CN204323679U - Possess many rotor wing unmanned aerial vehicles of sampled functions - Google Patents
Possess many rotor wing unmanned aerial vehicles of sampled functions Download PDFInfo
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- CN204323679U CN204323679U CN201420695238.6U CN201420695238U CN204323679U CN 204323679 U CN204323679 U CN 204323679U CN 201420695238 U CN201420695238 U CN 201420695238U CN 204323679 U CN204323679 U CN 204323679U
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- frame
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- sampling
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- rotor
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Abstract
The utility model provides a kind of many rotor wing unmanned aerial vehicles possessing sampled functions that can apply to the growth such as farmland and have the non-smooth surface of crop to carry out soil or water body to carry out sampling.It comprises frame (1), rotor (2), rotor motor (3) and leg (4); Frame (1) below is also provided with retractor device (5), and retractor device (5) is connected with sampling probe (6), (6) are provided with sampling mechanism to sampling probe; Retractor device (5) comprises cabinet (501), elevator motor (502), coupler (503), spool (504) and hawser (505); (501 in the bottom of frame (1) for cabinet; Elevator motor (502) and spool (504) are installed in cabinet (501), and elevator motor (502) is connected with spool (504) by coupler (503); Hawser (505) circle is around on spool (504), and hawser (505) is connected with sampling probe (6).
Description
Technical field
The utility model relates to a kind of unmanned plane, specifically refers to a kind of many rotor wing unmanned aerial vehicles possessing sampled functions applying to civil area.
Background technology
Unmanned plane is a kind of unmanned vehicle handled by radio robot or self process controller.It comes across the twenties in 20th century the earliest, is at that time to use as the target drone of training.That many country is for describing the term of latest generation robot airplane.From literal, this term can describe from kite, drone, to the cruise missile that V-1 fly bomb comes from development, but in the term of the military, is only limitted to reusable heavier-than-air aircraft.Unmanned plane is of many uses, and cost is low, and efficiency-cost ratio is good; Risk that no one was injured; Viability is strong, and maneuvering performance is good, easy to use, has extremely important effect, more hold out broad prospects at civil area in modern war.Can be divided into from technical standpoint definition: this several large class of depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol.
There to be the many rotor wing unmanned aerial vehicles possessing sampled functions of the most extensively prospect at civil area.The many rotor wing unmanned aerial vehicles possessing sampled functions of the prior art are mainly used in realtime graphic monitoring at civil area, and crop sprays control and small article transport etc.Its common structure as shown in Figure 1, it comprises frame 01, rotor 02, rotor motor 03 and the several major part of leg 04, frame 01 is provided with battery and control device of wireless, and then carries camera or sprinkler by user respectively according to user demand.And the contriver of present patent application is found by practice, unmanned plane of the prior art is when applying to agriculturally, mostly can only fly in the overhead of crop and carry out taking and spraying operation, and lack the device accordingly soil or the water body environment of plant growth sampled; In sum, be badly in need of at present wanting a kind of unmanned plane that can apply to the growths such as farmland and have the non-smooth surface of crop to carry out soil or water body to carry out sampling.
Utility model content
The technical problems to be solved in the utility model is, provides a kind of many rotor wing unmanned aerial vehicles possessing sampled functions that can apply to the growth such as farmland and have the non-smooth surface of crop to carry out soil or water body to carry out sampling.
For solving the problems of the technologies described above, the technical scheme that the utility model provides is: a kind of many rotor wing unmanned aerial vehicles possessing sampled functions, and it comprises frame, rotor, rotor motor and leg; Described rotor for having four at least, and is installed on the surrounding of frame by transverse link, is connected with a rotor motor below each rotor; Described leg is arranged on the below of frame; Frame is also provided with lithium cell for powering to consuming parts and for controlling the message handler with telecommunication; Also being provided with retractor device below described frame, described retractor device is connected with sampling probe, described sampling probe being provided with the sampling mechanism for gathering soil or water body sample; Described retractor device comprises cabinet, elevator motor, coupler, spool and hawser; Described cabinet is fixed on the bottom of frame; Described elevator motor and spool are installed in cabinet, and elevator motor is connected with spool by coupler; Hawser circle is around on spool, and the free end of hawser is connected with sampling probe.
As preferably, described sampling mechanism is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure.
As preferably, described frame, cabinet, coupler, spool and hawser are carbon fiber structural.
As improvement, sampling probe is provided with for the bluetooth communication with message handler radio communication.
