CN204916189U - Rectilinear unmanned train's aircraft - Google Patents
Rectilinear unmanned train's aircraft Download PDFInfo
- Publication number
- CN204916189U CN204916189U CN201520432260.6U CN201520432260U CN204916189U CN 204916189 U CN204916189 U CN 204916189U CN 201520432260 U CN201520432260 U CN 201520432260U CN 204916189 U CN204916189 U CN 204916189U
- Authority
- CN
- China
- Prior art keywords
- strut bar
- aeroplane
- unmanned
- high low
- chest
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000005855 radiation Effects 0.000 claims abstract description 8
- 239000000203 mixture Substances 0.000 claims description 2
- 239000002917 insecticide Substances 0.000 abstract description 3
- 239000007921 spray Substances 0.000 abstract description 3
- 230000000630 rising effect Effects 0.000 abstract 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Landscapes
- Catching Or Destruction (AREA)
Abstract
The utility model discloses a rectilinear unmanned train's aircraft, be provided with the gyro wheel on the bracing piece of bottom, can conveniently remove, the problem of the stand stretch avoiding causing because of the removal, be provided with the solar radiation board on the bispin wing, can utilize the sun to enable the rotor and rotate, the energy can be saved, the edge of backup pad is provided with the arc shielding plate, can be when overcast and rainy weather, and the harm of rainwater is avoided to the protection camera, be provided with position sensor in the medical kit, being provided with the inductor on the baffle, using together through position sensor and inductor, spray insecticide in the time of can rising a take the altitude aboard, improved its degree of automation, this rectilinear unmanned train's aircraft has the energy can be saved, advantage that degree of automation is high, has wide market prospect.
Description
Technical field
The utility model relates to unmanned plane apparatus field, is specifically related to the unmanned training aeroplane of a kind of high low type.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Can be divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc.Unmanned plane, by application, can be divided into military and civilian.Military aspect, unmanned plane is divided into scout and target drone.Unmanned plane+sector application is the real firm need of unmanned plane.At present taking photo by plane, agricultural plant protection, the field such as mapping application, expanded the purposes of unmanned plane itself greatly.
Summary of the invention
The purpose of this utility model is to provide a kind of high low type unmanned training aeroplane, optimizes traditional unmanned aerial vehicle, has and saves the energy, advantage that degree of automation is high.
For achieving the above object, the utility model provides following technical scheme: the unmanned training aeroplane of a kind of high low type, by Main Control Tank, frame, propeller arrangement and camera composition, described frame is made up of strut bar, connected by three-way pipe between described strut bar, described strut bar is welded with stay bearing plate, described propeller arrangement is arranged on the upper end of stay bearing plate, comprise DCB Specimen and motor cabinet, described DCB Specimen is fixed on motor cabinet by clip, described Main Control Tank is positioned at the side of strut bar, described camera is arranged on the bottom side of stay bearing plate, medicine-chest is fixed with on the downside of the strut bar of described centre, the both sides of described medicine-chest are provided with shower nozzle, baffle plate is provided with between described medicine-chest and shower nozzle.
Preferably, the strut bar of described bottom is provided with roller, described roller is fixed on strut bar by Collapsible rack, and Collapsible rack comprises support plate and rotating shaft, and described roller is positioned at support plate bottom.
Preferably, described DCB Specimen is provided with solar radiation plate.
Preferably, the edge of described stay bearing plate is provided with arc shutter.
Preferably, be provided with position sensor in described medicine-chest, described baffle plate is provided with inductor, described inductor is connected with position sensor.
The beneficial effect of above technical scheme is adopted to be: the utility model provides the unmanned training aeroplane of a kind of high low type, the strut bar of described bottom is provided with roller, movement can be facilitated, avoid the problem because of the mobile stand stretch caused, described DCB Specimen is provided with solar radiation plate, solar power can be utilized to make rotor rotational, save the energy, the edge of described stay bearing plate is provided with arc shutter, can when rainy weather, protection camera is from the infringement of rainwater, position sensor is provided with in described medicine-chest, described baffle plate is provided with inductor, be used in conjunction by position sensor and inductor, spray insecticide when can be raised to certain altitude aboard, improve its degree of automation, the unmanned training aeroplane of this high low type has the saving energy, the advantage that degree of automation is high, there are wide market outlook.
