CN207257976U - A kind of agricultural prospecting anticollision unmanned plane - Google Patents
A kind of agricultural prospecting anticollision unmanned plane Download PDFInfo
- Publication number
- CN207257976U CN207257976U CN201720858658.5U CN201720858658U CN207257976U CN 207257976 U CN207257976 U CN 207257976U CN 201720858658 U CN201720858658 U CN 201720858658U CN 207257976 U CN207257976 U CN 207257976U
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- strut
- cabin
- prospecting
- undercarriage
- rotor
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Abstract
The utility model discloses a kind of agricultural prospecting anticollision unmanned plane,Including undercarriage and cabin,The top of the undercarriage is equipped with rotor strut,And it is welded with strut between the cross bar of the bottom of undercarriage two,Prospecting camera is arranged with the strut,The undercarriage further includes the diagonal brace being welded between the cross bar of bottom two and rotor strut,The cabin is the spherical structure being fixedly mounted between rotor strut and strut,And it is provided with infrared camera and ultrasonic probe on the sphere equatorial line of cabin,Hatch door is provided with the outer surface of the cabin,Six rotor of the utility model and infrared camera,Ultrasonic probe is engaged,Stability and sensitivity when ensure that body flight,Built-in power supply box and controller strong antijamming capability,Spherical cabin coordinates the alternate installation of six infrared cameras and six ultrasonic probes,360 ° when realizing flight detect without dead angle,The generation of contingency when effectively prevent remote exploration,Practicality is good.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, and in particular to a kind of agricultural prospecting anticollision unmanned plane.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned vehicle that presetting apparatus manipulates.Unmanned plane is actually the general designation of unmanned vehicle, from technical standpoint
Definition can be divided into：This is several for unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol
Major class.Compared with manned aircraft, it has small, low cost, easy to use, low to operational environment requirement, battlefield existence energy
The advantages that power is stronger.Since UAV has great significance Future Air Combat, each main military country of the world all exists
Step up the development work of progress UAV.
With the disclosure of unmanned air vehicle technique knowledge, it also gradually enters into other every aspects in life, for example, take photo by plane and
Agriculture field etc., contracts necessary to family wherein agricultural prospecting unmanned plane is a wide range of plantation, can be brought to user greatly
Facility, while save substantial amounts of cost of labor, but reconnoitre unmanned plane now, since exploration scope is big, it is ground control not
Controllable factor is too many, and flying bird trees etc. can all produce collision phenomenon, and severe patient even directly damages body, and being brought to user makes
The inconvenience used and economic loss, need us and solve.
Utility model content
The purpose of this utility model is to provide a kind of agricultural prospecting anticollision unmanned plane, to solve to carry in above-mentioned background technology
Go out and reconnoitre unmanned plane now, since exploration scope is big, ground control uncontrollable factor is too many, and flying bird trees etc. can all produce and touch
Phenomenon is hit, severe patient even directly damages body, the problem of being brought to user using upper inconvenience and economic loss.
To achieve the above object, the utility model provides following technical solution：A kind of agricultural prospecting anticollision unmanned plane, including
Undercarriage and cabin, the top of the undercarriage is equipped with rotor strut, and is welded with support between the cross bar of the bottom of undercarriage two
Bar, is arranged with prospecting camera on the strut, the undercarriage further include be welded on the cross bar of bottom two and rotor strut it
Between diagonal brace, the cabin is the spherical structure being fixedly mounted between rotor strut and strut, and the sphere equatorial line of cabin
On be provided with infrared camera and ultrasonic probe, be provided with hatch door on the outer surface of the cabin, and the inside installation of cabin
There are power supply box and controller, prospecting camera, infrared camera, ultrasonic probe and the power supply box electrically connect with controller
Connect, the controller is electrically connected with ground control unit.
Preferably, the rotor strut is provided with six roots of sensation strut altogether, and is mounted on rotary fan on six roots of sensation strut, described
Rotary fan is electrically connected with built-in controller.
Preferably, the infrared camera and ultrasonic probe are respectively arranged with six, and six infrared cameras and six
On the alternate sphere equatorial line installed in cabin of a ultrasonic probe.
Preferably, the hatch door is connected through the hinge with cabin.
Preferably, the strut is welded with two altogether, and two struts are the arcuate structure to raise up.
Compared with prior art, the beneficial effects of the utility model are：Unmanned plane side safe to use scientific and reasonable for structure
Just, six rotors are engaged with infrared camera, ultrasonic probe, it is ensured that stability and sensitivity during body flight, it is built-in
Power supply box and controller strong antijamming capability, spherical cabin coordinate the phase of six infrared cameras and six ultrasonic probes
Between install, 360 ° when realizing flight are detected without dead angle, the generation of contingency when effectively prevent remote exploration, practical
Property is good.
Brief description of the drawings
Fig. 1 is the top view of the utility model；
Fig. 2 is the front view of the utility model.
In figure：1- undercarriages, 2- rotors strut, 3- rotary fans, 4- infrared cameras, 5- cabins, 6- ultrasonic probes,
7- hatch doors, 8- prospectings camera, 9- struts.
Embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained, shall fall within the protection scope of the present invention.