After adopting said structure, the utility model has following beneficial effect: be also provided with retractor device below described frame, and described retractor device is connected with sampling probe, described sampling probe is provided with the sampling mechanism for gathering soil or water body sample; Described retractor device comprises cabinet, elevator motor, coupler, spool and hawser; Described cabinet is fixed on the bottom of frame; Described elevator motor and spool are installed in cabinet, and elevator motor is connected with spool by coupler; Hawser circle is around on spool, and the free end of hawser is connected with sampling probe.Can be sampled the soil in the crop growth environment below it or water body when unmanned plane does not land by the combination of retractor device and sampling probe, the growth of crop while sampling, can not be had influence on.Described sampling mechanism is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure.Pointed cone structure can better be inserted in soil, is conducive to sampling cup and collects sample.Described frame, cabinet, coupler, spool and hawser are carbon fiber structural.Carbon fiber structural is stablized, and weight is little, greatly can improve the cruise duration of unmanned plane.Described sampling probe is provided with for the bluetooth communication with message handler radio communication.This design adopts communication, avoids the use of communication cable, further reduces the weight of whole device, also prevent the interference of cable to hawser simultaneously.
In sum, the utility model provides a kind of many rotor wing unmanned aerial vehicles possessing sampled functions that can apply to the growth such as farmland and have the non-smooth surface of crop to carry out soil or water body to carry out sampling.
Accompanying drawing explanation
Fig. 1 is the structural representation possessing many rotor wing unmanned aerial vehicles of sampled functions of the prior art.
Fig. 2 is the structural representation possessing many rotor wing unmanned aerial vehicles of sampled functions in the utility model.
Fig. 3 is the structure for amplifying schematic diagram of retractor device in Fig. 2 and sampling probe.
Fig. 4 is the structural representation of many rotor wing unmanned aerial vehicles under sampling state possessing sampled functions in the utility model.
As shown in the figure: in prior art 01, frame, 02, rotor, 03, rotor motor, 04, leg.
In the utility model: 1, frame, 2, rotor, 3, rotor motor, 4, leg, 5, retractor device, 6, sampling probe, 501, cabinet, 502, elevator motor, 503, coupler, 504, spool, 505, hawser.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
By reference to the accompanying drawings 2 and accompanying drawing 3, a kind of many rotor wing unmanned aerial vehicles possessing sampled functions, it comprises frame 1, rotor 2, rotor motor 3 and leg 4; Described rotor 2 for having four at least, and is installed on the surrounding of frame 1 by transverse link, is connected with a rotor motor 3 below each rotor 2; Described leg 4 is arranged on the below of frame 1; Frame 1 is also provided with lithium cell for powering to consuming parts and for controlling the message handler with telecommunication; Also being provided with retractor device 5 below described frame 1, described retractor device 5 is connected with sampling probe 6, described sampling probe 6 being provided with the sampling mechanism for gathering soil or water body sample; Described retractor device 5 comprises cabinet 501, elevator motor 502, coupler 503, spool 504 and hawser 505; Described cabinet 501 is fixed on the bottom of frame 1; Described elevator motor 502 and spool 504 are installed in cabinet 501, and elevator motor 502 is connected with spool 504 by coupler 503; Hawser 505 circle is around on spool 504, and the free end of hawser 505 is connected with sampling probe 6.
As preferably, described sampling mechanism is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure.
As preferably, described frame 1, cabinet 501, coupler 503, spool 504 and hawser 505 are carbon fiber structural.
As improvement, sampling probe 6 is provided with for the bluetooth communication with message handler radio communication.
After adopting said structure, the utility model has following beneficial effect: be also provided with retractor device 5 below described frame 1, described retractor device 5 being connected with sampling probe 6, described sampling probe 6 being provided with the sampling mechanism for gathering soil or water body sample; Described retractor device 5 comprises cabinet 501, elevator motor 502, coupler 503, spool 504 and hawser 505; Described cabinet 501 is fixed on the bottom of frame 1; Described elevator motor 502 and spool 504 are installed in cabinet 501, and elevator motor 502 is connected with spool 504 by coupler 503; Hawser 505 circle is around on spool 504, and the free end of hawser 505 is connected with sampling probe 6.Can be sampled the soil in the crop growth environment below it or water body when unmanned plane does not land by the combination of retractor device and sampling probe, the growth of crop while sampling, can not be had influence on.Described sampling mechanism is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure.Pointed cone structure can better be inserted in soil, is conducive to sampling cup and collects sample.Described frame 1, cabinet 501, coupler 503, spool 504 and hawser 505 are carbon fiber structural.Carbon fiber structural is stablized, and weight is little, greatly can improve the cruise duration of unmanned plane.Described sampling probe 6 is provided with for the bluetooth communication with message handler radio communication.This design adopts communication, avoids the use of communication cable, further reduces the weight of whole device, also prevent the interference of cable to hawser simultaneously.
In sum, the utility model provides a kind of many rotor wing unmanned aerial vehicles possessing sampled functions that can apply to the growth such as farmland and have the non-smooth surface of crop to carry out soil or water body to carry out sampling.
Further combined with accompanying drawing 4, the lifting of the sampling probe 6 of unmanned plane of the present utility model is directly realized by the forward and reverse of elevator motor 502, pop one's head in after sampling, elevator motor 502 meeting the automatic recovery hawser, the device of time set and record motor rotations is provided with, for the work of auxiliary control motor in elevator motor 502.Certainly, user also can be worked by video pictures direct Remote elevator motor 502, only needs to carry a camera on unmanned plane.Described elevator motor 502 can carry out communication by wired or wireless mode and message handler, also by the revolution device of inner time set and can carry central process unit oneself independent work.
Be described the utility model and embodiment thereof above, this description does not have restricted, and shown in accompanying drawing is also one of embodiment of the present utility model, and actual structure is not limited thereto.If generally speaking those of ordinary skill in the art enlightens by it, when not departing from the utility model and creating aim, design the frame mode similar to this technical scheme and embodiment without creationary, protection domain of the present utility model all should be belonged to.
Claims (4)
1. possess many rotor wing unmanned aerial vehicles of sampled functions, it comprises frame (1), rotor (2), rotor motor (3) and leg (4); Described rotor (2) for having four at least, and is installed on the surrounding of frame (1) by transverse link, and each rotor (2) below is connected with a rotor motor (3); Described leg (4) is arranged on the below of frame (1); Frame (1) is also provided with lithium cell for powering to consuming parts and for controlling the message handler with telecommunication; It is characterized in that: described frame (1) below is also provided with retractor device (5), described retractor device (5) being connected with sampling probe (6), described sampling probe (6) being provided with the sampling mechanism for gathering soil or water body sample; Described retractor device (5) comprises cabinet (501), elevator motor (502), coupler (503), spool (504) and hawser (505); Described cabinet (501) is fixed on the bottom of frame (1); Described elevator motor (502) and spool (504) are installed in cabinet (501), and elevator motor (502) is connected with spool (504) by coupler (503); Hawser (505) circle is around on spool (504), and the free end of hawser (505) is connected with sampling probe (6).
2. the many rotor wing unmanned aerial vehicles possessing sampled functions according to claim 1, it is characterized in that: described sampling mechanism is the sampling cup with heat detector, described sampling cup lower end is pointed cone structure.
3. the many rotor wing unmanned aerial vehicles possessing sampled functions according to claim 1, is characterized in that: described frame (1), cabinet (501), coupler (503), spool (504) and hawser (505) are carbon fiber structural.
4. the many rotor wing unmanned aerial vehicles possessing sampled functions according to claim 1, is characterized in that: (6) are provided with for the bluetooth communication with message handler radio communication sampling probe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420695238.6U CN204323679U (en) | 2014-11-19 | 2014-11-19 | Possess many rotor wing unmanned aerial vehicles of sampled functions |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420695238.6U CN204323679U (en) | 2014-11-19 | 2014-11-19 | Possess many rotor wing unmanned aerial vehicles of sampled functions |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204323679U true CN204323679U (en) | 2015-05-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420695238.6U Expired - Fee Related CN204323679U (en) | 2014-11-19 | 2014-11-19 | Possess many rotor wing unmanned aerial vehicles of sampled functions |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI577606B (en) * | 2015-11-09 | 2017-04-11 | National Chung-Shan Institute Of Science And Technology Armaments Bureau | A multi - link vertical retracting device |
-
2014
- 2014-11-19 CN CN201420695238.6U patent/CN204323679U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI577606B (en) * | 2015-11-09 | 2017-04-11 | National Chung-Shan Institute Of Science And Technology Armaments Bureau | A multi - link vertical retracting device |
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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 |
Granted publication date: 20150513 Termination date: 20151119 |
|
| EXPY | Termination of patent right or utility model |