CN205293058U - Conveniently carry on fixed wing uavs of jumbo size loading device - Google Patents
Conveniently carry on fixed wing uavs of jumbo size loading device Download PDFInfo
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- CN205293058U CN205293058U CN201620002462.1U CN201620002462U CN205293058U CN 205293058 U CN205293058 U CN 205293058U CN 201620002462 U CN201620002462 U CN 201620002462U CN 205293058 U CN205293058 U CN 205293058U
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- tailplane
- unmanned plane
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Abstract
The utility model relates to an unmanned aerial vehicle equipment technical field, in particular to conveniently carry on fixed wing uavs of jumbo size loading device, it includes the organism, and this organism includes fuselage, wing, tailplane, and fuselage both sides front portion is provided with the carbon pipe, is provided with the wing on this carbon pipe, and this wing trailing edge is provided with aileron and wing flap respectively, fuselage both sides rear portion is provided with tailplane, the last elevator that is provided with of tailplane, the afterbody is provided with vertical tail, the last rudder that is provided with of vertical tail, the fuselage is inside to be set up to two cabin sections, is load cabin, umbrella cabin by preceding in proper order after to, saves equipment compartment increasing load cabin bulk, it is not enough that it has solved unmanned aerial vehicle load cabin bulk, and jumbo size load unmanned aerial vehicle overall layout perfects the scheduling problem inadequately, has simple structure, and the space is bulky and easily assemble and advantage such as convenient maintenance.
Description
Technical field
This utility model relates to unmanned plane equipment technical field, particularly to a kind of convenient fixed-wing unmanned plane carrying large scale loading device.
Background technology
Unmanned plane is to carry out, by radio robot or airborne computer stored program controlled, the not manned vehicle that manipulates. Unmanned plane not only can complete the task that manned aircraft performs, and is more suitable for the task that people's aircraft should not perform.
Unmanned plane is as flying platform, multiple-task equipment can be carried, but owing to the microminiaturized process of industry special equipment is excessively slow, result in mission payload in the process that physics is installed and unmanned plane is required higher, the particularly bulk requirement to load cabin, and adopt plug-in pattern to be easy to task device is caused damage at the landing phases that takes off, exploitativeness is not strong, independent Increased Load cabin brings a degree of impact also can to the aerodynamic arrangement of complete machine, bring takeoff distance long, the problems such as flight attitude is steady not simultaneously.
Utility model content
The purpose of this utility model is in that the defect for prior art and deficiency, a kind of simple in construction is provided, a kind of convenient fixed-wing unmanned plane carrying large scale loading device reasonable in design, easy to use, it solve unmanned plane load cabin bulk not enough, the problems such as large scale load unmanned plane integral layout is perfect not, there is simple in construction, the advantages such as spatial volume is big and is easily assembled to and maintains easily.
For achieving the above object, the technical solution adopted in the utility model is:
A kind of convenient fixed-wing unmanned plane carrying large scale loading device described in the utility model, it includes body, and this body includes fuselage, wing, tailplane, and fuselage two forequarter is provided with carbon pipe, being provided with wing on this carbon pipe, this trailing edge is respectively arranged with aileron and wing flap; Rear portion, fuselage both sides is provided with tailplane, and tailplane is provided with elevator; Described afterbody is provided with vertical tail, and vertical tail is provided with rudder; Described fuselage interior is set to two cabin sections, is followed successively by load cabin, umbrella cabin from front to back, saves equipment compartment Increased Load cabin bulk; Described load cabin includes data radio station, automatic pilot, task device part, and load cabin inner bottom part is provided with fuel tank, and fuel tank is provided with automatic pilot, and automatic pilot front end is provided with data radio station; Described body front end is provided with engine mounting bracket, and this engine mounting bracket is provided with electromotor, and this electromotor is provided with propeller; The front portion of described body bottom surface arranges nose-gear installation position, is connected with nose-gear by bolt, and nose-gear is provided with front-wheel, and its bottom surface afterbody arranges guiding tail wheel.
