CN206360441U - Distributed unmanned plane charging hangar - Google Patents
Distributed unmanned plane charging hangar Download PDFInfo
- Publication number
- CN206360441U CN206360441U CN201621157163.1U CN201621157163U CN206360441U CN 206360441 U CN206360441 U CN 206360441U CN 201621157163 U CN201621157163 U CN 201621157163U CN 206360441 U CN206360441 U CN 206360441U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- hangar
- solar panel
- batteries
- charging
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 claims abstract description 5
- 230000005611 electricity Effects 0.000 claims abstract description 5
- 238000004891 communication Methods 0.000 claims description 7
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 4
- 229910052744 lithium Inorganic materials 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 238000002048 anodisation reaction Methods 0.000 claims description 3
- 239000000446 fuel Substances 0.000 claims description 3
- 230000006698 induction Effects 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 230000007246 mechanism Effects 0.000 claims description 3
- 229910052760 oxygen Inorganic materials 0.000 claims description 3
- 239000001301 oxygen Substances 0.000 claims description 3
- 230000009467 reduction Effects 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- JDZCKJOXGCMJGS-UHFFFAOYSA-N [Li].[S] Chemical compound [Li].[S] JDZCKJOXGCMJGS-UHFFFAOYSA-N 0.000 claims description 2
- 239000000428 dust Substances 0.000 claims description 2
- 239000007769 metal material Substances 0.000 claims description 2
- 239000004576 sand Substances 0.000 claims description 2
- 230000008719 thickening Effects 0.000 claims description 2
- 239000004922 lacquer Substances 0.000 claims 1
- 238000010422 painting Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 5
- 230000003287 optical effect Effects 0.000 description 4
- 239000002253 acid Substances 0.000 description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 239000000523 sample Substances 0.000 description 3
- 230000003028 elevating effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/56—Power conversion systems, e.g. maximum power point trackers
Landscapes
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Photovoltaic Devices (AREA)
Abstract
The utility model discloses a kind of distributed unmanned plane charging hangar, comprising：Hangar protection casing, airplane parking area, wireless charging module, single-chip microcomputer（Main control computer）, can the solar panel of slip lid, batteries, GPS/ Big Dipper positioning and communicating modules.Wherein single-chip microcomputer（Main control computer）, solar panel and batteries constitute one-level charging system, solar energy is stored in battery using solar panel；Wireless charging module and batteries constitute two grades of charging systems, and the electric energy of batteries is filled into the unmanned plane to poor electricity condition, single-chip microcomputer（Main control computer）The slip lid state of solar panel is controlled, driving solar panel covers protection unmanned plane or driving solar panel is opened, and berths or takes off to for unmanned plane.Thus, the hangar possess unmanned plane berth, protect, charging, the function such as positioning and communicating.Due to being configured with solar panel, the hangar distributed in the wild can be disposed and can accommodate several frame unmanned planes.The features such as the utility model has non-maintaining, long-life, off-line using.
Description
Technical field
The utility model is related to multi-rotor unmanned aerial vehicle technical field, and in particular to a kind of unmanned plane charging hangar.
Background technology
Multi-rotor unmanned aerial vehicle is a kind of unmanned plane for possessing hovering function, is in the past few years developed swift and violent.Taking photo by plane, tieing up inspection, plant
Guarantor, the in short-term field such as monitoring are using more and more.Especially for large area is unattended, special rugged environment (such as water
Storehouse, power station), its replace manually carry out it is on duty, observation, increase operating efficiency while, greatly reduce work danger and
Cost, is the application of great potential.But the bottleneck of multi-rotor unmanned aerial vehicle is short (within 30 minutes) in the flight time at present, fly
On row distance short (within 2km), often result in people and run at random, situations such as constantly changing battery.Unmanned plane is realized to a certain degree
Human capital reduction, but due to the bottleneck of the energy, it is impossible to real to realize the unmanned tasks carrying participated in.
For example, patent document (CN 205178593U) proposes the platform structure charged using solar energy to unmanned plane
Think, but deficiency is conceived to unmanned plane usage scenario, only meet charging, under the unmanned state without considering unmanned plane
Protection, communication, practical value is not high.The utility model constructs an energy and unmanned plane from the application scenarios of unmanned plane
Communicate, berthed for unmanned plane, and the system charged again under guard mode to unmanned plane, fill up the blank of the technical field.
The content of the invention
The utility model utilizes the skills such as solar energy, wireless charging, the positioning of the GPS/ Big Dippeves from the application scenarios of unmanned plane
Art is combined, and realizes the integral application berthed, protect, charge, positioned to unmanned plane.The hardware can help unmanned plane true
Unattended long endurance flight is realized in positive meaning.
The utility model devises a kind of unmanned plane charging hangar that distributed can be disposed.Hangar by hangar protect casing,
Airplane parking area, wireless charging module, single-chip microcomputer, can the solar panel of slip lid, batteries, GPS/ Big Dipper positioning and communicating module groups
Into.
Hangar can freely be distributed in no Grid, and the parking place of unmanned plane is informed by positioning signal, to poor electric
Unmanned plane carries out that in recharging, charging process the protection to unmanned plane can be realized.Even if the unmanned plane without charge requirement
It can be docked in hangar and seek asylum in harsh climate.
Hangar protection casing is made up of the good metal material of the weatherability such as aluminium alloy or stainless steel.Surface is applied
The list processing technique such as paint, anodization.The casing has the features such as acid and alkali-resistance, rainwater-proof, high intensity, impact resistance, is adapted to each
Harsh weather is planted, comprehensive protection is provided in unmanned plane therein to berthing.In a side roof part of casing, communication day is installed
Line, sends positioning signal, data transmission antenna can be also expanded to according to demand.
Airplane parking area is made up of high-strength insulating light sheet material.Airplane parking area possesses certain elevating function, is adapted to difference
The unmanned plane of size berths.Insulating thin reply is infrared or visible ray transparent, is easy to wireless charging module to unmanned seat in the plane
The optical search put.The thickness of insulating thin should be controlled strictly, it is to avoid the efficiency of reduction wireless charging.
Wireless charging module is located at the lower section of airplane parking area, and is close to airplane parking area thin plate.It should be entered according to required charge power
Row selection.The use induction type wireless charging module of small-power charging；The use resonance type wireless charging module of high-power charging.
Wireless charging module is furnished with optical alignment probe and mechanical movement function, to realize that wireless charging module can be accurately close to nobody
Machine, and the wireless charging receiving module matching in effective transmission range with unmanned plane.
Can slip lid solar panel be located at hangar protect casing top, be both the supply of the main source of energy of hangar, be also machine
The top protection board in storehouse.Battery charging sunny when for whole hangar, keeps the energy of hangar to fill.When
When receiving the demand that unmanned plane needs berth, solar panel sliding opening exposes airplane parking area.After unmanned plane is fully charged,
Solar panel sliding opening, unmanned plane takes off from airplane parking area.When receive unmanned plane need to berth protection demand after, the sun
Cell panel sliding opening, after unmanned plane berths, on slide lid.The package surface of the solar panel of solar panel should be carried out
Thickening is handled, and is hit with dealing with special atrocious weather (such as hail, sand and dust) and unmanned plane once in a while.
Batteries can use lead-acid battery, power lithium battery, lithium-sulfur cell, hydrogen according to cost and use requirement
Oxygen fuel cell etc..Batteries should possess ability simultaneously to multi rack unmanned plane charging simultaneously.Batteries should possess electricity
Pressure, the monitoring of electric current, easy access.
The beneficial effects of the utility model are：Integration solve the charging of unmanned plane, berth, protect, location requirement.
Solar power generation reduces the bracing wire cost of distributed placement；Wireless charging solves unmanned plane hardly possible positioning and is difficult to contact electric charging
Problem；Hangar solves the survival ability of unmanned plane in the presence of a harsh environment, reduces the maintenance cost of unmanned plane.For real meaning
Unmanned plane in justice performs the unmanned task of long-time there is provided possible.
Brief description of the drawings
Fig. 1 is the structural representation of distributed unmanned plane charging hangar,
Fig. 2 regards sectional view for the B-B direction of Fig. 1 distributed unmanned plane charging hangar,
The A-A regarding sectional views for the distributed unmanned plane charging hangar that Fig. 3 is Fig. 1.
Fig. 4 be distributed unmanned plane charging hangar can the solar panel of slip lid open plan structure when exposing airplane parking area
Schematic diagram.
Symbol description
1st, hangar protection casing；
2nd, airplane parking area；
3rd, wireless charging module；
4th, single-chip microcomputer；
5th, can slip lid solar panel；
6th, batteries；
7th, GPS/ Big Dippeves positioning and communicating module；
8th, communication antenna；
9th, drive mechanism；
10th, optical alignment is popped one's head in；
11st, XY twin shafts mobile platform.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, it is right exemplified by accompanying drawing
This utility model is further elaborated.It should be appreciated that specific implementation method described herein is only used for explaining this
Utility model, does not limit the utility model.
Unmanned plane charging hangar includes hangar protection casing (1), airplane parking area (2), wireless charging module (3), single-chip microcomputer
(4), can the solar panel (5) of slip lid, batteries (6), GPS/ Big Dipper positioning and communicating modules (7).
The single-chip microcomputer（Main control computer）(4), the solar panel (5) and the batteries (6) constitute one-level
Solar energy, is stored in battery by charging system using solar panel (5).
The wireless charging module (3) and the batteries (6) constitute two grades of charging systems, by batteries (6)
Electric energy fills the unmanned plane to poor electricity condition.
The single-chip microcomputer（Main control computer）(4) the slip lid state of control solar panel (5), drives solar panel
(5) cover protection unmanned plane or driving solar panel (5) is opened, berth or take off to for unmanned plane.
It is preferred that, hangar protection casing (1) selection aluminium alloy or stainless steel etc. are machined into.Surface painted,
The list processing technique such as anodization.There is communication antenna (data transmission antenna) (8) extraction in the side of casing.It should be drawn in casing processing
Divide some functional areas, as shown in FIG. 1 to 3, batteries installing zone, single-chip microcomputer installing zone, positioning are followed successively by from the bottom to top
Communication module installing zone, wireless charging module installing zone, airplane parking area installing zone, solar panel installing zone.Wherein batteries
Installation region should be noted that insulation protection and sealing property.Batteries (6) installation region should be easy to radiating close proximity to casing.
One-chip computer module (4) can be close to lower shoe, be easy to radiating.
It is preferred that, airplane parking area (2) are made up of high-strength insulating light sheet material.Airplane parking area (2) possesses certain elevating function,
Different size of unmanned plane is adapted to berth.The lower section of insulation board is provided with rhone, can exclude rainwater in time, protects simultaneously
The batteries of lower section, single-chip microcomputer, positioning and communicating module be not by rain erosion.
It is preferred that, wireless charging module is located at the lower section of airplane parking area, and is close to airplane parking area thin plate.As shown in FIG. 1 to 3,
Wireless charging module is installed on XY twin shafts mobile platform (11) equipped with optical alignment probe (10).Optic probe (10) is found
Unmanned plane witness marker and by feedback of the information to single-chip microcomputer (4), and guides platform to move by single-chip microcomputer (4) control.Wireless charging
Module should try one's best the big wire of selection stroke, such as spring wire, it is to avoid wire harness moving process tension snaps or excessively loose mounting board.
After wireless charging module is started to charge up, mobile platform power supply should be cut off, it is to avoid malfunction.Wireless charging module (3) can be according to nobody
Charge power is selected needed for machine, low power use induction type wireless charging module, powerful use resonance type wireless
Charging module.
It is preferred that, in the chute that solar panel (5) is installed at the top of hangar, it is covered by driving stepper motor, step
Stepper motor is controlled by the instruction of single-chip microcomputer (4).Limiter is provided with the both sides of chute.Solar panel should it is symmetrical simultaneously
Synchronously cover, as shown in Figure 4, it is to avoid unnecessary centre-of gravity shift.
It is preferred that, batteries (6) can use lead-acid battery, power lithium battery, lithium according to cost and use requirement
Sulphur battery, hydrogen-oxygen fuel cell etc..The voltage of batteries, the Monitoring Data of electric current should set panel to be showed on cabinet
It is real, or data communication module is passed into control terminal.
