CN204323680U - Possesses the unmanned plane of snap catch ability - Google Patents
Possesses the unmanned plane of snap catch ability Download PDFInfo
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- CN204323680U CN204323680U CN201420695337.4U CN201420695337U CN204323680U CN 204323680 U CN204323680 U CN 204323680U CN 201420695337 U CN201420695337 U CN 201420695337U CN 204323680 U CN204323680 U CN 204323680U
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- spool
- transmission gear
- brake equipment
- rotor
- unmanned plane
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Abstract
The utility model provides a kind of farmland etc. that can apply to and grows the unmanned plane possessing snap catch ability having the non-smooth surface of crop to carry out soil or water body sampling, and it comprises frame, rotor, rotor motor, leg, retractor device and sampling probe; Retractor device comprises cabinet, spool, spool, the first transmission gear, power-transfer clutch, the second transmission gear, hawser and brake equipment; Rotor motor is dual-axle motor; Lower rotary shaft is connected with output gear, output gear is connected with the first transmission gear, first transmission gear is connected with the second transmission gear by power-transfer clutch simultaneously, second transmission gear is connected with spool, spool and spool circumference fit, hawser is wound on spool, and the free end of hawser is connected with sampling probe; Brake equipment is arranged on the end of spool; Cabinet is fixed on rotor motor, and spool, power-transfer clutch and brake equipment are fixed on casing; Rotor motor, power-transfer clutch, brake equipment and sampling probe are all electrically connected with message handler.
Description
Technical field
The utility model relates to a kind of unmanned plane, specifically refers to a kind of unmanned plane possessing snap catch ability 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 unmanned plane possessing snap catch ability of the most extensively prospect at civil area.The unmanned plane possessing snap catch ability of the prior art is 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 farmland etc. that can apply to grow the unmanned plane having the non-smooth surface of crop to carry out soil or water body sampling.
Utility model content
The technical problems to be solved in the utility model is, provides a kind of farmland etc. that can apply to grow the unmanned plane possessing snap catch ability having the non-smooth surface of crop to carry out soil or water body sampling.
For solving the problems of the technologies described above, the technical scheme that the utility model provides is: a kind of unmanned plane possessing snap catch ability, 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 the lithium cell for powering to consuming parts and the message handler for controlling unmanned plane and telecommunication; It comprises retractor device and sampling probe; Described retractor device comprises cabinet, spool, spool, the first transmission gear, power-transfer clutch, the second transmission gear, hawser and brake equipment; Described rotor motor is the dual-axle motor comprising rotating shaft and lower rotary shaft; Lower rotary shaft is provided with output gear, upper rotating shaft is connected with wing, output gear is connected with the first transmission gear, first transmission gear is connected with the second transmission gear by power-transfer clutch simultaneously, second transmission gear is connected with spool, spool and the spacing fit of spool circumference, hawser is wound on spool, and the free end of hawser is connected with sampling probe; Brake equipment is arranged on the end of spool; Described cabinet is fixed on rotor motor, and spool, power-transfer clutch and brake equipment are fixed on casing; Rotor motor, power-transfer clutch, brake equipment and sampling probe are all electrically connected with message handler.
As preferably, described sampling probe is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure, and the periphery of sampling cup is provided with clump weight.
As preferably, described frame, rotor, rotor motor and leg, cabinet, spool, spool, the first transmission gear, power-transfer clutch, the second transmission gear, hawser and brake equipment are carbon fiber structural.
As improvement, sampling probe is provided with for the bluetooth communication with message handler radio communication.
As improvement, described brake equipment is automatically controlled spiral expanding bar, and described automatically controlled spiral expanding bar is offseted by bar head and spool sidewall and realizes friction braking.
After adopting said structure, the utility model has following beneficial effect: it comprises retractor device and sampling probe; Described retractor device comprises cabinet, spool, spool, the first transmission gear, power-transfer clutch, the second transmission gear, hawser and brake equipment; Described rotor motor is the dual-axle motor comprising rotating shaft and lower rotary shaft; Lower rotary shaft is provided with output gear, upper rotating shaft is connected with wing, output gear is connected with the first transmission gear, first transmission gear is connected with the second transmission gear by power-transfer clutch simultaneously, second transmission gear is connected with spool, spool and the spacing fit of spool circumference, hawser is wound on spool, and the free end of hawser is connected with sampling probe; Brake equipment is arranged on the end of spool; Described cabinet is fixed on rotor motor, and spool, power-transfer clutch and brake equipment are fixed on casing; Rotor motor, power-transfer clutch, brake equipment and sampling probe are all electrically connected with message handler.Cleverly adopt dual-axle motor combine with elevator structure, drive spool to rotate by the lower end of rotor motor, so as on carry sampling probe, when sampling probe need whereabouts sample time, be then realized by the deadweight of power-transfer clutch, brake equipment and probe.This practicality when unmanned plane does not land to the soil in the crop growth environment below it or water body sampling, can not have influence on the growth of crop by the combination of retractor device and sampling probe while sampling.Described sampling probe is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure, and the periphery of sampling cup is provided with clump weight.Pointed cone structure can better be inserted in soil, is conducive to sampling cup and collects sample, and clump weight can use the stable whereabouts of sampling cup.Described frame, rotor, rotor motor and leg, cabinet, spool, spool, the first transmission gear, power-transfer clutch, the second transmission gear, hawser and brake equipment 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.Described brake equipment is automatically controlled spiral expanding bar, and described automatically controlled spiral expanding bar is offseted by bar head and spool sidewall and realizes friction braking, and automatically controlled spiral expanding bar structure is simplified more, and braking effect can meet the demand of spool.
