CN206766343U - One kind collection sample anticollision unmanned plane - Google Patents
One kind collection sample anticollision unmanned plane Download PDFInfo
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- CN206766343U CN206766343U CN201621041591.8U CN201621041591U CN206766343U CN 206766343 U CN206766343 U CN 206766343U CN 201621041591 U CN201621041591 U CN 201621041591U CN 206766343 U CN206766343 U CN 206766343U
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- fuselage
- unmanned plane
- horn
- collection
- collection sample
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Abstract
The utility model discloses one kind to gather sample anticollision unmanned plane, include fuselage, horn and rotor blade, it is all connected with being provided with horn in the middle part of the side of fuselage four, horn upper end is provided with rotor blade, four horn ends are connected with anti-collision ring, signal receiving module is provided with the left of back, control chip is provided with the right side of signal receiving module, altimeter is provided with the right side of control chip, fuselage lower end is provided with cover cylinder, magnetic envelope is provided with the middle part of cover cylinder, upper magnetic seals up end and is provided with motor, motor output end is connected with draught line, draught line lower end is connected with collection bucket, collection bucket upper end is fixedly installed lower magnetic envelope, fuselage lower end both sides are provided with support frame.The utility model can so be made the data of acquisition have more scale datas, can be obtained more three-dimensional data analysis using sealable lifting bucket collection sample, the positioning of engagement height instrument, and with the addition of anti-collision ring can improve the security of aircraft.
Description
Technical field
A kind of unmanned plane is the utility model is related to, is specifically a kind of collection sample anticollision unmanned plane.
Background technology
UAV, abbreviation unmanned plane（UAV）, it is a kind of new ideas multipurpose equipment being in developing rapidly,
It has maneuverability, be swift in response, unmanned flight and operation require the advantages of relatively low.Unmanned plane is by carrying different practicalities
Device, it can be used for carrying out high-order area detection and sample collection, launch the work(such as small article, real-time imaging transmission at a distance
Energy, it is the strong supplement of satellite remote sensing and traditional air remote sensing.The scope of application of unmanned plane is related to military, scientific research and civilian at present
Three big fields, specifically electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement are seized
The multiple fields application such as private, border patrol and public security anti-terrorism is very wide.
In the prior art, when carrying out sample collection using unmanned plane, harvester is hung using pull rope, the sample of collection
It is easily unrestrained, while also can not effectively carry out gas collecting.
In the prior art, unmanned plane is when in use sometimes because fortuitous event collides, the existing general machine of unmanned plane
Alar part is all located at side end, easily damages in an impact and causes air crash.
Utility model content
The purpose of this utility model is to provide a kind of collection sample anticollision unmanned plane, to solve in above-mentioned background technology
The problem of proposition.
To achieve the above object, the utility model provides following technical scheme：
One kind collection sample anticollision unmanned plane, includes fuselage, horn and rotor blade, the middle part on the side of fuselage four
It is all connected with being provided with horn, the horn upper end is provided with rotor blade, and the rotor blade circle centre position is provided with rotating shaft,
Four horn ends are connected with anti-collision ring, and the anti-collision ring outer ring and the horn are provided with fixed spiral shell with respect to place
Silk, the back left side are provided with signal receiving module, and the signal receiving module upper end is provided with antenna, the signal
Control chip is provided with the right side of receiving module, is provided with altimeter on the right side of the control chip, the fuselage inner bottom part both ends are set
Balancing weight is equipped with, the fuselage lower end is provided with cover cylinder, and magnetic envelope is provided with the middle part of the cover cylinder, and the upper magnetic is sealed up end and set
There is motor, the motor output end is connected with draught line, and the draught line lower end is connected with collection bucket, described to gather on bucket
End is fixedly installed lower magnetic envelope, and fuselage lower end both sides are provided with support frame.
As further program of the utility model：The fuselage is square plastic casing.
As further program of the utility model：The anti-collision ring is the aluminium alloy circle for being enclosed with rubber.
As further program of the utility model：The motor connects with the control chip, the control chip energy
The electric motor starting is enough controlled, the motor is the servomotor for being connected with frequency converter.
As further program of the utility model：The draught line is wire, and the draught line lower end is divided into four strands.
As further program of the utility model：The collection bucket is aluminum alloy hollow bucket, the diameter of the collection bucket
It is smaller 1cm than the cover cylinder.
As further program of the utility model：The control chip can control the lower magnetic envelope and the upper magnetic envelope
Attract each other.
As further program of the utility model：Support frame as described above bottom is pasted with rubber blanket.
Compared with prior art, the beneficial effects of the utility model are：The utility model is matched somebody with somebody using lifting bucket collection sample
The positioning of altimeter is closed, can so make the data of acquisition there are more scale datas, can when carrying out later data analysis
Data statistics is become more three-dimensional；With the addition of anti-collision ring can improve the security of aircraft, can avoid setting in fuselage
Various elements be damaged in accident collision, effectively raise the adaptive type of aircraft；Kept away using controllable magnetic envelope
Exempt to gather the problems such as unrestrained leakage occurs for the sample gathered in bucket, improve the efficiency of collection sample.
