts following technical scheme:
One follows four-axle aircraft, mainly comprise: aircraft and the telecommand equipment with four horns, described aircraft interior is equipped with memory device, treater and engine installation, filming apparatus and The Cloud Terrace are housed bottom aircraft, the treater of described aircraft interior is electrically connected on memory device, engine installation, first dual-mode antenna and the first GPS locator, described telecommand equipment inside is provided with controller, controller is electrically connected on manipulation handle, second dual-mode antenna and the second GPS locator, the longitude and latitude data that second GPS locator is measured by the second dual-mode antenna by telecommand equipment are sent to aircraft, thus aircraft will monitor telecommand equipment position, treater can calculate the distance between aircraft and telecommand equipment.
Further; the engine installation of described aircraft interior is primarily of brushless motor plate, brushless motor and propeller; aircraft is respectively equipped with brushless motor, propeller and protective case at four horn ends, and aircraft is connected to treater at the brushless motor plate of four horn inside.
Further, described aircraft interior is provided with height detecting device, and barometric information is sent to treater by height detecting device.
Further, described aircraft interior is provided with the ultrasonic transduter for detecting objects in front, and ultrasonic transduter is electrically connected on treater.
Further, described telecommand equipment is provided with read out instrument, and read out instrument receives the photographic images of filming apparatus.
Further, described telecommand equipment top is provided with the second dual-mode antenna and the second GPS locator.
In such scheme, described aircraft and telecommand equipment shell adopt ABS plastic raw material to make.
The beneficial effects of the utility model are:
1, the utility model adopts two GPS locator to carry out the distance of sense aircraft and telecommand equipment, when flying at the rural atmosphere of complexity, aircraft can teaching display stand motion dynamic following, what solve aircraft follows the problem of taking photo by plane, compare and conventional aircraft, not only simply easy to operate, be applicable to various age level, and shooting effect is strengthened very well;
2, the protective case of four-axle aircraft four horn ends can not only protect propeller and body by actv., and avoids the propeller of aircraft in flight course rotates to collide other objects, causes air crash out of control; Brushless motor makes the flying power of four-axle aircraft and flight life-span increase substantially;
3, four-axle aircraft inside is provided with ultrasonic transduter and height detecting device, and when telecommand equipment followed by aircraft, its ultrasonic transduter effectively can obtain the object in explorer vehicle front, thus the track collision free of change of flight is to object; Height detecting device determines flying height by detecting air pressure numerical value, improves four-axle aircraft positional precision, can control the distance of aircraft and telecommand equipment accurately.
accompanying drawing illustrates:
Accompanying drawing 1 is aircraft block diagram of the present utility model;
Accompanying drawing 2 is telecommand equipment block diagram of the present utility model;
Accompanying drawing 3 is frame diagram of the present utility model.
detailed description of the invention:
Can have the object of the utility model, feature and function to make juror and further understand, hereby lift preferred embodiment and coordinate graphic being described in detail as follows:
Refer to shown in Fig. 1 ~ 3, it is the accompanying drawing of the preferred embodiment of the utility model, one follows four-axle aircraft, mainly comprise: aircraft 1 and the telecommand equipment 2 with four horns, memory device 11 is equipped with in described aircraft 1 inside, treater 12 and engine installation 13, filming apparatus 4 and The Cloud Terrace 5 are housed bottom aircraft 1, filming apparatus 4 used The Cloud Terrace 5 to be arranged on bottom aircraft 1, when aircraft 1 is when flying, the picture of aerial photographing just can be recorded by filming apparatus 4, the treater 12 of aircraft 1 inside is electrically connected on memory device 11, engine installation 13, first dual-mode antenna 14 and the first GPS locator 15, its aircraft 1 is received telecommand equipment 2 by the first dual-mode antenna 14 and is sent control signal, described telecommand equipment 2 inside is provided with controller 21, controller 21 is electrically connected on manipulation handle 22, second dual-mode antenna 23 and the second GPS locator 24, manipulation handle 22 pairs of controllers 21 send instruction, the longitude and latitude data that second GPS locator is measured by the second dual-mode antenna by telecommand equipment are sent to aircraft, thus aircraft will monitor telecommand equipment position, treater can calculate the distance between aircraft and telecommand equipment, telecommand equipment 2 refreshes reading by controller 21 immediately to the second GPS locator 24, the longitude and latitude of telecommand equipment 2 is sent to aircraft 1 by the very first time, aircraft 1 carries out flight displacement according to the longitude and latitude of telecommand equipment 2, keep the distance of specifying.