In sum, the utility model provides and a kind ofly can apply to the growth such as farmland and have the non-smooth surface of crop to carry out the unmanned plane possessing snap catch ability of soil or water body sampling.
Accompanying drawing explanation
Fig. 1 is the structural representation possessing the unmanned plane of snap catch ability of the prior art.
Fig. 2 is the structural representation possessing the unmanned plane of snap catch ability in the utility model.
Fig. 3 is the structure for amplifying schematic diagram of retractor device in Fig. 2 and sampling probe part.
Fig. 4 is the structural representation of the unmanned plane possessing snap catch ability 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, 301, upper rotating shaft, 302, lower rotary shaft, 303, output gear, 501, cabinet, 502, spool, 503, spool, 504, the first transmission gear, 505, power-transfer clutch, the 506, second transmission gear, 507, hawser, 508, brake equipment.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
2 to accompanying drawing 4 by reference to the accompanying drawings, a kind of unmanned plane possessing snap catch ability, and 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 the lithium cell for powering to consuming parts and the message handler for controlling unmanned plane and telecommunication; It comprises retractor device 5 and sampling probe 6; Described retractor device 5 comprises cabinet 501, spool 502, spool 503, first transmission gear 504, power-transfer clutch 505, second transmission gear 506, hawser 507 and brake equipment 508; Described rotor motor 3 is the dual-axle motor comprising rotating shaft 301 and lower rotary shaft 302; Lower rotary shaft 302 is provided with output gear 303, upper rotating shaft 301 is connected with wing, output gear 303 is connected with the first transmission gear 504, first transmission gear 504 is connected with the second transmission gear 506 by power-transfer clutch 505 simultaneously, second transmission gear 506 is connected with spool 503, spool 503 and the circumferential spacing fit of spool 502, hawser 507 is wound on spool 502, and the free end of hawser 507 is connected with sampling probe 6; Brake equipment 508 is arranged on the end of spool 502; Described cabinet 501 is fixed on rotor motor 3, and spool 503, power-transfer clutch 505 and brake equipment 508 are fixed on casing 501; Rotor motor 3, power-transfer clutch 505, brake equipment 508 and sampling probe 6 are all electrically connected with message handler.
As preferably, described sampling probe 6 is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure, and the periphery of sampling cup is provided with clump weight.
As preferably, described frame 1, rotor 2, rotor motor 3 and leg 4, cabinet 501, spool 502, spool 503, first transmission gear 504, power-transfer clutch 505, second transmission gear 506, hawser 507 and brake equipment 508 are carbon fiber structural.
As improvement, sampling probe 6 is provided with for the bluetooth communication with message handler radio communication.
As improvement, described brake equipment 508 is automatically controlled spiral expanding bar, and described automatically controlled spiral expanding bar is offseted by bar head and spool 502 sidewall and realizes friction braking.
Through facts have proved, after adopting said structure, the utility model has following beneficial effect: it comprises retractor device and sampling probe; Described retractor device comprises cabinet, spool, spool, the first transmission gear, power-transfer clutch, the second transmission gear, hawser and brake equipment; Described rotor motor is the dual-axle motor comprising rotating shaft and lower rotary shaft; Lower rotary shaft is provided with output gear, upper rotating shaft is connected with wing, output gear is connected with the first transmission gear, first transmission gear is connected with the second transmission gear by power-transfer clutch simultaneously, second transmission gear is connected with spool, spool and the spacing fit of spool circumference, hawser is wound on spool, and the free end of hawser is connected with sampling probe; Brake equipment is arranged on the end of spool; Described cabinet is fixed on rotor motor, and spool, power-transfer clutch and brake equipment are fixed on casing; Rotor motor, power-transfer clutch, brake equipment and sampling probe are all electrically connected with message handler.Cleverly adopt dual-axle motor combine with elevator structure, drive spool to rotate by the lower end of rotor motor, so as on carry sampling probe, when sampling probe need whereabouts sample time, be then realized by the deadweight of power-transfer clutch, brake equipment and probe.This practicality when unmanned plane does not land to the soil in the crop growth environment below it or water body sampling, can not have influence on the growth of crop by the combination of retractor device and sampling probe while sampling.Described sampling probe is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure, and the periphery of sampling cup is provided with clump weight.Pointed cone structure can better be inserted in soil, is conducive to sampling cup and collects sample, and clump weight can use the stable whereabouts of sampling cup.Described frame, rotor, rotor motor and leg, cabinet, spool, spool, the first transmission gear, power-transfer clutch, the second transmission gear, hawser and brake equipment 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.Described brake equipment is automatically controlled spiral expanding bar, and described automatically controlled spiral expanding bar is offseted by bar head and spool sidewall and realizes friction braking, and automatically controlled spiral expanding bar structure is simplified more, and braking effect can meet the demand of spool.
In sum, the utility model provides and a kind ofly can apply to the growth such as farmland and have the non-smooth surface of crop to carry out the unmanned plane possessing snap catch ability of soil or water body sampling.
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 (5)
1. possess a unmanned plane for snap catch ability, 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 the lithium cell for powering to consuming parts and the message handler for controlling unmanned plane and telecommunication; It is characterized in that: it comprises retractor device (5) and sampling probe (6); Described retractor device (5) comprises cabinet (501), spool (502), spool (503), the first transmission gear (504), power-transfer clutch (505), the second transmission gear (506), hawser (507) and brake equipment (508); Described rotor motor (3) is the dual-axle motor comprising rotating shaft (301) and lower rotary shaft (302); Lower rotary shaft (302) is provided with output gear (303), upper rotating shaft (301) is connected with wing, output gear (303) is connected with the first transmission gear (504), first transmission gear (504) is connected with the second transmission gear (506) by power-transfer clutch (505) simultaneously, second transmission gear (506) is connected with spool (503), spool (503) and the circumferential spacing fit of spool (502), hawser (507) is wound on spool (502), and the free end of hawser (507) is connected with sampling probe (6); Brake equipment (508) is arranged on the end of spool (502); Described cabinet (501) is fixed on rotor motor (3), and spool (503), power-transfer clutch (505) and brake equipment (508) are fixed on casing (501); Rotor motor (3), power-transfer clutch (505), brake equipment (508) and sampling probe (6) are all electrically connected with message handler.
2. the unmanned plane possessing snap catch ability according to claim 1, is characterized in that: described sampling probe (6) is the sampling cup with heat detector, and described sampling cup lower end is pointed cone structure, and the periphery of sampling cup is provided with clump weight.
3. the unmanned plane possessing snap catch ability according to claim 1, is characterized in that: described frame (1), rotor (2), rotor motor (3) and leg (4), cabinet (501), spool (502), spool (503), the first transmission gear (504), power-transfer clutch (505), the second transmission gear (506), hawser (507) and brake equipment (508) are carbon fiber structural.
4. the unmanned plane possessing snap catch ability according to claim 1, is characterized in that: (6) are provided with for the bluetooth communication with message handler radio communication sampling probe.
5. the unmanned plane possessing snap catch ability according to claim 1, it is characterized in that: described brake equipment (508) is automatically controlled spiral expanding bar, described automatically controlled spiral expanding bar is offseted by bar head and spool (502) sidewall and realizes friction braking.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420695337.4U CN204323680U (en) | 2014-11-19 | 2014-11-19 | Possesses the unmanned plane of snap catch ability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420695337.4U CN204323680U (en) | 2014-11-19 | 2014-11-19 | Possesses the unmanned plane of snap catch ability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204323680U true CN204323680U (en) | 2015-05-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420695337.4U Expired - Fee Related CN204323680U (en) | 2014-11-19 | 2014-11-19 | Possesses the unmanned plane of snap catch ability |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204323680U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105424410A (en) * | 2015-11-12 | 2016-03-23 | 浙江省海洋水产研究所 | Automatic water collecting equipment with water surface points fixed |
| CN105699125A (en) * | 2016-03-09 | 2016-06-22 | 武汉博感空间科技有限公司 | Suspension type UAV (unmanned aerial vehicle) water sampler system |
-
2014
- 2014-11-19 CN CN201420695337.4U patent/CN204323680U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105424410A (en) * | 2015-11-12 | 2016-03-23 | 浙江省海洋水产研究所 | Automatic water collecting equipment with water surface points fixed |
| CN105699125A (en) * | 2016-03-09 | 2016-06-22 | 武汉博感空间科技有限公司 | Suspension type UAV (unmanned aerial vehicle) water sampler system |
| CN105699125B (en) * | 2016-03-09 | 2018-10-30 | 武汉博感空间科技有限公司 | A kind of suspension type unmanned plane water-quality sampler system |
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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 |