Brief description of the drawings
Fig. 1 is a kind of structural representation for gathering sample anticollision unmanned plane.
Fig. 2 is a kind of structural representation for gathering sample anticollision unmanned plane middle fuselage.
In figure：1- fuselages, 2- horns, 3- rotor blades, 4- rotating shafts, 5- anti-collision rings, 6- fixed screws, 7- signals receive mould
Block, 8- antennas, 9- control chips, 10- altimeters, 11- balancing weights, 12- motors, 13- cover cylinders, the upper magnetic envelopes of 14-, 15- draught lines,
16- gathers bucket, and magnetic seals under 17-, 18- support frames.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Refer to Fig. 1~2, in the utility model embodiment, one kind collection sample anticollision unmanned plane, include fuselage 1,
Horn 2 and rotor blade 3, the fuselage 1 are square plastic casing, are all connected with being provided with horn in the middle part of the side of fuselage 1 four
2, the upper end of horn 2 is provided with rotor blade 3, and the rotor blade 3 is spiral sector, the center of circle of rotor blade 3
Place is provided with rotating shaft 4, and the rotor blade 3 can be by the rotating shaft 4 in the surface pivots of horn 2, the rotor blade 3
The thrust that balance can be provided after rotation drives the fuselage 1 to suspend, and four horns 2 end is connected with anticollision
Circle 5, the anti-collision ring 5 are the aluminium alloy circle for being enclosed with rubber, and the anti-collision ring 5 can effectively protect fuselage 1, the anticollision
Enclose 5 outer rings and the horn 2 and place is provided with fixed screw 6, the fixed screw 6 can be by the horn 2 and described anti-
Hit circle 5 to be fixed together, if in use, the anti-collision ring 5 has the phenomenon of damaged aging, the fixation can be dismantled
Screw 6 carries out repairing replacing to the anti-collision ring 5, and the upper left-hand of fuselage 1 is provided with signal receiving module 7, the signal
The upper end of receiving module 7 is provided with antenna 8, and controllers can send signal by handheld remote control device, and the antenna 8 receives
Hand-held device and the UNICOM of the signal receiving module 7, the right side of signal receiving module 7 are provided with control chip 9 after signal,
The control chip 9 can collect the signal data of whole device, and control each several part power set, the control by data
The right side of coremaking piece 9 is provided with altimeter 10, and the altimeter 10 can measure the instant height above sea level where the fuselage 1, and
And pass data at the control chip 9, the inner bottom part of fuselage 1 is provided at both ends with balancing weight 11, the balancing weight 11
Whole device relative equilibrium can be ensured, it is easier to balance is kept in flight, the lower end of fuselage 1 is provided with cover cylinder 13, institute
It is the hollow cylinder for being fixed on the bottom of fuselage 1 to state cover cylinder 13, and the middle part of cover cylinder 13 is provided with magnetic envelope 14, the upper magnetic
Sealing 14 centers and be provided with circular hole, the upper magnetic seals 14 upper ends and is provided with motor 12, and the motor 12 and the control chip 9 connect,
The control chip 9 can control the electric motor starting, and the motor is the servomotor for being connected with frequency converter, and the motor 12 is defeated
Go out end and be connected with draught line 15, the draught line 15 is wire, and the lower end of draught line 15 is divided into four strands, the traction
The lower end of line 15 is connected with collection bucket 16, and the collection bucket 16 is aluminum alloy hollow bucket, the lower end of draught line 15 and the collection
16 inwalls of bucket are fixedly connected, and the motor 12 can be drawn the collection bucket 16 by the draught line 15 and be lifted after starting, institute
Stating collection bucket 16 can be used for gathering air and water sample, and the diameter of the collection bucket 16 is than the 13 small 1cm of cover cylinder, the collection
16 upper ends of bucket are fixedly installed lower magnetic envelope 17, and the control chip 9 can control the lower magnetic envelope 17 and the upper magnetic to seal 14 phases
Mutually attract, the collection bucket 16 enters in the cover cylinder 13 after rising, and the control chip 9 controls the upper magnetic envelope 14 and described
Lower magnetic envelope 17 attracts each other, and can now avoid the gaseous sample in the collection bucket 16 or water sample from overflowing, the lower end of fuselage 1
Both sides are provided with support frame 18, and the bottom of support frame as described above 18 is pasted with rubber blanket, can play buffering when the fuselage 1 lands
Effect.