Accompanying drawing explanation
Fig. 1 is the structural representation of the unmanned training aeroplane of a kind of high low type of the utility model;
Fig. 2 is the structural representation of Collapsible rack;
Fig. 3 is the structural representation of solar radiation plate;
Wherein: 1-Main Control Tank, 2-frame, 3-propeller arrangement, 4-camera, 5-strut bar, 6-three-way pipe, 7-stay bearing plate, 8-DCB Specimen, 9-motor cabinet, 10-clip, 11-medicine-chest, 12-shower nozzle, 13-baffle plate, 14-roller, 15-Collapsible rack, 16-support plate, 17-rotating shaft, 18-solar radiation plate, 19-arc shutter, 20-position sensor, 21-inductor.
Detailed description of the invention
The technological means realized for making the utility model, creation characteristic, reaching object and effect is easy to understand, below in conjunction with detailed description of the invention, setting forth the utility model further.
As shown in Figure 1, the unmanned training aeroplane of a kind of high low type, by Main Control Tank 1, frame 2, propeller arrangement 3 and camera 4 form, described frame 2 is made up of strut bar 5, connected by three-way pipe 6 between described strut bar 5, described strut bar 5 is welded with stay bearing plate 7, described propeller arrangement 3 is arranged on the upper end of stay bearing plate 7, comprise DCB Specimen 8 and motor cabinet 9, described DCB Specimen 8 is fixed on motor cabinet 9 by clip 10, described Main Control Tank 1 is positioned at the side of strut bar 5, described camera 4 is arranged on the bottom side of stay bearing plate 7, medicine-chest 11 is fixed with on the downside of the strut bar 5 of described centre, the both sides of described medicine-chest 11 are provided with shower nozzle 12, baffle plate 13 is provided with between described medicine-chest 11 and shower nozzle 12.
In addition, as shown in Figure 2,3, the strut bar 5 of described bottom is provided with roller 14, described roller 14 is fixed on strut bar 5 by Collapsible rack 15, Collapsible rack 15 comprises support plate 16 and rotating shaft 17, described roller 14 is positioned at support plate 16 bottom, described DCB Specimen 8 is provided with solar radiation plate 18, the edge of described stay bearing plate 7 is provided with arc shutter 19, position sensor 20 is provided with in described medicine-chest 11, described baffle plate 13 is provided with inductor 21, and described inductor 21 is connected with position sensor 20.
Based on above-mentioned, the utility model provides the unmanned training aeroplane of a kind of high low type, the strut bar of described bottom is provided with roller, movement can be facilitated, avoid the problem because of the mobile stand stretch caused, described DCB Specimen is provided with solar radiation plate, solar power can be utilized to make rotor rotational, save the energy, the edge of described stay bearing plate is provided with arc shutter, can when rainy weather, protection camera is from the infringement of rainwater, position sensor is provided with in described medicine-chest, described baffle plate is provided with inductor, be used in conjunction by position sensor and inductor, spray insecticide when can be raised to certain altitude aboard, improve its degree of automation, the unmanned training aeroplane of this high low type has the saving energy, the advantage that degree of automation is high, there are wide market outlook.
As known by the technical knowledge, the utility model can be realized by other the embodiment not departing from its Spirit Essence or essential feature.Therefore, above-mentioned disclosed embodiment, with regard to each side, being all casehistory, is not only.Allly all to be included in the utility model within the scope of the utility model or being equal to the change in scope of the present utility model.
