CN205872493U - Unmanned vehicles sampled data control system - Google Patents
Unmanned vehicles sampled data control system Download PDFInfo
- Publication number
- CN205872493U CN205872493U CN201620813943.0U CN201620813943U CN205872493U CN 205872493 U CN205872493 U CN 205872493U CN 201620813943 U CN201620813943 U CN 201620813943U CN 205872493 U CN205872493 U CN 205872493U
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- aircraft fuselage
- aircraft
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- sensor
- central processing
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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- Sampling And Sample Adjustment (AREA)
Abstract
The utility model belongs to unmanned vehicles control field especially relates to an unmanned vehicles sampled data control system, include aircraft fuselage, central processing unit, solar cell panel, battery, baroceptor, air flow sensor, air velocity transducer, GPS locator, color video camera, photosensitive sensor, siren, lift drive, drive the bird ware, the lower wing of aircraft fuselage both sides, fin, aircraft fuselage's front end all is equipped with an infrared ray sensor, aircraft fuselage's both sides are equipped with the colored flash light of a plurality of LED respectively, aircraft fuselage's top is equipped with atmospheric pollutants granule sample thief, the top of atmospheric pollutants granule sample thief is equipped with can dismantle rain -proof cover, not only can gather empty gas sample article according to the size of wind speed and air current, can also break down to the aircraft through safety airbag device and protect when dropping, has avoided aircraft and atmospheric pollutants granule sample thief to damage.
Description
Technical field
This utility model belongs to unmanned vehicle control field, particularly relates to a kind of unmanned vehicle sampled-data control system.
Background technology
Air sampler is known in the art, and the current regular air method of sampling is mainly carried by staff
Atmosphere sampling instrument carries out spot sampling, or sets sampled point in appointed place, lays high-tech analytical tool, directly will divide
Analysing the data of gained and be sent to environmental protection by network, both sample modes cut both ways, and the former motility is high, but expend big
Amount time and manpower and materials, although the latter's precision is high, speed is fast, but mobile dumb, and acquisition range is limited, it is most important that
The cost that it is high, the most all more than million RMB.And strategically located and difficult of access landform is being let out with adverse circumstances such as poisonous chemical gas
Leakage, or the air sampling aspect that the special occasions such as overhanging cliff is carried out, if by sample collector's manual operation, it is necessary to personal
Go through dangers, not only have life dangerous, and pressure is big at heart, affects sampling work.
Utility model content
The purpose of this utility model is for above-mentioned deficiency present in prior art, proposes a kind of unmanned vehicle sampling
Control system, is possible not only to the size according to wind speed and air-flow and gathers air sample, it is also possible to by air bag device to flying
Row device breaks down and protects when dropping, it is to avoid aircraft and atmosphere pollution particle sampler damage, and by can
Dismounting rain cover and lightning arrester achieve aircraft and can gather air sample in the rain.
This utility model solves it and technical problem is that and realize by the following technical solutions:
A kind of unmanned vehicle sampled-data control system, including aircraft fuselage, central processing unit, solar panel, storage
Battery, baroceptor, pneumatic sensor, air velocity transducer, GPS locator, color video camera, light sensor, siren,
Lifting drive, bird-scaring unit；
Described aircraft fuselage be respectively provided on two sides with top wing and lower wing, the rear end of described aircraft fuselage is provided with tail
The wing, described solar panel is respectively arranged at the empennage of described aircraft fuselage and the upper machine of the both sides of described aircraft fuselage
On the wing, the lower wing of the both sides of described aircraft fuselage and described aircraft fuselage is all wound with fluorescent belt, described aircraft
The bottom of fuselage is provided with air bag device and distance measuring sensor；
The lower wing of described aircraft fuselage both sides, empennage, the front end of aircraft fuselage are equipped with an infrared ray sensing
Device, described aircraft fuselage be respectively provided on two sides with multiple LED alternating flashing light, the top of described aircraft fuselage is provided with air
Contaminant particle sampler, is provided with multiple storage bag, described atmospheric pollution composition granule in described atmosphere pollution particle sampler
Sampler is provided with timer, and the top of described atmosphere pollution particle sampler is provided with detachable rain cover, described detachably
The top of rain cover is provided with lightning arrester, is provided with rechargeable battery, described solar energy in described atmosphere pollution particle sampler
Cell panel is connected with accumulator, and described accumulator is connected with described central processing unit, rechargeable battery respectively, described colored shooting
Machine is arranged on the top wing of aircraft fuselage side；
Described infrared ray sensor, baroceptor, pneumatic sensor, air velocity transducer, GPS locator, range finding sensing
Device, video camera, light sensor all inputs with described central processing unit are connected, described LED alternating flashing light, timer,
Siren, lifting drive, bird-scaring unit, atmosphere pollution particle sampler, trigger device all with described central processing unit
Outfan connects；
Being respectively equipped with bird-scaring unit on the lower wing of the both sides of described aircraft fuselage, described lifting drive is arranged at and flies
The inside of row device fuselage.