Operation principle of the present utility model is：When in use, signal receiving module 7 can be connected by hand-held remote control handle
Controlling rotor blade 3 to start by control chip 9 drives fuselage 1 to fly, and in-flight needs to gather air sample and water in fuselage 1
Sample, now control draught line 15 to decline by the controlled motor of control chip 9 and drive collection bucket 16 to decline, now gathering can in bucket 16
To gather air sample or go deep into gathering water sample in waters, after the completion of control collection bucket 16 rise, when collection bucket 16 enter cover cylinder
In 13, magnetic envelope 14 and lower magnetic envelope 17 are attracted each other in control, and the sample for avoiding collecting is unrestrained to be overflowed, the altimeter on fuselage 1
10 are capable of the instant height of real-time display aircraft, and by antenna 8 by data sharing to hand-held remote-control handle, Neng Gouji
The particular location of record collection sample.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (8)
1. one kind collection sample anticollision unmanned plane, includes fuselage, horn and rotor blade, it is characterised in that the fuselage
It is all connected with being provided with horn in the middle part of four sides, the horn upper end is provided with rotor blade, the rotor blade circle centre position
Rotating shaft is provided with, four horn ends are connected with anti-collision ring, and the anti-collision ring outer ring and the horn are set with respect to place
Fixed screw is equipped with, is provided with signal receiving module on the left of the back, the signal receiving module upper end is provided with day
Line, control chip is provided with the right side of the signal receiving module, is provided with altimeter on the right side of the control chip, in the fuselage
Bottom is provided at both ends with balancing weight, and the fuselage lower end is provided with cover cylinder, and magnetic envelope, the upper magnetic are provided with the middle part of the cover cylinder
Seal up end and be provided with motor, the motor output end is connected with draught line, and the draught line lower end is connected with collection bucket, institute
State collection bucket upper end and be fixedly installed lower magnetic envelope, fuselage lower end both sides are provided with support frame.
2. a kind of collection sample anticollision unmanned plane according to claim 1, it is characterised in that the fuselage is square
Plastic casing.
3. a kind of collection sample anticollision unmanned plane according to claim 1, it is characterised in that the anti-collision ring is parcel
There is the aluminium alloy circle of rubber.
4. a kind of collection sample anticollision unmanned plane according to claim 1, it is characterised in that the motor and the control
Coremaking piece connects, and the control chip can control the electric motor starting, and the motor is the servomotor for being connected with frequency converter.
5. a kind of collection sample anticollision unmanned plane according to claim 1, it is characterised in that the draught line is steel wire
Line, the draught line lower end are divided into four strands.
6. a kind of collection sample anticollision unmanned plane according to claim 1, it is characterised in that the collection bucket closes for aluminium
Golden hollow barrel, the diameter of the collection bucket are smaller 1cm than the cover cylinder.
7. a kind of collection sample anticollision unmanned plane according to claim 1, it is characterised in that the control chip can be with
The lower magnetic envelope and the upper magnetic envelope is controlled to attract each other.
8. a kind of collection sample anticollision unmanned plane according to claim 1, it is characterised in that glue support frame as described above bottom
Post rubber blanket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621041591.8U CN206766343U (en) | 2016-09-08 | 2016-09-08 | One kind collection sample anticollision unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621041591.8U CN206766343U (en) | 2016-09-08 | 2016-09-08 | One kind collection sample anticollision unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206766343U true CN206766343U (en) | 2017-12-19 |
Family
ID=60646889
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201621041591.8U Active CN206766343U (en) | 2016-09-08 | 2016-09-08 | One kind collection sample anticollision unmanned plane |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622426A (en) * | 2018-04-26 | 2018-10-09 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN109239499A (en) * | 2018-11-02 | 2019-01-18 | 江苏嘉顿威尔电气有限公司 | A kind of detection platform of unmanned plane lightning protection detection system |
| CN110001933A (en) * | 2019-04-06 | 2019-07-12 | 胡永星 | A kind of unmanned plane keeping stable state by changing center of gravity |
| CN110108521A (en) * | 2019-06-12 | 2019-08-09 | 李茜 | A kind of gas sample case for atmospheric monitoring |
| CN114508134A (en) * | 2022-03-15 | 2022-05-17 | 盛东如东海上风力发电有限责任公司 | Underwater robot for underwater detection in offshore wind power single pile |
-
2016
- 2016-09-08 CN CN201621041591.8U patent/CN206766343U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622426A (en) * | 2018-04-26 | 2018-10-09 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN108622426B (en) * | 2018-04-26 | 2019-11-08 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN109239499A (en) * | 2018-11-02 | 2019-01-18 | 江苏嘉顿威尔电气有限公司 | A kind of detection platform of unmanned plane lightning protection detection system |
| CN110001933A (en) * | 2019-04-06 | 2019-07-12 | 胡永星 | A kind of unmanned plane keeping stable state by changing center of gravity |
| CN110108521A (en) * | 2019-06-12 | 2019-08-09 | 李茜 | A kind of gas sample case for atmospheric monitoring |
| CN114508134A (en) * | 2022-03-15 | 2022-05-17 | 盛东如东海上风力发电有限责任公司 | Underwater robot for underwater detection in offshore wind power single pile |
| CN114508134B (en) * | 2022-03-15 | 2024-01-23 | 盛东如东海上风力发电有限责任公司 | Underwater robot for underwater detection in offshore wind power single pile |
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