CN204197283U - A kind of many rotor wing unmanned aerial vehicles - Google Patents
A kind of many rotor wing unmanned aerial vehicles Download PDFInfo
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- CN204197283U CN204197283U CN201420663578.0U CN201420663578U CN204197283U CN 204197283 U CN204197283 U CN 204197283U CN 201420663578 U CN201420663578 U CN 201420663578U CN 204197283 U CN204197283 U CN 204197283U
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- spool
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- hawser
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Abstract
The utility model provides a kind of many rotor wing unmanned aerial vehicles 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, rotor, rotor motor and leg; Also being provided with retractor device below frame, retractor device is connected with sampling probe, sampling probe being provided with the sampling mechanism for gathering soil or water body sample; Retractor device comprises cabinet, elevator motor, power-transfer clutch, spool and hawser; Cabinet is fixed on the bottom of frame; Elevator motor and spool are installed in cabinet, and elevator motor is connected with spool by power-transfer clutch; Hawser circle is around on spool, and the free end of hawser is connected with sampling probe; Spool is also provided with brake disc, cabinet is provided with a pair braking clamp for braking disc; The caliper of braking clamp is driven by miniature motor; Power-transfer clutch is the electric control structure be electrically connected with message handler.
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 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 many rotor wing unmanned aerial vehicles of the most extensively prospect at civil area.Many rotor wing unmanned aerial vehicles 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 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, 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, power-transfer clutch, 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 power-transfer clutch; Hawser circle is around on spool, and the free end of hawser is connected with sampling probe; Spool is also provided with brake disc, cabinet is provided with a pair braking clamp for braking disc; The caliper of described braking clamp is driven by miniature motor; Described power-transfer clutch is the electric control structure be electrically connected with message handler.
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, power-transfer clutch, 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, power-transfer clutch, 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 power-transfer clutch; Hawser circle is around on spool, and the free end of hawser is connected with sampling probe; Spool is also provided with brake disc, cabinet is provided with a pair braking clamp for braking disc; The caliper of described braking clamp is driven by miniature motor; Described power-transfer clutch is the electric control structure be electrically connected with message handler.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 can not be had influence on while sampling, the ingenious combination of power-transfer clutch and brake disc can drive hawser to fall by the deadweight of sampling probe, the height of whereabouts can be controlled by brake disc simultaneously, driven by elevator motor again when needs rise and rise, so more save electric energy, controllability is also higher.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, power-transfer clutch, 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 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 of many rotor wing unmanned aerial vehicles of the prior art.
Fig. 2 is the structural representation of the many rotor wing unmanned aerial vehicles 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 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, power-transfer clutch, 504, spool, 505, brake disc, 506, braking clamp, 507, 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, 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, power-transfer clutch 503, spool 504 and hawser 507; 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 power-transfer clutch 503; Hawser 507 circle is around on spool 504, and the free end of hawser 507 is connected with sampling probe 6; Spool 504 is also provided with brake disc 505, cabinet 501 is provided with a pair braking clamp 506 for braking disc 505; The caliper of described braking clamp 506 is driven by miniature motor; Described power-transfer clutch 503 is the electric control structure be electrically connected with message handler.
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, power-transfer clutch 503, spool 504 and hawser 507 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, power-transfer clutch 503, spool 504 and hawser 507; 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 power-transfer clutch 503; Hawser 507 circle is around on spool 504, and the free end of hawser 507 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, power-transfer clutch 503, spool 504 and hawser 507 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 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 sampling probe 6 of unmanned plane of the present utility model descend through power-transfer clutch by the disengaging of machine shaft and spool rotating shaft, braking clamp unclamps simultaneously, realized by the free fall of sampling probe own wt, pop one's head in after sampling, by power-transfer clutch, elevator motor 502 is connected to reclaim hawser with spool again, and brake gear is used to the falling head controlling sampling probe, 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.
Described power-transfer clutch, has relevant matured product in prior art, directly buying can realize the product that diaxon connects and disconnects two states control.
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. a rotor wing unmanned aerial vehicle more than, 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), power-transfer clutch (503), spool (504) and hawser (507); 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 power-transfer clutch (503); Hawser (507) circle is around on spool (504), and the free end of hawser (507) is connected with sampling probe (6); Spool (504) is also provided with brake disc (505), cabinet (501) is provided with a pair braking clamp for braking disc (505) (506); The caliper of described braking clamp (506) is driven by miniature motor; Described power-transfer clutch (503) is the electric control structure be electrically connected with message handler.
2. many rotor wing unmanned aerial vehicles according to claim 1, is characterized in that: described sampling mechanism is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure.
3. many rotor wing unmanned aerial vehicles according to claim 1, is characterized in that: described frame (1), cabinet (501), power-transfer clutch (503), spool (504) and hawser (507) are carbon fiber structural.
4. many rotor wing unmanned aerial vehicles 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 |
|---|---|---|---|
| CN201420663578.0U CN204197283U (en) | 2014-11-07 | 2014-11-07 | A kind of many rotor wing unmanned aerial vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420663578.0U CN204197283U (en) | 2014-11-07 | 2014-11-07 | A kind of many rotor wing unmanned aerial vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204197283U true CN204197283U (en) | 2015-03-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420663578.0U Withdrawn - After Issue CN204197283U (en) | 2014-11-07 | 2014-11-07 | A kind of many rotor wing unmanned aerial vehicles |
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| Country | Link |
|---|---|
| CN (1) | CN204197283U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354857A (en) * | 2014-11-07 | 2015-02-18 | 成都好飞机器人科技有限公司 | Unmanned aerial vehicle with multiple rotor wings |
| CN105936336A (en) * | 2016-05-27 | 2016-09-14 | 合肥德秦人居环境科技有限公司 | Wide water surface water sample collecting air, water and land multi-rotor unmanned plane |
| CN108778927A (en) * | 2015-09-23 | 2018-11-09 | 沃尔玛阿波罗有限责任公司 | The system and method for delivering product with unmanned delivery aircraft |
-
2014
- 2014-11-07 CN CN201420663578.0U patent/CN204197283U/en not_active Withdrawn - After Issue
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354857A (en) * | 2014-11-07 | 2015-02-18 | 成都好飞机器人科技有限公司 | Unmanned aerial vehicle with multiple rotor wings |
| CN108778927A (en) * | 2015-09-23 | 2018-11-09 | 沃尔玛阿波罗有限责任公司 | The system and method for delivering product with unmanned delivery aircraft |
| US11053006B2 (en) | 2015-09-23 | 2021-07-06 | Walmart Apollo, Llc | Systems and methods of delivering products with unmanned delivery aircrafts |
| CN105936336A (en) * | 2016-05-27 | 2016-09-14 | 合肥德秦人居环境科技有限公司 | Wide water surface water sample collecting air, water and land multi-rotor unmanned plane |
| CN105936336B (en) * | 2016-05-27 | 2018-01-12 | 合肥德秦人居环境科技有限公司 | Use multi-rotor unmanned aerial vehicle in a kind of wide water surface water sampling sky land and water three |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20150311 Effective date of abandoning: 20160413 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |