CN104085529A - Eight-rotor-wing unmanned plane system - Google Patents
Eight-rotor-wing unmanned plane system Download PDFInfo
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- CN104085529A CN104085529A CN201410371722.8A CN201410371722A CN104085529A CN 104085529 A CN104085529 A CN 104085529A CN 201410371722 A CN201410371722 A CN 201410371722A CN 104085529 A CN104085529 A CN 104085529A
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Abstract
The invention discloses an eight-rotor-wing unmanned plane system, which relates to the technical field of an unmanned plane. The eight-rotor-wing unmanned plane system comprises a plane body, a remote measuring device, a ground workstation, propellers, a lithium battery, rotor wing supports, brushless motors, an autostability cradle head system, a flight control system and an image transmitting system, wherein the plane body is uniformly provided with a plurality of rotor wing supports, the end part of each rotor wing support is connected with the corresponding propeller through the corresponding brushless motor and an electronic speed controller system, the lithium battery is arranged above the plane body, the flight control system and the image transmitting system are arranged below the plane body through the autostability cradle head system, and the inner sides of the rotor wing supports on two sides of the plane body are respectively provided with an unmanned plane supporting frame; the flight control system is connected with the remote measuring device, the remote measuring device is connected with the ground workstation, and the ground workstation is also connected with the autostability cradle head system, the flight control system and the image transmitting system. The eight-rotor-wing unmanned plane system has the characteristics of large carrying capacity, long durability, small size, light weight, small target feature, rapidness, mobility and flexibility in use, convenience in operation, application and maintenance and the like and can independently execute an electric power inspection task as an independent system.
Description
Technical field
What the present invention relates to is unmanned plane technical field, is specifically related to a kind of eight rotor wing unmanned aerial vehicle systems.
Background technology
Current domestic rotor wing unmanned aerial vehicle, some volumes are larger, can load-carrying larger, but price and oil are moving, fly and within fifties hours, just have carbon distribution, need to clear up, and maintenance cost is very expensive; Four rotor wing unmanned aerial vehicles that some is small-sized, although the bodily form is less, load-carrying is also very little, only has 500-1000 gram, is difficult to meet current demand, stationarity and the ease for operation of flight all have much room for improvement.
in sum, the load-carrying of current existing unmanned plane is little, and cruise duration is short, and target property is large, uses inconvenience, operates also more complicated, can not independently carry out electric inspection process task.
Summary of the invention
For the deficiency existing in prior art, the present invention seeks to be to provide a kind of eight rotor wing unmanned aerial vehicle systems, have that load carrying ability is large, cruise duration is long, volume is little, lightweight, target property is little, use quick, maneuverability, operation is used and keep in repair the features such as easy, the independent electric inspection process task of carrying out of establishing one's own system.
To achieve these goals, the present invention realizes by the following technical solutions: eight rotor wing unmanned aerial vehicle systems, comprise body, telemetry equipment, surface work station, screw propeller, lithium cell, rotor support, brushless motor, increase steady The Cloud Terrace system, flight control system and image transmission system, on body, be evenly equipped with a plurality of rotor supports, rotor bracket end is connected with screw propeller by brushless motor and electric operation dispatching system, body top is provided with lithium cell, body below is provided with flight control system and image transmission system by increasing steady The Cloud Terrace system, and the rotor support of body both sides inner side is provided with unmanned plane bracing frame, described flight control system is connected with telemetry equipment, and telemetry equipment is connected with surface work station, and surface work station is also connected with image transmission system with the steady The Cloud Terrace system of increasing, flight control system.
As preferably, described surface work station comprises control system, power supply, charger, voltage and current detecting device, video display unit (VDU), airborne equipment controls transmitter, ground station's computer, wireless video receiver, joy stick function switch and data receiver, control system respectively with power supply, video display unit (VDU), airborne equipment controls transmitter, ground station's computer is connected, power supply respectively with charger, voltage and current detecting device is connected, video display unit (VDU), airborne equipment controls transmitter, ground station's computer respectively with wireless video receiver, joy stick function switch is connected with data receiver.
As preferably, the steady The Cloud Terrace system of described increasing comprises airborne attitude sensor, micro controller system, servo drive, Z axis angular adjustment apparatus, X-axis angular adjustment apparatus and Y-axis angular adjustment apparatus, airborne attitude sensor is connected with servo drive by micro controller system, and servo drive is connected with Z axis angular adjustment apparatus, X-axis angular adjustment apparatus and Y-axis angular adjustment apparatus respectively.Described micro controller system is for receiving the data of airborne attitude sensor, these data of union obtain servo-drive information, and this servo-drive information is passed to servo drive, by servo drive, drive corresponding X-axis angular adjustment apparatus, Y-axis angular adjustment apparatus and Z axis angular adjustment apparatus.
Beneficial effect of the present invention:
1, aircraft has remote control, autonomous flight ability, can real time modifying flight air route and task setting;
2, observing and controlling and information transmission equipment have the function of remote control, real time information transmission, have multimachine, the compatible work of multistation and certain anti-intercepting and capturing, antijamming capability;
3, reconnaissance mission equipment Real-time Obtaining target image information round the clock, has manually, automatic control operation mode, can find rapidly, catches, identification, tracking target;
4, flight is controlled with information processing station and is had the function that aircraft is carried out remote control distributor and airborne task device is controlled, and has the demonstration of flight parameter/flight path, routeing and real time modifying flight planning, resets the ability of task pattern; There is the ability that realizes the first viewing angle control flight by video; Have the abilities such as the video standard signal of reception, processing/memory image, data stack in real time, have the ability that target positioning and guiding are hit, Qie Nengyu higher level commanding agency, information handling center and command echelon interlink;
5, ground handling equipment has the ability of simple detection, maintenance and training, has the function of quick-replaceable consumable accessory, reserve power battery pack and bimodal charging;
6, launch rapidly in total system outfield, has vehicle-mounted motor-driven and portable ability on a large scale.
Accompanying drawing explanation
Below in conjunction with the drawings and specific embodiments, describe the present invention in detail;
Fig. 1 is structural representation of the present invention;
Fig. 2 is the structure schematic diagram of the body in the present invention;
Fig. 3 is the control block diagram at surface work of the present invention station;
Fig. 4 is the structured flowchart of the steady The Cloud Terrace system of increasing of the present invention.
The specific embodiment
For technological means, creation characteristic that the present invention is realized, reach object and effect is easy to understand, below in conjunction with the specific embodiment, further set forth the present invention.
With reference to Fig. 1-4, this specific embodiment is by the following technical solutions: eight rotor wing unmanned aerial vehicle systems, comprise body 1, telemetry equipment 2, surface work station 3, screw propeller 4, lithium cell 5, rotor support 6, brushless motor 7, increase steady The Cloud Terrace system 8, flight control system 9 and image transmission system 10, on body 1, be evenly equipped with a plurality of rotor supports 6, rotor support 6 ends are connected with screw propeller 4 by brushless motor 7 and electric operation dispatching system, body 1 top is provided with lithium cell 5, body 1 below is provided with flight control system 9 and image transmission system 10 by increasing steady The Cloud Terrace system 8, and rotor support 6 inner sides of body 1 both sides are provided with unmanned plane bracing frame, described flight control system 9 is connected with telemetry equipment 2, and telemetry equipment 2 is connected with surface work station 3, and surface work station 3 is also connected with image transmission system 10 with the steady The Cloud Terrace system 8 of increasing, flight control system 9.
It should be noted that described electric operation dispatching system adopts discrete design, each components and parts adopt Integration Design, have that volume is little, lightweight, pig-tail wire and an advantage such as weld nugget is few, the life-span is long, reliability is high, performance is good.
Described housing construction adopts advanced composite material, material selection U.S. DuPont company high-strength carbon fiber synthetic material and 7075 aviation aluminum alloy materials, 7075 aerolite tensile strength >=560MPa.Housing construction is intended adopting tower structure, has guaranteed that housing construction is firm.
Described surface work station 3 adopt high-strength engineering plastics as housing, firmly resistance toly fall, good waterproof performance, be adapted at field and carry out operation.Screen adopts 17 cun of high brightness liquid crystal displays.Configuration High Performance industrial grade calculates core.Built-in high-sensitivity digital receiver.Adopt directed satellite automatic follow-up antenna system.Support the operations such as control lever and keyboard.
The steady The Cloud Terrace system 8 of described increasing can be carried out X/Y/Z tri-axles and be controlled and the stable unmanned plane Self-stabilization holder of automatic horizontal, comprise airborne attitude sensor, the micro controller system being connected with described airborne attitude sensor, the servo drive being connected with described micro controller system, the X-axis angular adjustment apparatus being driven by described servo drive, Y-axis angular adjustment apparatus and Z axis angular adjustment apparatus; Described micro controller system is for receiving the data of airborne attitude sensor, these data of union obtain servo-drive information, and this servo-drive information is passed to servo drive, by servo drive, drive corresponding X-axis angular adjustment apparatus, Y-axis angular adjustment apparatus and Z axis angular adjustment apparatus.The unmanned plane Self-stabilization holder of this specific embodiment, makes ground staff make airborne equipment (as high definition camera, pick up camera etc.) carry out the motion of X-axis/Y-axis/Z axis by ground control equipment pair, makes it reach the accuracy in degree of stability and the orientation of image.
Described image transmission system 9 adopts NEX-5 slr camera.
The unmanned plane of this specific embodiment is coated shell design entirely, can effectively stop sand bed, misty rain impact.The key positions such as motor are done to waterproof sand prevention to be processed.The blank areas such as electric wire are adopted to waterproof joint.To flying to control control capsule, install seal ring etc. additional.Degree of protection reaches IP45.
The telemetry equipment 2 of this specific embodiment has following feature:
Succinct, traditional display interface with style is set.Have " System menu ", " associated menu ", etc. complicated menu level arrange, all functions are divided into " BASIC(base menu) " and " ADVANCE(advanced menu) ", this is identical with the look & feel of the existing equipments such as FF9, the content of some function setting item and display format almost do not become, and this design makes the easier left-hand seat of old user.
2. the many basic function that have telecommand equipment of new generation.10C carries out the product of Systematic Design from new height, and is not only the simple upgrade of old 9 channel units.Very detailed etc. such as can select, remain emphatic on the Premium Features such as application " flying condition " between PCM standard and FASST2. 4G standard, to the classification of aircraft rudder surface and mixing.In use, you can experience its fusion just as equipment of new generation and last generation really, under new standard, designing, is not indispensable content but removed complicated, obscure menu and PCM2048 like this, thereby has reduced cost, accelerated the speed that data are inputted.
This specific embodiment is selected autonomous driving equipment, greatly improves and flies to control stability.Portability multiple-task load.Can be used for carrying out the multiple air taskings such as Data acquisition,, measurement, detection, investigation, in electric inspection process field, can bring into play its efficient, disguised strong feature, can carry out distant surveillance to object.
More than show and described groundwork of the present invention and principal character and advantage of the present invention.The technical personnel of the industry should be understood; the present invention is not restricted to the described embodiments; that in above-described embodiment and specification sheets, describes just illustrates principle of the present invention; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements all fall in the claimed scope of the invention.The claimed scope of the present invention is defined by appending claims and equivalent thereof.
Claims (6)
1. eight rotor wing unmanned aerial vehicle systems, it is characterized in that, comprise body (1), telemetry equipment (2), surface work station (3), screw propeller (4), lithium cell (5), rotor support (6), brushless motor (7), increase steady The Cloud Terrace system (8), flight control system (9) and image transmission system (10), on body (1), be evenly equipped with a plurality of rotor supports (6), rotor support (6) end is connected with screw propeller (4) by brushless motor (7) and electric operation dispatching system, body (1) top is provided with lithium cell (5), body (1) below is provided with flight control system (9) and image transmission system (10) by increasing steady The Cloud Terrace system (8), and the rotor support (6) of body (1) both sides inner side is provided with unmanned plane bracing frame, described flight control system (9) is connected with telemetry equipment (2), telemetry equipment (2) is connected with surface work station (3), and surface work station (3) are also connected with image transmission system (10) with increasing steady The Cloud Terrace system (8), flight control system (9).
2. eight rotor wing unmanned aerial vehicle systems according to claim 1, it is characterized in that, described surface work station (3) comprises control system (31), power supply (32), charger (33), voltage and current detecting device (34), video display unit (VDU) (35), airborne equipment controls transmitter (36), ground station's computer (37), wireless video receiver (38), joy stick function switch (39) and data receiver (310), control system (31) respectively with power supply (32), video display unit (VDU) (35), airborne equipment controls transmitter (36), ground station's computer (37) is connected, power supply (32) respectively with charger (33), voltage and current detecting device (34) is connected, video display unit (VDU) (35), airborne equipment controls transmitter (36), ground station's computer (37) respectively with wireless video receiver (38), joy stick function switch (39) is connected with data receiver (310).