Claims (5)
1. the unmanned training aeroplane of high low type, it is characterized in that: by Main Control Tank, frame, propeller arrangement and camera composition, described frame is made up of strut bar, connected by three-way pipe between described strut bar, described strut bar is welded with stay bearing plate, described propeller arrangement is arranged on the upper end of stay bearing plate, comprise DCB Specimen and motor cabinet, described DCB Specimen is fixed on motor cabinet by clip, described Main Control Tank is positioned at the side of strut bar, described camera is arranged on the bottom side of stay bearing plate, medicine-chest is fixed with on the downside of the strut bar of described centre, the both sides of described medicine-chest are provided with shower nozzle, baffle plate is provided with between described medicine-chest and shower nozzle.
2. the unmanned training aeroplane of a kind of high low type according to claim 1, it is characterized in that: the strut bar of described bottom is provided with roller, described roller is fixed on strut bar by Collapsible rack, and Collapsible rack comprises support plate and rotating shaft, and described roller is positioned at support plate bottom.
3. the unmanned training aeroplane of a kind of high low type according to claim 1, is characterized in that: described DCB Specimen is provided with solar radiation plate.
4. the unmanned training aeroplane of a kind of high low type according to claim 1, is characterized in that: the edge of described stay bearing plate is provided with arc shutter.
5. the unmanned training aeroplane of a kind of high low type according to claim 1, is characterized in that: be provided with position sensor in described medicine-chest, and described baffle plate is provided with inductor, and described inductor is connected with position sensor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520432260.6U CN204916189U (en) | 2015-06-23 | 2015-06-23 | Rectilinear unmanned train's aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520432260.6U CN204916189U (en) | 2015-06-23 | 2015-06-23 | Rectilinear unmanned train's aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204916189U true CN204916189U (en) | 2015-12-30 |
Family
ID=54965343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520432260.6U Expired - Fee Related CN204916189U (en) | 2015-06-23 | 2015-06-23 | Rectilinear unmanned train's aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204916189U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108784560A (en) * | 2017-04-28 | 2018-11-13 | 蔡连锁 | Clean the unmanned plane during flying device in building |
-
2015
- 2015-06-23 CN CN201520432260.6U patent/CN204916189U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108784560A (en) * | 2017-04-28 | 2018-11-13 | 蔡连锁 | Clean the unmanned plane during flying device in building |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206273678U (en) | The unmanned plane that a kind of variable empennage is controlled with folded wing | |
| WO2015143093A3 (en) | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | |
| CN205239913U (en) | Top load unmanned aerial vehicle convenient to take off and land fast | |
| CN206243457U (en) | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle | |
| EP4417510A3 (en) | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | |
| CN102556336A (en) | Wing fast unfolding device for folding-wing unmanned plane | |
| WO2015143098A3 (en) | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades | |
| CN206615406U (en) | The automatic auxiliary landing system of rotor wing unmanned aerial vehicle | |
| CN105217033A (en) | Amphibious rotor wing unmanned aerial vehicle | |
| CN106585975A (en) | Compact unmanned aerial vehicle | |
| CN204587305U (en) | The electronic unmanned plane of multifunctional foldable eight rotor | |
| CN206984354U (en) | A kind of aircraft | |
| CN204173155U (en) | A kind of delta-wing aircraft | |
| CN204822084U (en) | Many rotor unmanned aerial vehicle | |
| CN204916189U (en) | Rectilinear unmanned train's aircraft | |
| CN205087129U (en) | Folded form aircraft of taking photo by plane | |
| CN104787335A (en) | 3D printed solar unmanned aerial vehicle | |
| CN207053044U (en) | A kind of electric power inspection system based on unmanned plane | |
| CN104002968A (en) | Small conical rotary flapping wing air vehicle | |
| CN204937497U (en) | A kind of frame-type large carrying convolution wing structure | |
| CN204310051U (en) | A kind of take solar powered aircraft as the meteorological aircraft of carrier | |
| CN209209028U (en) | One kind is verted three rotor VTOL all-wing aircraft of type | |
| CN207985228U (en) | A kind of novel unmanned plane of taking photo by plane | |
| CN204956918U (en) | Unmanned aerial vehicle bispin wing structure | |
| CN103661944A (en) | Solar saucer-type aircraft with unmanned perennial aerial hovering function |
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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151230 Termination date: 20160623 |