In such scheme, the engine installation 13 of aircraft 1 inside is primarily of brushless motor plate 131, brushless motor 132 and propeller 133, aircraft 1 is respectively equipped with brushless motor 132, propeller 133 and protective case 134 at four horn ends, aircraft 1 is connected to treater 12 at the brushless motor plate 131 of four horn inside, treater 12 controls brushless motor 132 and propeller 133 by brushless motor plate 131, thus controlling speed and the direction of aircraft 1 flight, protective case 134 can avoid the propeller 133 in rotation to collide other objects very well; Described aircraft 1 inside is provided with height detecting device 16, height detecting device 16 is baroceptor, barometric information is sent to treater 12 by height detecting device 16, detect the height of flight, height detecting device 16 coordinates the first GPS locator 15 to determine the Spatial Dimension of aircraft 1, thus the distance of calculating aircraft 1 and telecommand equipment 2; Described aircraft 1 inside is provided with the ultrasonic transduter 17 for detecting objects in front, ultrasonic transduter 17 is electrically connected on treater 12, when telecommand equipment 2 followed by aircraft 1, its ultrasonic transduter 17 effectively can obtain the object in explorer vehicle front, thus the track collision free of change of flight is to object.
Above-mentioned telecommand equipment 2 is provided with read out instrument 6, read out instrument 6 receives the photographic images of filming apparatus 4, aircraft 1 starts filming apparatus 4 when flying, and the image aloft photographed is sent on the read out instrument 6 of telecommand equipment 2, manipulator can distant surveillance shooting picture, and described telecommand equipment 2 top is provided with the second dual-mode antenna 23 and the second GPS locator 24.Described aircraft 1 and telecommand equipment 2 shell adopt ABS plastic raw material to make, and the crash resistance of product is strengthened.
Embodiment 1: operator starts aircraft 1 follow the mode by telecommand equipment 2, when operator carry telecommand equipment 2 move time, the controller 21 of telecommand equipment 2 inside refreshes reading immediately to the second GPS locator 24, and by the second dual-mode antenna 23, longitude and latitude signal is sent to aircraft 1, aircraft 1 receives longitude and latitude signal by the first dual-mode antenna 14, and this signal is sent to inner treater 12, the data that treater 12 sends in conjunction with the first GPS locator 15 and height detecting device 16 carry out computing, direction and the speed of aircraft 1 flight is adjusted by aircraft 1 and telecommand equipment 2 longitude and latitude between the two, aircraft 1 and telecommand equipment 2 keep the distance set between the two, the dynamic following of teaching display stand motion, following of aircraft 1 is kept to take photo by plane.
Embodiment 2: operator starts aircraft 1 by telecommand equipment 2 and to make a return voyage pattern, when operator carry telecommand equipment 2 static time, the controller 21 of telecommand equipment 2 inside reads the second GPS locator 24 internal data, and by the second dual-mode antenna 23, longitude and latitude signal is sent to aircraft 1, aircraft 1 receives longitude and latitude signal by the first dual-mode antenna 14, and this signal is sent to inner treater 12, signal control engine installation 13 is sent by treater 12, the direction that adjustment aircraft 1 flies, until the first GPS locator 15 and the second GPS locator 24 to measure longitude and latitude consistent, aircraft 1 does dropping action, complete a key to make a return voyage.
Certainly, above diagram is only the utility model better embodiment, not limits range of use of the present utility model with this, therefore, every make in the utility model principle equivalence change all should be included in protection domain of the present utility model.
Claims (7)
1. follow four-axle aircraft for one kind, mainly comprise: aircraft (1) and the telecommand equipment (2) with four horns, memory device (11) is equipped with in described aircraft (1) inside, treater (12) and engine installation (13), filming apparatus (4) and The Cloud Terrace (5) are equipped with in aircraft (1) bottom, it is characterized in that: the treater (12) of described aircraft (1) inside is electrically connected on memory device (11), engine installation (13), first dual-mode antenna (14) and the first GPS locator (15), described telecommand equipment (2) inside is provided with controller (21), controller (21) is electrically connected on manipulation handle (22), second dual-mode antenna (23) and the second GPS locator (24), the longitude and latitude data that second GPS locator (24) is measured are sent to aircraft (1) by the second dual-mode antenna (23) by telecommand equipment (2), thus aircraft (1) will monitor telecommand equipment (2) position, treater (12) can calculate the distance between aircraft (1) and telecommand equipment (2).