It is preferred that, erection sequence of each module (part) in hangar protection casing is：Single-chip microcomputer (4), batteries
(6), GPS/ Big Dippeves positioning and communicating module (7), XY twin shafts mobile platform (10), wireless charging module (3), airplane parking area (2), the sun
Cell panel drive mechanism (9), solar panel (5).
Claims (6)
1. a kind of distributed unmanned plane charging hangar, it is characterised in that include：Hangar protection casing (1), airplane parking area (2), wireless
Charging module (3), single-chip microcomputer (4), can the solar panel (5) of slip lid, batteries (6), GPS/ Big Dipper positioning and communicating modules
(7), the single-chip microcomputer (4), the solar panel (5) and the batteries (6) constitute one-level charging system, utilize the sun
Solar energy is stored in battery by cell panel (5), and the wireless charging module (3) and the batteries (6) constitute two grades
Charging system, the unmanned plane to poor electricity condition is filled by the electric energy of batteries (6), and the single-chip microcomputer (4) calculates for system master
Machine, slip lid state, the search of wireless charging module (3) and the motion of control solar panel (5) and GPS/ Big Dipper positioning and communicatings
The transmission-receiving function of module (7).
2. distribution unmanned plane charging hangar as claimed in claim 1, it is characterised in that the hangar protection casing (1) by
The metal material of the good weatherability such as aluminium alloy or stainless steel is constituted, and surface should have lacquer painting to protect or anodization, it is to avoid
Reflected light disturbs unmanned plane optics, has communication antenna (8) to draw data transmission antenna in the side of casing.
3. distribution unmanned plane charging hangar as claimed in claim 1, it is characterised in that the airplane parking area (2) is by high-strength exhausted
Edge light sheet material is constituted, it is to avoid reduction wireless charging efficiency.
4. distribution unmanned plane charging hangar as claimed in claim 1, it is characterised in that the wireless charging module (3) is adopted
With induction type wireless charging mode or resonance type wireless charging modes.
5. distribution unmanned plane charging hangar as claimed in claim 1, it is characterised in that can slip lid the solar panel
(5) it is made up of solar panel with corresponding drive mechanism (9), slip lid action, sun electricity is carried out under single-chip microcomputer (5) control
The package surface of pond plate should carry out thickening processing, to deal with the especially atrocious weather such as hail, sand and dust.
6. distribution unmanned plane charging hangar as claimed in claim 1, it is characterised in that the batteries (6) use lead
Sour battery, power lithium battery, lithium-sulfur cell or hydrogen-oxygen fuel cell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621157163.1U CN206360441U (en) | 2016-10-25 | 2016-10-25 | Distributed unmanned plane charging hangar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621157163.1U CN206360441U (en) | 2016-10-25 | 2016-10-25 | Distributed unmanned plane charging hangar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206360441U true CN206360441U (en) | 2017-07-28 |
Family
ID=59369216
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621157163.1U Expired - Fee Related CN206360441U (en) | 2016-10-25 | 2016-10-25 | Distributed unmanned plane charging hangar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206360441U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106368478A (en) * | 2016-10-25 | 2017-02-01 | 任连萌 | Distributed unmanned aerial vehicle charging machine hangar |
| CN110608727A (en) * | 2019-11-06 | 2019-12-24 | 青岛罗博飞海洋技术有限公司 | Seaweed bed monitoring system and method |
-
2016
- 2016-10-25 CN CN201621157163.1U patent/CN206360441U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106368478A (en) * | 2016-10-25 | 2017-02-01 | 任连萌 | Distributed unmanned aerial vehicle charging machine hangar |
| CN110608727A (en) * | 2019-11-06 | 2019-12-24 | 青岛罗博飞海洋技术有限公司 | Seaweed bed monitoring system and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200904 Address after: 200050 floor 1, building 6, No. 525, Yuanjiang Road, Minhang District, Shanghai Patentee after: Shanghai Hanjun automation equipment Co.,Ltd. Address before: 200240, room 406, 1007 Binchuan Road, Shanghai, Minhang District Co-patentee before: Dai Wei Patentee before: Ren Lianmeng |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170728 |