Preferably, described aircraft atmospheric pollution granule sampled-data control system also includes wireless communication apparatus, manual operation
Dish, ground control terminal, display, and described wireless communication apparatus controls terminal with central processing unit, ground respectively and is connected, described
Manual operation dish controls terminal with ground and is connected, and described ground controls terminal and is connected with display.
Preferably, the inside of described aircraft fuselage is provided with battery backup, and described battery backup is connected with accumulator.
Compared with prior art, this utility model produces and provides the benefit that: provide a kind of unmanned vehicle controlling of sampling
System, is possible not only to the size according to wind speed and air-flow and gathers air sample, it is also possible to by air bag device to aircraft
Break down and protect when dropping, it is to avoid aircraft and atmosphere pollution particle sampler damage, and are gathering in the rain
During air sample, protect aircraft and atmosphere pollution particle sampler by detachable rain cover and lightning arrester, and
By being provided with infrared ray sensor and scarer, it is to avoid aircraft is clashed into and damages, and is surveyed by light sensor
Determine light intensity, controlled the opening time of LED alternating flashing light by central processing unit, improve aircraft distinguishing at night
Knowledge and magnanimity, and it is wound with fluorescent belt by lower wing, can make aircraft after running into fault night, be easily found.
Accompanying drawing explanation
Below in conjunction with the accompanying drawings this utility model is further illustrated:
Fig. 1 is system diagram of the present utility model；
Fig. 2 is Flight Vehicle Structure schematic diagram；
Fig. 3 is detachable rain cover structure chart.
Wherein: 1, aircraft fuselage；2, top wing；3, lower wing；4, empennage；5, atmosphere pollution particle sampler；6、
Infrared ray sensor；7, LED alternating flashing light；8, bird-scaring unit；9, color video camera；10, detachable rain cover；11, lightning-arrest dress
Put.
Detailed description of the invention
Below in conjunction with embodiment, this utility model is described further:
As Figure 1-3, this utility model provides a kind of unmanned vehicle sampled-data control system, including aircraft fuselage 1,
Central processing unit, solar panel, accumulator, baroceptor, pneumatic sensor, air velocity transducer, GPS locator, coloured silk
Color video camera 9, light sensor, siren, lifting drive, bird-scaring unit 8；
Described aircraft fuselage 1 be respectively provided on two sides with top wing 2 and lower wing 3, the rear end of described aircraft fuselage sets
Empennage 4, described solar panel is had to be respectively arranged at empennage 4 and the both sides of described aircraft fuselage of described aircraft fuselage
Top wing 2 on, the lower wing 3 of the both sides of described aircraft fuselage and described aircraft fuselage is all wound with fluorescent belt, institute
The bottom stating aircraft fuselage is provided with air bag device and distance measuring sensor；
The lower wing of described aircraft fuselage 1 both sides, empennage, the front end of aircraft fuselage are equipped with an infrared ray sensing
Device 6, described aircraft fuselage be respectively provided on two sides with multiple LED alternating flashing light 7, the top of described aircraft fuselage is provided with greatly
Gas contaminant particle sampler 5, is provided with multiple storage bag, described atmosphere pollution in described atmosphere pollution particle sampler 5
Particle sampler 5 is provided with timer, and the top of described atmosphere pollution particle sampler is provided with detachable rain cover 10, described
The top of detachable rain cover 10 is provided with lightning arrester 11, is provided with rechargeable battery in described atmosphere pollution particle sampler 5,
Described solar panel is connected with accumulator, and described accumulator is connected with described central processing unit, rechargeable battery respectively, institute
State color video camera 9 to be arranged on the top wing 2 of aircraft fuselage 1 side；
Described infrared ray sensor, baroceptor, pneumatic sensor, air velocity transducer, GPS locator, range finding sensing
Device, video camera, light sensor all inputs with described central processing unit are connected, described LED alternating flashing light, timer,
Siren, lifting drive, bird-scaring unit, atmosphere pollution particle sampler, trigger device all with described central processing unit
Outfan connects；
Being respectively equipped with bird-scaring unit 8 on the lower wing 3 of the both sides of described aircraft fuselage 1, described lifting drive is arranged
Inside in aircraft fuselage.