2. one according to claim 1 follows four-axle aircraft; it is characterized in that: the engine installation (13) of described aircraft (1) inside mainly contains brushless motor plate (131), brushless motor (132) and propeller (133); aircraft (1) is respectively equipped with brushless motor (132), propeller (133) and protective case (134) at four horn ends, and aircraft (1) is connected to treater (12) at the brushless motor plate (131) of four horn inside.
3. one according to claim 2 follows four-axle aircraft, it is characterized in that: described aircraft (1) inside is provided with height detecting device (16), and barometric information is sent to treater (12) by height detecting device (16).
4. one according to claim 3 follows four-axle aircraft, it is characterized in that: described aircraft (1) inside is provided with the ultrasonic transduter (17) for detecting objects in front, and ultrasonic transduter (17) is electrically connected on treater (12).
5. one according to claim 1 follows four-axle aircraft, it is characterized in that: described telecommand equipment (2) is provided with read out instrument (6), and read out instrument (6) receives the photographic images of filming apparatus (4).
6. one according to claim 5 follows four-axle aircraft, it is characterized in that: described telecommand equipment (2) top is provided with the second dual-mode antenna (23) and the second GPS locator (24).
7. the one according to claim 1-6 any one follows four-axle aircraft, it is characterized in that: described aircraft (1) and telecommand equipment (2) shell adopt ABS plastic raw material to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520106371.8U CN204452931U (en) | 2015-02-14 | 2015-02-14 | One follows four-axle aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520106371.8U CN204452931U (en) | 2015-02-14 | 2015-02-14 | One follows four-axle aircraft |
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| CN204452931U true CN204452931U (en) | 2015-07-08 |
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| CN201520106371.8U Expired - Fee Related CN204452931U (en) | 2015-02-14 | 2015-02-14 | One follows four-axle aircraft |
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Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105045281A (en) * | 2015-08-13 | 2015-11-11 | 深圳一电科技有限公司 | Unmanned aerial vehicle flight control method and device |
| CN105182348A (en) * | 2015-09-10 | 2015-12-23 | 浙江江宇电机有限公司 | Ultrasonic-wave-based unmanned plane real time positioning and tracking device and application technology of the same |
| CN105204520A (en) * | 2015-09-17 | 2015-12-30 | 深圳市十方联智科技有限公司 | Method for controlling unmanned aerial vehicle |
| CN105235912A (en) * | 2015-10-30 | 2016-01-13 | 深圳高启科技有限公司 | Aerial photography collection unmanned aerial vehicle for law enforcement of police fire protection and control method thereof |
| CN105278544A (en) * | 2015-10-30 | 2016-01-27 | 小米科技有限责任公司 | Control method and device of unmanned aerial vehicle |
| CN105527975A (en) * | 2015-12-09 | 2016-04-27 | 周润华 | Target tracking system based on UAV |
| CN105818977A (en) * | 2016-03-29 | 2016-08-03 | 马骏 | Novel ultrasonic detection unmanned aerial vehicle based on Internet of Things |
| CN105867361A (en) * | 2016-04-18 | 2016-08-17 | 深圳市道通智能航空技术有限公司 | Method and device for flight direction control and unmanned aerial vehicle thereof |
| CN105857593A (en) * | 2016-05-16 | 2016-08-17 | 苏州金建达智能科技有限公司 | Four-rotor multipurpose flying robot |
| WO2017075678A1 (en) * | 2015-11-05 | 2017-05-11 | Elio Tecnologia, Serviços E Participações Ltda. | Unmanned ellipsoid aircraft and corresponding construction method |
| CN106741892A (en) * | 2016-12-05 | 2017-05-31 | 广西大学 | A kind of many rotor aerial photography aircrafts |
| CN106892110A (en) * | 2015-12-21 | 2017-06-27 | 深圳市鼎创旭飞科技有限公司 | Police public address system |