After adopting said structure, this utility model has the beneficial effect that a kind of convenient fixed-wing unmanned plane carrying large scale loading device described in the utility model, it solve unmanned plane load cabin bulk not enough, the problems such as large scale load unmanned plane integral layout is perfect not, there is simple in construction, the advantages such as spatial volume is big and is easily assembled to and maintains easily.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is side structure schematic diagram of the present utility model.
Description of reference numerals:
1, propeller; 2, electromotor; 3, engine mounting bracket; 4, wing; 5, load cabin; 6, umbrella cabin; 7, tailplane; 8, vertical tail; 9, rudder; 10, tail wheel; 11, carbon pipe; 12, nose-gear; 13, front-wheel; 14, wing flap; 15, aileron; 16, data radio station; 17, automatic pilot; 18, fuel tank; 19, elevator.
Detailed description of the invention
Below in conjunction with accompanying drawing, this utility model is further described.
As shown in Figure 1 and Figure 2, a kind of convenient fixed-wing unmanned plane carrying large scale loading device described in the utility model, it includes body, this body includes fuselage, wing 4, tailplane 7, fuselage two forequarter is provided with carbon pipe 11, being provided with wing 4 on this carbon pipe 11, on this wing 4, medial surface is respectively arranged with aileron 15 and wing flap 14; Rear portion, fuselage both sides is provided with tailplane 7;
Rear portion, described fuselage both sides is provided with tailplane 7, and tailplane 7 is provided with elevator 19;
Described afterbody is provided with vertical tail 8, and vertical tail 8 is provided with rudder 9;
Described fuselage interior is set to two cabin sections, is followed successively by load cabin 5, umbrella cabin 6 from front to back, saves equipment compartment Increased Load cabin 5 bulk; Described load cabin 5 includes data radio station 16, automatic pilot 17, task device part, and load cabin 5 inner bottom part is provided with fuel tank 18, and fuel tank 18 is provided with automatic pilot 17, and automatic pilot 17 front end is provided with data radio station 16;
Described body front end is provided with engine mounting bracket 3, and this engine mounting bracket 3 is provided with electromotor 2, and this electromotor 2 is provided with propeller 1;
The front portion of described body bottom surface arranges nose-gear installation position, is connected with nose-gear 12 by bolt, and nose-gear 12 is provided with front-wheel 13, and its bottom surface afterbody arranges guiding tail wheel 10.
Equipment compartment in fuselage in design, is removed by this utility model, only retains load cabin and Liang Ge storehouse, umbrella cabin, so that greatly add space, load cabin, meets the social requirement for load cabin large space instantly.
In this utility model: body adopts fixed-wing normal arrangement, body includes adopting bolt and the fuselage of carbon pipe connection, wing, tailplane; Fuselage interior is divided into two cabin sections, it is followed successively by load cabin, umbrella cabin from front to back, data radio station, automatic pilot and task device are partially installed in load cabin, automatic pilot is arranged in load cabin the top of fuel tank, electromotor and propeller are arranged in the mounting seat of body front end, are connected with body by engine mounting bracket. Fore-body arranges nose-gear installation position, is connected with nose-gear by bolt, and afterbody arranges guiding tail wheel.
Aircraft dismounts according to fuselage, wing, tailplane, is fixed by carbon pipe and screw between fuselage, wing, tailplane, ensures stability and the safety of aircraft to greatest extent, aileron, wing flap, elevator, rudder steering wheel be placed in body. Elevator deflecting facet controls the pitch attitude of aircraft, and aileron control surface deflection controls the roll attitude of aircraft, and rudder surface controls the course of aircraft. Design flight speed 15m/s��35m/s, designs flying height 100m��5000m. Aircraft handling performance is high, and to handling, hands skill set requirements is low, is more easy to operation.