3. eight rotor wing unmanned aerial vehicle systems according to claim 1, it is characterized in that, the steady The Cloud Terrace system of described increasing (8) comprises airborne attitude sensor (81), micro controller system (82), servo drive (83), Z axis angular adjustment apparatus (84), X-axis angular adjustment apparatus (85) and Y-axis angular adjustment apparatus (86), airborne attitude sensor (81) is connected with servo drive (83) by micro controller system (82), servo drive (83) respectively with Z axis angular adjustment apparatus (84), X-axis angular adjustment apparatus (85) is connected with Y-axis angular adjustment apparatus (86).Described micro controller system (82) is for receiving the data of airborne attitude sensor (81), these data of union obtain servo-drive information, and this servo-drive information is passed to servo drive (83), by servo drive (83), drive corresponding X-axis angular adjustment apparatus (85), Y-axis angular adjustment apparatus (83) and Z axis angular adjustment apparatus (84).
4. eight rotor wing unmanned aerial vehicle systems according to claim 1, is characterized in that, described electric operation dispatching system adopts separated structure.
5. eight rotor wing unmanned aerial vehicle systems according to claim 1, is characterized in that, described body (1) adopts advanced composite material, material selection U.S. DuPont company high-strength carbon fiber synthetic material and 7075 aviation aluminum alloy materials.
6. eight rotor wing unmanned aerial vehicle systems according to claim 1, is characterized in that, described surface work station (3) adopt high-strength engineering plastic as housing, firmly resistance toly fall, good waterproof performance, be adapted at field and carry out operation; Screen adopts 17 cun of high brightness liquid crystal displays.Configuration High Performance industrial grade calculates core; Built-in high-sensitivity digital receiver; Adopt directed satellite automatic follow-up antenna system; Support the operations such as control lever and keyboard.
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| CN201410371722.8A CN104085529A (en) | 2014-07-31 | 2014-07-31 | Eight-rotor-wing unmanned plane system |
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| CN201410371722.8A CN104085529A (en) | 2014-07-31 | 2014-07-31 | Eight-rotor-wing unmanned plane system |
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| CN104317288A (en) * | 2014-10-22 | 2015-01-28 | 陕西亿美万泰科技有限公司 | Unmanned aerial vehicle system for police multipurpose surveillance |
| CN104407607A (en) * | 2014-10-15 | 2015-03-11 | 天津全华时代航天科技发展有限公司 | Unmanned aerial vehicle first-person perspective control system |
| CN104554716A (en) * | 2015-01-27 | 2015-04-29 | 深圳雷柏科技股份有限公司 | Split type unmanned aerial vehicle |
| CN105388795A (en) * | 2015-12-18 | 2016-03-09 | 天津光电通信技术有限公司 | Miniaturized man-machine interaction system |
| CN106708093A (en) * | 2017-01-17 | 2017-05-24 | 广东容祺智能科技有限公司 | Multistage intelligent unmanned aerial vehicle (UAV) throwing system |
| CN110265792A (en) * | 2018-03-12 | 2019-09-20 | 杭州海康威视数字技术股份有限公司 | Antenna assembly and unmanned plane |
| TWI701190B (en) * | 2015-03-12 | 2020-08-11 | 美商奈庭吉爾智慧系統公司 | Automated drone security systems |
| CN113345123A (en) * | 2021-06-07 | 2021-09-03 | 国网四川省电力公司检修公司 | Unmanned aerial vehicle-based power transmission line inspection system for alpine and high-altitude areas |
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| CN113345123A (en) * | 2021-06-07 | 2021-09-03 | 国网四川省电力公司检修公司 | Unmanned aerial vehicle-based power transmission line inspection system for alpine and high-altitude areas |
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Address after: 264003 Shandong city of Yantai province high tech Zone eight road No. 17 Mashan Street Applicant after: Shandong Chuanghui Electronic Technology Co., Ltd. Address before: 264003 Shandong city of Yantai province high tech Zone eight road No. 17 Mashan Street Applicant before: SHANDONG CHUANGHUI ELECTRONIC SCIENCE & TECHNOLOGY CO., LTD. |
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