| CN107108030A (en) * | 2016-09-21 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN108064209A (en) * | 2017-04-26 | 2018-05-22 | 深圳市大疆创新科技有限公司 | Unmanned vehicle |
| US10710711B2 (en) | 2016-09-21 | 2020-07-14 | SZ DJI Technology Co., Ltd. | Systems and methods for UAV sensor placement |
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- 2015-02-14 CN CN201520106371.8U patent/CN204452931U/en not_active Expired - Fee Related
Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105045281A (en) * | 2015-08-13 | 2015-11-11 | 深圳一电科技有限公司 | Unmanned aerial vehicle flight control method and device |
| CN105182348A (en) * | 2015-09-10 | 2015-12-23 | 浙江江宇电机有限公司 | Ultrasonic-wave-based unmanned plane real time positioning and tracking device and application technology of the same |
| CN105204520A (en) * | 2015-09-17 | 2015-12-30 | 深圳市十方联智科技有限公司 | Method for controlling unmanned aerial vehicle |
| CN105204520B (en) * | 2015-09-17 | 2018-07-06 | 深圳市十方联智科技有限公司 | A kind of control method of unmanned vehicle |
| CN105278544B (en) * | 2015-10-30 | 2018-05-08 | 小米科技有限责任公司 | The control method and device of unmanned vehicle |
| CN105235912A (en) * | 2015-10-30 | 2016-01-13 | 深圳高启科技有限公司 | Aerial photography collection unmanned aerial vehicle for law enforcement of police fire protection and control method thereof |
| CN105278544A (en) * | 2015-10-30 | 2016-01-27 | 小米科技有限责任公司 | Control method and device of unmanned aerial vehicle |
| US11999460B2 (en) | 2015-11-05 | 2024-06-04 | Elio Tecnologia Servicos E Particip | Unmanned ellipsoid multi-rotor airship and respective method of construction |
| US10919610B2 (en) | 2015-11-05 | 2021-02-16 | Elio Tecnologia, Serviços E Participaçoes Ltda. | Unmanned ellipsoid multi-rotor airship and respective method of construction |
| WO2017075678A1 (en) * | 2015-11-05 | 2017-05-11 | Elio Tecnologia, Serviços E Participações Ltda. | Unmanned ellipsoid aircraft and corresponding construction method |
| CN105527975A (en) * | 2015-12-09 | 2016-04-27 | 周润华 | Target tracking system based on UAV |
| CN106892110A (en) * | 2015-12-21 | 2017-06-27 | 深圳市鼎创旭飞科技有限公司 | Police public address system |
| CN105818977B (en) * | 2016-03-29 | 2018-10-26 | 泉州台商投资区华林设计有限公司 | Ultrasonic detection unmanned aerial vehicle based on Internet of things |
| CN105818977A (en) * | 2016-03-29 | 2016-08-03 | 马骏 | Novel ultrasonic detection unmanned aerial vehicle based on Internet of Things |
| CN105867361A (en) * | 2016-04-18 | 2016-08-17 | 深圳市道通智能航空技术有限公司 | Method and device for flight direction control and unmanned aerial vehicle thereof |
| US11117662B2 (en) | 2016-04-18 | 2021-09-14 | Autel Robotics Co., Ltd. | Flight direction display method and apparatus, and unmanned aerial vehicle |
| CN105857593A (en) * | 2016-05-16 | 2016-08-17 | 苏州金建达智能科技有限公司 | Four-rotor multipurpose flying robot |
| CN107108030A (en) * | 2016-09-21 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| US10710711B2 (en) | 2016-09-21 | 2020-07-14 | SZ DJI Technology Co., Ltd. | Systems and methods for UAV sensor placement |
| CN106741892A (en) * | 2016-12-05 | 2017-05-31 | 广西大学 | A kind of many rotor aerial photography aircrafts |
| CN106741892B (en) * | 2016-12-05 | 2019-06-28 | 广西大学 | A kind of more rotor aerial photography aircrafts |
| CN108064209A (en) * | 2017-04-26 | 2018-05-22 | 深圳市大疆创新科技有限公司 | Unmanned vehicle |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 515000 Shantou new industrial zone, Chenghai, Guangdong Patentee after: GUANGDONG CHENGXING UNMANNED AERIAL VEHICLE COMPANY LIMITED Address before: 515000 Shantou new industrial zone, Chenghai, Guangdong Patentee before: Guangdong Chengxing Modelairplane Science Company Limted |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150708 Termination date: 20190214 |
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| CF01 | Termination of patent right due to non-payment of annual fee |