Described aircraft atmospheric pollution granule sampled-data control system also includes wireless communication apparatus, manual operation dish, ground
Controlling terminal, display, described wireless communication apparatus controls terminal with central processing unit, ground respectively and is connected, described artificial behaviour
Making dish to be connected with ground control terminal, described ground controls terminal and is connected with display.
The inside of described aircraft fuselage is provided with battery backup, and described battery backup is connected with accumulator.
The operation principle of this unmanned vehicle sampled-data control system is: when sampling, and controlling terminal by ground will
Aircraft flies to appointed place, in flight course, is provided with by the empennage of aircraft fuselage 1, both sides lower wing 3 and front end
Infrared ray sensor 6, the distance around birds and aircraft fuselage 1 can be monitored, around birds and aircraft fuselage 1
When distance is more than risk distance, process by communicating information to central processing unit, thus control bird-scaring unit 8 and open and carry out
Drive, when the distance around birds and aircraft fuselage 1 is less than risk distance, controls lifting by central processing unit and drive dress
Put and raise, it is to avoid with birds bump against, when aircraft flies to appointed place laggard row air sampling, by air velocity transducer,
The data recorded are transferred to central processing unit and process by pneumatic sensor, baroceptor, when meeting the requirements, by
Central processor opens timer and atmosphere pollution particle sampler 5 is sampled, and carries out timing by timer, when arrival sets
When fixing time, open another storage bag while closing a storage bag by central processing unit and be collected, by being provided with
Solar panel aircraft can be made to carry out long-distance flight, save power supply simultaneously, taken the photograph by colour while sampling
Surrounding is taken pictures by camera 9, is sent to central processing unit and is sent to ground control terminal by wireless transport module again,
Shown by display screen, surrounding can be observed, when aircraft is in night flying, pass through light sensor
The light intensity recorded is sent to central processing unit, when light intensity is less than setting, opens LED alternating flashing light 7, carry
The identification of high aircraft, when dropping when aircraft breaks down in flight course, measures flight by distance measuring sensor
Distance between device and ground, when less than setting, controls air bag device by central processing unit and opens, to aircraft
Protect, open siren simultaneously, remind the crowd on ground to note having object to land, it is to avoid human body is damaged, when
Detachable rain cover 10 and lightning arrester can be installed to the top of atmosphere pollution particle sampler 5 when the rainy day samples
11, aircraft fuselage 1 and atmosphere pollution particle sampler 5 are protected.
This system is possible not only to the size according to wind speed and air-flow and gathers air sample, it is also possible to pass through air bag device
Aircraft is broken down when dropping and protect, it is to avoid aircraft and atmosphere pollution particle sampler damage, and lead to
Cross detachable rain cover and lightning arrester achieves aircraft and can gather air sample in the rain.
It is described in detail of the present utility model above by embodiment, but described content is the most of the present utility model
Preferred embodiment, it is impossible to be considered for limiting practical range of the present utility model.All made according to this utility model application range
Impartial change and improvement etc., within all should still belonging to patent covering scope of the present utility model.