Dynamical system has mainly comprised gasoline type piston engine, wooden constant pitch airscrew and fuel tank, gasoline type piston engine and wooden constant pitch airscrew are arranged in the mounting seat of body front end, it is connected with body by engine mounting bracket, centre arranges fire wall, the impact of aircraft is preferably minimized by engine vibration, wooden constant pitch airscrew is pulling force oar, and fuel tank is the ABS engineering plastics fuel tank of customization, provides enough fuel oils for electromotor.Electromotor is gasoline type piston engine, and under enough pulling force, unmanned plane both can rolling start, it is possible to catapult-assisted take-off, and in combination with the layout of aircraft, distance of taking off only needs 50m��100m, hence it is evident that be better than the unmanned plane of same type. The dynamical system of this unmanned plane is simple to operate, easy to maintenance, and the flight preparation time is short, it is possible to rapidly enter aerial mission state.
Remote controller and automatic pilot are Flight Control Section, remote controller is for closely intervention to the adjustment of flight attitude and emergency case, especially the takeoff and landing stage, during use, freely switching between remote manual control state and automatic Pilot state can be completed by remote controller. Automatic pilot is arranged on above fuel tank, possess automatic Pilot and Autonomous Control unmanned plane function, adopt PID control method, by the control signal that the ground remote control information retrieval of data link transmission is correct, to 3 to acceleration, 3 be received to the data of gyro data, baroceptor and navigator collection and feed back to ground control station. Control program adopts the angle of attack to control the height of unmanned plane, and elevator controls the angle of attack of unmanned plane, the speed of Throttle Opening Control unmanned plane. Crosswise joint adopts elevon combination control mode, and after deviation occur in the flight route point of unmanned plane and the way point of setting, aileron exports, by control rate, the gradient that rudder amount makes unmanned plane maintenance fixing, and elevator keeps the height of unmanned plane. In unmanned plane take-off process, automatic pilot can take off by Autonomous Control unmanned aerial vehicle ejecting, flight course sends instruction according to the task route planned in advance to actuator, control actuator and perform corresponding task, and change and the planning of flight path route can be carried out in real time according to actual task demand, operator can carry out the control execution of more important task business by trajectory planning and path adjustment, autonomous flight can be carried out by the prebriefed pattern that mission requirements is arranged in advance, complete the data acquisition to mission area by Autonomous Control task device and work. Earth station can show the electronic chart of flight range, flight path, flight parameter, aspect etc. in unmanned plane during flying process, all parameters and number boat data can be downloaded in real time in-flight, task complete after by prebriefed pattern autonomous flight to predetermined drop zone, and Autonomous Control unmanned plane releases a parachute stable landing, additionally needing, by remote controller, airborne automatic pilot is switched back into remote state also dependent on actual space enrironment and use, visual control unmanned plane carries out sliding landing.
On-board data transmission radio station is installed in fuselage load cabin, and the number of on-board data transmission radio station passes antenna and adopts columnar antenna.
Payload portion can adopt multiple low-altitude remote sensing equipment, such as video camera, camera, EO-1 hyperion, miniSAR etc.
Completing taking off of unmanned plane by sliding to run or launch two ways, when rolling start, unmanned plane is mainly completed unmanned plane Non-follow control by ground system, is switched to automatic navigation mode after unmanned plane rises to safe altitude. Completed the autonomous flight control in unmanned plane preplanned mission course line by navigation control system, arrive mission area and obtain remotely-sensed data. Can realize independently taking off simultaneously, rely on launching cradle to complete unmanned plane and take off. Unmanned plane can complete the application of different field by carrying different mission payload equipment, performs corresponding task.
Way of recycling can adopt parachuting and downhill race two ways, adopts the way point of automatic pilot to arrange in advance, it is possible to is set as that arrival set point coordinate can release a parachute and stops electromotor simultaneously.Adopting tail wheel type landing gear, nose-gear installs pulley, and afterbody installs guiding tail wheel, controls the unmanned plane direction of motion on ground, and undercarriage is processed with 6061 aluminiums for main material, adopts arc-shaped shock-absorbing structure, completes the aircraft grounding by skidding.
It is as shown in the table for its total technical index:
The advantage that this utility model is different from tradition unmanned plane is as follows:
1) the multiple industry requirements such as emergency monitoring, geographical mapping, environmental conservation, oil line walking can, be met, especially for carrying the light-duty loading device of large scale, highly versatile, practicality are high, and safety, reliability, stationary performance are good, have installation, use, the feature such as easy to maintenance;
2) this takes charge of practical experience for many years, and industrial advantages are obvious, and less costly, it is easy to marketing.
A kind of convenient fixed-wing unmanned plane carrying large scale loading device described in the utility model, it solve unmanned plane load cabin bulk not enough, the problems such as large scale load unmanned plane integral layout is perfect not, there is simple in construction, the advantages such as spatial volume is big and is easily assembled to and maintains easily.
The above is only better embodiment of the present utility model, therefore all equivalences done according to the structure described in this utility model patent claim, feature and principle change or modify, and are all included in this utility model patent claim.
Claims (1)
1. the convenient fixed-wing unmanned plane carrying large scale loading device, it includes body, and this body includes fuselage, wing, tailplane, and fuselage two forequarter is provided with carbon pipe, and this carbon pipe is provided with wing, and this trailing edge is respectively arranged with aileron and wing flap; Rear portion, fuselage both sides is provided with tailplane, and tailplane is provided with elevator; Described afterbody is provided with vertical tail, and vertical tail is provided with rudder; It is characterized in that: described fuselage interior is set to two cabin sections, be followed successively by load cabin, umbrella cabin from front to back, save equipment compartment Increased Load cabin bulk; Described load cabin includes data radio station, automatic pilot, task device part, and load cabin inner bottom part is provided with fuel tank, and fuel tank is provided with automatic pilot, and automatic pilot front end is provided with data radio station; Described body front end is provided with engine mounting bracket, and this engine mounting bracket is provided with electromotor, and this electromotor is provided with propeller; The front portion of described body bottom surface arranges nose-gear installation position, is connected with nose-gear by bolt, and nose-gear is provided with front-wheel, and its bottom surface afterbody arranges guiding tail wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620002462.1U CN205293058U (en) | 2016-01-05 | 2016-01-05 | Conveniently carry on fixed wing uavs of jumbo size loading device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620002462.1U CN205293058U (en) | 2016-01-05 | 2016-01-05 | Conveniently carry on fixed wing uavs of jumbo size loading device |
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| CN205293058U true CN205293058U (en) | 2016-06-08 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201620002462.1U Expired - Fee Related CN205293058U (en) | 2016-01-05 | 2016-01-05 | Conveniently carry on fixed wing uavs of jumbo size loading device |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105974494A (en) * | 2016-07-14 | 2016-09-28 | 无锡信大气象传感网科技有限公司 | Radio-sondage system based on dual-redundancy fixed wing unmanned aerial vehicle |
| CN106094057A (en) * | 2016-07-14 | 2016-11-09 | 无锡信大气象传感网科技有限公司 | A kind of radio sounding system based on fixed-wing unmanned plane |
| CN108146611A (en) * | 2017-12-22 | 2018-06-12 | 中山市得高行知识产权中心（有限合伙） | A kind of portable agricultural formula unmanned plane and its application method |
-
2016
- 2016-01-05 CN CN201620002462.1U patent/CN205293058U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105974494A (en) * | 2016-07-14 | 2016-09-28 | 无锡信大气象传感网科技有限公司 | Radio-sondage system based on dual-redundancy fixed wing unmanned aerial vehicle |
| CN106094057A (en) * | 2016-07-14 | 2016-11-09 | 无锡信大气象传感网科技有限公司 | A kind of radio sounding system based on fixed-wing unmanned plane |
| CN108146611A (en) * | 2017-12-22 | 2018-06-12 | 中山市得高行知识产权中心（有限合伙） | A kind of portable agricultural formula unmanned plane and its application method |
| CN108146611B (en) * | 2017-12-22 | 2022-03-11 | 中山市得高行知识产权中心（有限合伙） | Portable agricultural unmanned aerial vehicle and use method thereof |
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| Date | Code | Title | Description |
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| 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: 20160608 Termination date: 20200105 |
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| CF01 | Termination of patent right due to non-payment of annual fee |