- 2 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of agricultural prospecting anticollision unmanned plane, including rise
Fall frame 1 and cabin 5, the top of undercarriage 1 is equipped with rotor strut 2, and is welded with strut between the cross bar of the bottom of undercarriage 1 two
9, be arranged with prospecting camera 8 on strut 9, undercarriage 1 further include be welded on it is oblique between the cross bar of bottom two and rotor strut 2
Support, cabin 5 is the spherical structure being fixedly mounted between rotor strut 2 and strut 9, and is set on the sphere equatorial line of cabin 5
There are infrared camera 4 and ultrasonic probe 6, hatch door 7 is provided with the outer surface of cabin 5, and the inside of cabin 5 is provided with power supply
Case and controller, prospecting camera 8, infrared camera 4, ultrasonic probe 6 and power supply box are electrically connected with controller, control
Device is electrically connected with ground control unit.
In the present embodiment, it is preferred that rotor strut 2 is provided with six roots of sensation strut altogether, and is mounted on rotating on six roots of sensation strut
Flabellum 3, rotary fan 3 are electrically connected with built-in controller, and six rotor flying stability are good.
In the present embodiment, it is preferred that infrared camera 4 and ultrasonic probe 6 are respectively arranged with six, and six infrared take the photograph
As first 4 and six ultrasonic probes 6 it is alternate on the sphere equatorial line of cabin 5, realize in flight course 360 ° complete
Orientation is without dead angle real-time detection, and accident collision accident when effectively prevent remote exploration occurs, and practical value is high.
In the present embodiment, for the ease of the maintenance and debugging of built-in controller and power supply box, it is preferred that hatch door 7 and cabin 5
It is connected through the hinge.
In the present embodiment, it is preferred that strut 9 is welded with two altogether, and two struts 9 are the arc knot to raise up
Structure, one in front and one in back two struts 9 to raise up carry spherical cabin 5, and cooperate and pass through with rotor strut 2 and diagonal brace
Bolt is fixedly connected, and the stability of cabin 5 is more preferable.
Operation principle：Safe ready when the utility model is used, user have debugged built-in controller according to correct way
After ground control unit, you can input exploration uses, in flight course, six rotors and infrared camera 4, ultrasonic probe
6 are engaged, it is ensured that stability and sensitivity during body flight, built-in power supply box and controller strong antijamming capability, ball
The cabin 5 of shape coordinates the alternate installation of six infrared cameras 4 and six ultrasonic probes 6, realizes 360 ° of nothings during flight
Dead angle detects, the generation of accident collision accident when effectively prevent remote exploration, and practicality is good.
While there has been shown and described that the embodiment of the utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from the principle of the utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of agricultural prospecting anticollision unmanned plane, including undercarriage (1) and cabin (5), it is characterised in that：The undercarriage (1)
Top be equipped with rotor strut (2), and strut (9) is welded between the cross bar of the bottom of undercarriage (1) two, the strut (9)
On be arranged with prospecting camera (8), the undercarriage (1), which further includes, to be welded between the cross bar of bottom two and rotor strut (2)
Diagonal brace, the cabin (5) is to be fixedly mounted on spherical structure between rotor strut (2) and strut (9), and cabin (5)
Infrared camera (4) and ultrasonic probe (6) are provided with sphere equatorial line, cabin is provided with the outer surface of the cabin (5)
Door (7), and the inside of cabin (5) is provided with power supply box and controller, the prospecting camera (8), infrared camera (4), surpass
Sonic probe (6) and power supply box are electrically connected with controller, and the controller is electrically connected with ground control unit.
A kind of 2. agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that：The rotor strut (2) is altogether
Six roots of sensation strut is provided with, and rotary fan (3) is mounted on six roots of sensation strut, the rotary fan (3) and built-in controller
It is electrically connected.
A kind of 3. agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that：The infrared camera (4)
Six, and six infrared cameras (4) and the alternate installation of six ultrasonic probes (6) are respectively arranged with ultrasonic probe (6)
On the sphere equatorial line of cabin (5).
A kind of 4. agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that：The hatch door (7) and cabin
(5) it is connected through the hinge.
A kind of 5. agricultural prospecting anticollision unmanned plane according to claim 1, it is characterised in that：The strut (9) is welded altogether
There are two, and two struts (9) are the arcuate structure to raise up.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720858658.5U CN207257976U (en) | 2017-07-16 | 2017-07-16 | A kind of agricultural prospecting anticollision unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720858658.5U CN207257976U (en) | 2017-07-16 | 2017-07-16 | A kind of agricultural prospecting anticollision unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207257976U true CN207257976U (en) | 2018-04-20 |
Family
ID=61926933
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720858658.5U Active CN207257976U (en) | 2017-07-16 | 2017-07-16 | A kind of agricultural prospecting anticollision unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207257976U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108715224A (en) * | 2018-06-28 | 2018-10-30 | 山东浩坤安全技术咨询有限公司 | A kind of unmanned plane crash protection |
-
2017
- 2017-07-16 CN CN201720858658.5U patent/CN207257976U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108715224A (en) * | 2018-06-28 | 2018-10-30 | 山东浩坤安全技术咨询有限公司 | A kind of unmanned plane crash protection |
| CN108715224B (en) * | 2018-06-28 | 2021-11-30 | 江苏翔龙智能装备科技有限公司 | Unmanned aerial vehicle crash-proof device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Xu Zhiyong Inventor before: Wang Lei |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180411 Address after: 755000 the Ningxia Hui Autonomous Region B, Shapotou Science Park, Zhongguancun, Shapotou, central Wei city. Patentee after: Central aviation science and Technology Development Co Ltd Address before: 518104 Yuxing building, Baoan District Sha Jing Street, Shenzhen, Guangdong 708 Patentee before: Shenzhen pan Sen Electronics Co., Ltd. |