Claims (3)
1. a unmanned vehicle sampled-data control system, it is characterised in that: include aircraft fuselage (1), central processing unit, the sun
Can cell panel, accumulator, baroceptor, pneumatic sensor, air velocity transducer, GPS locator, color video camera (9), photosensitive
Sensor, siren, lifting drive, bird-scaring unit (8)；
Described aircraft fuselage (1) be respectively provided on two sides with top wing (2) and lower wing (3), the rear end of described aircraft fuselage
Being provided with empennage (4), described solar panel is respectively arranged at the empennage (4) of described aircraft fuselage and described aircraft fuselage
Both sides top wing (2) on, the lower wing (3) of the both sides of described aircraft fuselage and described aircraft fuselage is all wound with
Fluorescent belt, the bottom of described aircraft fuselage is provided with air bag device and distance measuring sensor；
The lower wing of described aircraft fuselage (1) both sides, empennage, the front end of aircraft fuselage are equipped with an infrared ray sensor
(6), described aircraft fuselage be respectively provided on two sides with multiple LED alternating flashing light (7), the top of described aircraft fuselage is provided with
Atmosphere pollution particle sampler (5), is provided with multiple storage bag, described air in described atmosphere pollution particle sampler (5)
Contaminant particle sampler (5) is provided with timer, and the top of described atmosphere pollution particle sampler is provided with the most rainproof
Cover (10), the top of described detachable rain cover (10) is provided with lightning arrester (11), described atmosphere pollution particle sampler (5)
In be provided with rechargeable battery, described solar panel is connected with accumulator, described accumulator respectively with described central processing unit,
Rechargeable battery connects, and described color video camera (9) is arranged on the top wing (2) of aircraft fuselage (1) side；
Described infrared ray sensor, baroceptor, pneumatic sensor, air velocity transducer, GPS locator, distance measuring sensor, take the photograph
Camera, light sensor all inputs with described central processing unit are connected, described LED alternating flashing light, timer, alarm
Device, lifting drive, bird-scaring unit, atmosphere pollution particle sampler, trigger device all with the output of described central processing unit
End connects；
Being respectively equipped with bird-scaring unit (8) on the lower wing (3) of the both sides of described aircraft fuselage (1), described lifting drive sets
It is placed in the inside of aircraft fuselage.
A kind of aircraft sampled-data control system the most according to claim 1, it is characterised in that: described aircraft atmospheric pollution
Granule sampled-data control system also includes that wireless communication apparatus, manual operation dish, ground control terminal, display, described channel radio
News device controls terminal with central processing unit, ground respectively and is connected, and described manual operation dish controls terminal with ground and is connected, described
Ground controls terminal and is connected with display.
A kind of aircraft sampled-data control system the most according to claim 1, it is characterised in that: described aircraft fuselage interior
Portion is provided with battery backup, and described battery backup is connected with accumulator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620813943.0U CN205872493U (en) | 2016-07-26 | 2016-07-26 | Unmanned vehicles sampled data control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620813943.0U CN205872493U (en) | 2016-07-26 | 2016-07-26 | Unmanned vehicles sampled data control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205872493U true CN205872493U (en) | 2017-01-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620813943.0U Expired - Fee Related CN205872493U (en) | 2016-07-26 | 2016-07-26 | Unmanned vehicles sampled data control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205872493U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107402399A (en) * | 2017-09-06 | 2017-11-28 | 郑州大学 | Birds backpack positions and communication system and communication means |
| WO2019131583A1 (en) * | 2017-12-28 | 2019-07-04 | 国立大学法人名古屋大学 | Particle capturer and rotorcraft comprising same |
-
2016
- 2016-07-26 CN CN201620813943.0U patent/CN205872493U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107402399A (en) * | 2017-09-06 | 2017-11-28 | 郑州大学 | Birds backpack positions and communication system and communication means |
| WO2019131583A1 (en) * | 2017-12-28 | 2019-07-04 | 国立大学法人名古屋大学 | Particle capturer and rotorcraft comprising same |
| CN112074722A (en) * | 2017-12-28 | 2020-12-11 | 国立大学法人东海国立大学机构 | Particle trap and rotorcraft provided with same |
| JPWO2019131583A1 (en) * | 2017-12-28 | 2021-10-21 | 国立大学法人東海国立大学機構 | Particle trap and rotary wing aircraft equipped with it |
| JP7240676B2 (en) | 2017-12-28 | 2023-03-16 | 国立大学法人東海国立大学機構 | Particle trap and rotorcraft equipped with the same |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170111 Termination date: 20200726 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |