CN205440848U - Unmanned aerial vehicle of folded cascade horn, cabin constancy of temperature - Google Patents
Unmanned aerial vehicle of folded cascade horn, cabin constancy of temperature Download PDFInfo
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- CN205440848U CN205440848U CN201620154979.2U CN201620154979U CN205440848U CN 205440848 U CN205440848 U CN 205440848U CN 201620154979 U CN201620154979 U CN 201620154979U CN 205440848 U CN205440848 U CN 205440848U
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Abstract
The utility model relates to an unmanned air vehicle technique field is an unmanned aerial vehicle of folded cascade horn, cabin constancy of temperature particularly, including the host computer fuselage, two parts about the host computer fuselage divide into, shang mian the part is for controlling the cabin, lower portion is the constant temperature machine cabin, connect a plurality of collapsible carbon fiber tube horns on the host computer fuselage, collapsible carbon fiber tube horn is Y shape, the host computer fuselage is connected to the collapsible carbon fiber tube horn of Y shape bottom one end, two ends at the Y collapsible carbon fiber tube horn top of shape are equipped with two motors that have the screw respectively, the collapsible carbon fiber tube horn cross section of Y shape is the point of rotation, two support arms at the Y collapsible carbon fiber tube horn top of shape can be folding to the inboard along the point of rotation. The utility model discloses can be to the folding of many rotors horn, the transportation is convenient, monitors cabin real -time temperature through temperature detection module to improve unmanned aerial vehicle flight efficiency.
Description
[technical field]
This utility model relates to unmanned air vehicle technique field, a kind of folding horn, the unmanned plane of cabin temperature constant.
[background technology]
Unmanned plane is the most manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself.Unmanned plane correlation technique develops rapidly both at home and abroad, and UAS is of a great variety, the wide distinct characteristics of purposes, causes it when size, quality, voyage, boat, flying height, flight speed, and task dispatching many-side has larger difference.Gyroplane is a vitals of unmanned plane, but under normal circumstances gyroplane always to there is structure the compactest, oversize, it has not been convenient to carry out carrying the situation of transport.For this situation, a lot of unmanned planes are all to realize folding and launching by fixed disassembly screw, however it is necessary that the instrument of carrying with, for carrying and using the most very inconvenient, and screw is easily lost or stripped thread through being dismounted for multiple times, it is likely that the security performance of aircraft can be affected.For multiaxis gyroplane, heat radiation insulation is also a problem needing to consider, seldom can consider heat radiation and be incubated and process fairly perfect in existing body designs.Current most many rotors have the highest requirement to weight and the rigidity of frame, because this is bigger on flight efficiency and the flight safety impact of many rotors.
The blade of the most many rotors in market is installed in above motor, and in flight course, motor can have certain inhibition to downward air-flow, thus has a certain impact the flight efficiency of many rotors.Owing to unmanned plane is that battery and control system are placed on same layer, number of modules battery to be walked around cabling, the capacity of resisting disturbance causing modules is more weak.
[utility model content]
This utility model is that, anti-electromagnetic interference capability, body inconvenient to carry for above-mentioned multiaxis gyroplane dispel the heat the low problem of the bad flight efficiency caused, and a kind of convenient transportation of research and development, saves space, folding horn, can keep the unmanned plane of cabin temperature constant.
To achieve these goals, a kind of folding horn of design, the unmanned plane of cabin temperature constant, including main machine body, main machine body is divided into upper and lower two parts, upper part is for controlling cabin, lower part is constant temperature cabin, some collapsible carbon fiber pipe horns are connected on main machine body, collapsible carbon fiber pipe horn is Y-shaped, Y shape collapsible carbon fiber pipe horn bottom end connects main machine body, two, top of Y shape collapsible carbon fiber pipe horn end is respectively equipped with two motors with propeller, Y shape collapsible carbon fiber pipe horn infall is the point of rotation, two, top of Y shape collapsible carbon fiber pipe horn support arm can be along the point of rotation to folded inside；Being provided with battery in described constant temperature cabin, be provided with control system in controlling cabin, battery and control system are respectively arranged at the levels of main machine body.
Constant temperature is provided with temperature detecting module in cabin, can monitor the temperature in constant temperature cabin in real time, and built-in temperature control system carries out real time control machine cabin temperature according to the rotating speed of desired temperature Yu the discrepancy adjustment fan of real time temperature.
The propeller of described motor is installed towards ground, and propeller is arranged on below motor.
Two support arm angles of described Y shape collapsible carbon fiber pipe horn are 120 °, and after folding, two support arms are respectively 60 ° with main shaft angle.
Main machine body is provided with undercarriage.
The cross point of Y shape collapsible carbon fiber pipe horn connects two support arms by linkwork.
Constant temperature cabin is by switch constant temperature machine cabin door loading and unloading battery, and controlling above cabin is GPS mounting seat, and thermostatic control cabin is additionally provided with vent.
This utility model compared with the existing technology, has an advantage in that:
1. many rotors horn can be folded, achieve the convenience of transport and idle time save space, the most do not lose the aesthetic property of self simultaneously, in the case of stretching, the angle of each branch of every Y type carbon fiber pipe becomes 120 degree, whole many rotor wing unmanned aerial vehicles are allowed to have preferable symmetry, after folding, two motor arms that Y type carbon fiber pipe stretches out and main shaft angle are within 60 degree；
2. on the one hand the design of the carbon of more than rotor horn effective Y type carbon pipe achieves the effect of folding, on the other hand also saves the weight of many fuselages itself in the case of the rigidity ensureing many rotors self, thus adds the load capacity of aircraft；
3. the modularized design of more than rotor fuselage, upper strata is for controlling cabin, and lower floor is battery flat; well arranged; body space can be more reasonably utilized, reduce body volume and weight, and fuselage space waste; many rotors heat dissipation channel is allowed more to optimize; the joint of unnecessary frequent plug is protected by fuselage modularized design, strengthens reliability when plugging plug, easy to loading and unloading; modular fuselage designs so that the anti-electromagnetic interference capability of whole flight control system strengthens；
4. the design in constant temperature cabin, by temperature detecting module to cabin real time temperature monitoring, and the control that temperature control system is to cabin real time temperature, as long as no matter allowing many rotors at which kind of environment in controlled range, can ensure that whole cabin is stable at intended optimum temperature, thus improve unmanned plane during flying efficiency；
5., by propeller being contained in the lower section of motor, relative to propeller being contained in its body that motor decreases the above resistance to prop-blast, flying required electric energy before decreasing aircraft, improve the flight efficiency of many rotors.
[accompanying drawing explanation]
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation after this utility model folds；
Fig. 3 is side view of the present utility model；
Fig. 4 is rearview of the present utility model；
In figure: 1. fuselage 2.GPS3. folding point 4. motor cabinet 5. propeller 6.Y type rotor arm 7 undercarriage 8. controls constant temperature machine cabin door 11. antenna 12. constant temperature cabin, constant temperature cabin 10., cabin 9. vent；
Specify Fig. 1 as this utility model Figure of abstract.
[detailed description of the invention]
The utility model is described in further detail below in conjunction with the accompanying drawings, and the structure of this device and principle are the most clearly for the people of this specialty.Should be appreciated that specific embodiment described herein, only in order to explain this utility model, is not used to limit this utility model.
As shown in Figures 1 to 4, many rotor wing unmanned aerial vehicles in this utility model include: many rotors horn 6, the cross point of each Y type carbon fiber pipe that fuselage 1 (being made up of control cabin 8 and constant temperature cabin 9), the folding Y type carbon fiber pipe of undercarriage 7, three form are to be linked together two with the carbon fiber pipe of propeller motor 4 by linkwork 3, realize folding reliably and launching, wherein constant temperature cabin by switch constant temperature machine cabin door 10 loading and unloading battery, control to be that GPS mounting seat 2, thermostatic control cabin are additionally provided with vent 12 above cabin 8.
Control cabin is integrated with control module substantially, including flying to control the modules such as plate, Voltage stabilizing module, number biography, figure biography, receiver, facilitates the integrated of many rotors whole system, the reliability of increase whole system.When many rotor wing unmanned aerial vehicles are in folded state, Y type carbon fiber pipe 6 surveys folding toward the carbon fiber pipe at two motor 4 places overhang at cross point 3 in fuselage 1.As Fig. 2 be these many rotor wing unmanned aerial vehicles folding after structure, fuselage both sides motor arm is the most parallel, greatly reduces the space shared by aircraft.
When many rotor wing unmanned aerial vehicles task to be performed when, 6 motor arms are flexed outward respectively, corrugated tubing outside by fastening carbon fiber pipe fastens the carbon fiber pipe at each motor helical oar place, as shown in figure Fig. 1, many rotor wing unmanned aerial vehicles when being extended configuration, by opening constant temperature machine cabin door 10, battery is put in.
Claims (7)
1. a folding horn, the unmanned plane of cabin temperature constant, including main machine body, it is characterized in that main machine body is divided into upper and lower two parts, upper part is for controlling cabin, lower part is constant temperature cabin, some collapsible carbon fiber pipe horns are connected on main machine body, collapsible carbon fiber pipe horn is Y-shaped, Y shape collapsible carbon fiber pipe horn bottom end connects main machine body, two, top of Y shape collapsible carbon fiber pipe horn end is respectively equipped with two motors with propeller, Y shape collapsible carbon fiber pipe horn infall is the point of rotation, two, top of Y shape collapsible carbon fiber pipe horn support arm can be along the point of rotation to folded inside；Being provided with battery in described constant temperature cabin, be provided with control system in controlling cabin, battery and control system are respectively arranged at the levels of main machine body.
A kind of folding horn the most as claimed in claim 1, the unmanned plane of cabin temperature constant, it is provided with temperature detecting module in it is characterized in that constant temperature cabin, can monitor the temperature in constant temperature cabin in real time, built-in temperature control system carries out real time control machine cabin temperature according to the rotating speed of desired temperature Yu the discrepancy adjustment fan of real time temperature.
A kind of folding horn the most as claimed in claim 1, the unmanned plane of cabin temperature constant, it is characterised in that the propeller of described motor is installed towards ground, and propeller is arranged on below motor.
A kind of folding horn the most as claimed in claim 1, the unmanned plane of cabin temperature constant, it is characterised in that two support arm angles of described Y shape collapsible carbon fiber pipe horn are 120 °, after folding, two support arms are respectively 60 ° with main shaft angle.
A kind of folding horn the most as claimed in claim 1, the unmanned plane of cabin temperature constant, it is characterised in that main machine body is provided with undercarriage.
A kind of folding horn the most as claimed in claim 1, the unmanned plane of cabin temperature constant, it is characterised in that the cross point of Y shape collapsible carbon fiber pipe horn connects two support arms by linkwork.
A kind of folding horn the most as claimed in claim 1, the unmanned plane of cabin temperature constant, it is characterised in that constant temperature cabin is by switch constant temperature machine cabin door loading and unloading battery, and controlling above cabin is GPS mounting seat, and thermostatic control cabin is additionally provided with vent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620154979.2U CN205440848U (en) | 2016-03-01 | 2016-03-01 | Unmanned aerial vehicle of folded cascade horn, cabin constancy of temperature |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620154979.2U CN205440848U (en) | 2016-03-01 | 2016-03-01 | Unmanned aerial vehicle of folded cascade horn, cabin constancy of temperature |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205440848U true CN205440848U (en) | 2016-08-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201620154979.2U Active CN205440848U (en) | 2016-03-01 | 2016-03-01 | Unmanned aerial vehicle of folded cascade horn, cabin constancy of temperature |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539811A (en) * | 2016-03-01 | 2016-05-04 | 上海东古航空科技有限公司 | UAV (unmanned aerial vehicle) provided with foldable arms and constant-temperature cabin |
| CN107284649A (en) * | 2017-07-16 | 2017-10-24 | 湖南高垅航空植保科技有限责任公司 | A kind of many rotor plant protection unmanned planes of Y types |
-
2016
- 2016-03-01 CN CN201620154979.2U patent/CN205440848U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539811A (en) * | 2016-03-01 | 2016-05-04 | 上海东古航空科技有限公司 | UAV (unmanned aerial vehicle) provided with foldable arms and constant-temperature cabin |
| CN107284649A (en) * | 2017-07-16 | 2017-10-24 | 湖南高垅航空植保科技有限责任公司 | A kind of many rotor plant protection unmanned planes of Y types |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 200120 1202A room, No. 570, midsummer Road, Zhangjiang Town, Shanghai, Pudong New Area Patentee after: Shanghai Donggu Intelligent Technology Co., Ltd. Address before: 200120 1202A room, No. 570, midsummer Road, Zhangjiang Town, Shanghai, Pudong New Area Patentee before: SHANGHAI DONGGU AVIATION TECHNOLOGY CO., LTD. |