CN107010240A - A kind of solar recharging landing platform of unmanned plane - Google Patents
A kind of solar recharging landing platform of unmanned plane Download PDFInfo
- Publication number
- CN107010240A CN107010240A CN201710335082.9A CN201710335082A CN107010240A CN 107010240 A CN107010240 A CN 107010240A CN 201710335082 A CN201710335082 A CN 201710335082A CN 107010240 A CN107010240 A CN 107010240A
- Authority
- CN
- China
- Prior art keywords
- supporting plate
- landing platform
- unmanned plane
- solar
- solar panel
- 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.)
- Pending
Links
- 238000003466 welding Methods 0.000 claims abstract description 4
- 238000013016 damping Methods 0.000 abstract description 2
- 230000000694 effects Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000006748 scratching Methods 0.000 description 1
- 230000002393 scratching effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Power Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a kind of solar recharging landing platform of unmanned plane, including supporting plate, landing platform, solar panel, battery, described supporting plate is rectangular configuration, described supporting plate lower weld installs four support bases, supporting leg is installed by bearing pin on described support base, described supporting plate top connects landing platform by many springs, the table top of described landing platform is set to the rectangular configuration with supporting plate formed objects, described four lateral edges of supporting plate set solar panel, described solar panel is rotated by hinge and supporting plate and connected, described battery is connected to solar panel, a socket is also associated with described battery, described hinge is fixed on solar panel and supporting plate by welding manner, described supporting leg is telescopic strut, generally, the present invention, which has, to be easy to carry, damping effect is good, also there is function of solar charging simultaneously.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, it is related to a kind of unmanned plane landing platform, particularly a kind of unmanned plane is too
Sun can charge landing platform.
Background technology
UAV referred to as " unmanned plane ", is manipulated not using radio robot and the programme-control provided for oneself
Manned aircraft.Now, unmanned plane is widely used in taking photo by plane and agriculture field, it is often necessary to carries out operation to mountain area or field and appoints
Business, therefore, unmanned plane is accomplished by some rugged hill paths or takeoff and anding in ridge, because landing road surface is concavo-convex
Injustice, unmanned plane often can not normally be taken off, and can also produce certain danger when unmanned plane lands, and cause nothing
The man-machine scratching in landing is damaged.In addition, during operation in the wild unmanned plane apart from charge point farther out, increase the difficulty of charging,
Therefore the charging continuation of the journey of unmanned plane becomes particularly important.
The content of the invention
It is an object of the invention to provide a kind of solar recharging landing platform of unmanned plane, landing platform structure letter
It is single, simple installation is manufactured, is easy to carry, with shock-absorbing function, battery is stored in while can convert solar energy into electrical energy
In for unmanned plane provide cleaning electric energy, improve unmanned plane endurance.
The object of the present invention is achieved like this：A kind of solar recharging landing platform of unmanned plane, including supporting plate, rise
Platform, solar panel, battery drop, and described supporting plate is rectangular configuration, and described supporting plate lower weld installs four
Supporting leg is installed by bearing pin on individual support base, described support base, described supporting plate top connects landing by many springs
Platform, the table top of described landing platform is set to the rectangular configuration with supporting plate formed objects, described four sides of supporting plate
Face edge sets solar panel, and described solar panel is rotated by hinge and supporting plate to be connected, described electric power storage
Pond, which is connected on solar panel, described battery, is also associated with a socket.
Described hinge is fixed on solar panel and supporting plate by welding manner.
Described supporting leg is telescopic strut, and described supporting leg bottom is set to cutting-edge structure.
Air level is set in the middle part of described landing platform upper surface, and described landing platform upper is provided with landing cross
Know.
Described spring is uniformly arranged between supporting plate and landing platform.
The beneficial effect comprise that：Supporting leg of the present invention is all telescopic strut, can extend and shorten, can not only
Adapt to set up under different geographical environments, be also convenient for carrying.Two are, what the present invention was set between supporting plate and landing platform
Multigroup spring, with shock-absorbing function, can effectively reduce the impulsive force to landing platform during unmanned plane landing, make unmanned plane
Landing it is more steady.Three are, the present invention is mounted with solar panel, solar cell in the side of supporting plate by hinge
Plate can be rotated around supporting plate, conveniently can make it just to the sun by regulation solar panel, solar panel can be by the sun
Electric energy can be converted into, and is stored in battery, battery can provide electric energy for unmanned plane, unmanned plane is solved and works in the wild
When be not easy to charging the problem of, effectively improve the endurance of unmanned plane.
Brief description of the drawings
Fig. 1 is positive structure diagram of the invention.
Fig. 2 is overlooking the structure diagram of the invention.
Fig. 3 is present invention looks up structural representation of the invention.
Fig. 4 for the present invention positive structure diagram when not installing solar panel.
Fig. 5 for the present invention right side structure schematic view when not installing solar panel.
Fig. 6 is vertical section structure schematic diagram of the invention.
In figure：1st, supporting plate 2, landing platform 3, solar panel 4, battery 5, support base 6, bearing pin
7th, supporting leg 8, spring 9, hinge 10, socket 11, air level 12, cross mark.
Embodiment
Below in conjunction with the accompanying drawings to embodiments of the invention further instruction.
Embodiment 1
As shown in figures 1-6, the solar recharging landing platform of a kind of unmanned plane, including supporting plate 1, landing platform 2, solar energy
Cell panel 3, battery 4, described supporting plate 1 are rectangular configuration, and the described lower weld of supporting plate 1 installs four support bases 5,
Supporting leg 7 is installed by bearing pin 6 on described support base 5, the described top of supporting plate 1 connects landing platform by many springs 8
2, the table top of described landing platform 2 is set to the rectangular configuration with the formed objects of supporting plate 1, described 1 four sides of supporting plate
Face edge sets solar panel 3, and described solar panel 3 is rotated by hinge 9 and supporting plate 1 to be connected, described
Battery 4 is connected on solar panel 3, described battery 4 and is also associated with a socket 10.
Described hinge 9 is fixed on solar panel 3 and supporting plate 1 by welding manner.
Described supporting leg 7 is telescopic strut, and the described bottom of supporting leg 7 is set to cutting-edge structure.
The described upper surface middle part of landing platform 2 sets air level 11, and the described top of landing platform 2 is provided with landing ten
Word mark 12.
Described spring 8 is uniformly arranged between supporting plate 1 and landing platform 2.
The present invention is when in use：A kind of solar recharging landing platform of unmanned plane, including supporting plate, landing platform, too
Positive energy cell panel, battery, the bottom of supporting plate is provided with four support bases, support base installs supporting leg, supporting leg by bearing pin
It is the pole with Telescopic, and the bottom of supporting leg is set to be convenient for the cutting-edge structure of ground fixation.Supporting plate top
Multigroup spring is set, and landing platform is installed on the top of spring.When landing platform is set up, supporting leg is first turned on, by landing
Platform is fixed on ground, then adjusts supporting leg, makes the bubble in the air level on landing platform placed in the middle, now the platform of landing platform
Face is level.Then, unmanned plane is put at the cross mark of landing platform, taking off for unmanned plane can be manipulated by remote control
And landing.Solar panel is set in four lateral edges of supporting plate, solar panel is rotated by hinge and supporting plate
Link together, battery is connected by electric wire and is also associated with solar panel, battery on a socket, unmanned plane
Charging wire plug insertion socket is chargeable.
Generally, the present invention have be easy to carry, damping effect it is good, while also excellent with function of solar charging
Point.
Claims (5)
1. a kind of solar recharging landing platform of unmanned plane, including supporting plate, landing platform, solar panel, battery,
Described supporting plate is rectangular configuration, and described supporting plate lower weld is installed to be passed through on four support bases, described support base
Bearing pin installs supporting leg, and described supporting plate top connects landing platform by many springs, and the table top of described landing platform is set
It is set to the rectangular configuration with supporting plate formed objects, it is characterised in that：Described four lateral edges of supporting plate set solar energy
Cell panel, described solar panel is rotated by hinge and supporting plate to be connected, and described battery is connected to solar-electricity
A socket is also associated with pond plate, described battery.
2. a kind of solar recharging landing platform of unmanned plane according to claim 1, it is characterised in that：Described hinge
Solar panel and supporting plate are fixed on by welding manner.
3. a kind of solar recharging landing platform of unmanned plane according to claim 1, it is characterised in that：Described supporting leg
For telescopic strut, described supporting leg bottom is set to cutting-edge structure.
4. a kind of solar recharging landing platform of unmanned plane according to claim 1, it is characterised in that：Described landing
Air level is set in the middle part of platform upper surface, and described landing platform upper is provided with landing cross mark.
5. a kind of solar recharging landing platform of unmanned plane according to claim 1, it is characterised in that：Described spring
It is uniformly arranged between supporting plate and landing platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710335082.9A CN107010240A (en) | 2017-05-12 | 2017-05-12 | A kind of solar recharging landing platform of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710335082.9A CN107010240A (en) | 2017-05-12 | 2017-05-12 | A kind of solar recharging landing platform of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107010240A true CN107010240A (en) | 2017-08-04 |
Family
ID=59449228
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710335082.9A Pending CN107010240A (en) | 2017-05-12 | 2017-05-12 | A kind of solar recharging landing platform of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107010240A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033031A (en) * | 2018-01-11 | 2018-05-15 | 辽宁通用航空研究院 | Field unmanned flight's platform with solar charging device |
| CN108263631A (en) * | 2017-12-26 | 2018-07-10 | 中国科学院长春光学精密机械与物理研究所 | A kind of unmanned plane guiding and landing system |
| CN109896033A (en) * | 2017-12-07 | 2019-06-18 | 智飞智能装备科技东台有限公司 | A kind of portable multifunctional unmanned plane landing platform |
| CN110104195A (en) * | 2019-05-14 | 2019-08-09 | 广东电网有限责任公司 | A kind of unmanned plane automatic charging system with solar panel |
| CN111731519A (en) * | 2020-03-04 | 2020-10-02 | 蓝箭航天空间科技股份有限公司 | Landing support mechanism for recovering spacecraft and spacecraft |
| CN113460252A (en) * | 2020-03-30 | 2021-10-01 | 自然资源部第二海洋研究所 | Multifunctional ocean engineering corollary equipment |
| CN113968351A (en) * | 2021-12-03 | 2022-01-25 | 国网湖北省电力有限公司咸宁供电公司 | Charging station for power transmission and distribution line inspection unmanned aerial vehicle |
| CN114426105A (en) * | 2022-03-02 | 2022-05-03 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
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| CN104527991A (en) * | 2014-11-11 | 2015-04-22 | 国网辽宁省电力有限公司检修分公司 | Portable dust preventive lifting platform for UAV (unmanned aerial vehicle) in mountainous region |
| CN205178593U (en) * | 2015-12-09 | 2016-04-20 | 长沙钛合电子设备有限公司 | Unmanned aerial vehicle platform that charges |
| CN106114884A (en) * | 2016-06-28 | 2016-11-16 | 安庆市佰斯特电子科技有限公司 | A kind of unmanned plane based on Stewart parallel institution stops charging station |
| CN106114886A (en) * | 2016-06-28 | 2016-11-16 | 安庆市佰斯特电子科技有限公司 | A kind of novel electric power reconnoitres unmanned plane electric energy ancillary equipment |
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| CN206939104U (en) * | 2017-05-12 | 2018-01-30 | 河南省酷农航空植保科技有限公司 | A kind of solar recharging landing platform of unmanned plane |
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2017
- 2017-05-12 CN CN201710335082.9A patent/CN107010240A/en active Pending
Patent Citations (6)
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| CN104527991A (en) * | 2014-11-11 | 2015-04-22 | 国网辽宁省电力有限公司检修分公司 | Portable dust preventive lifting platform for UAV (unmanned aerial vehicle) in mountainous region |
| CN205178593U (en) * | 2015-12-09 | 2016-04-20 | 长沙钛合电子设备有限公司 | Unmanned aerial vehicle platform that charges |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109896033A (en) * | 2017-12-07 | 2019-06-18 | 智飞智能装备科技东台有限公司 | A kind of portable multifunctional unmanned plane landing platform |
| CN108263631A (en) * | 2017-12-26 | 2018-07-10 | 中国科学院长春光学精密机械与物理研究所 | A kind of unmanned plane guiding and landing system |
| CN108033031A (en) * | 2018-01-11 | 2018-05-15 | 辽宁通用航空研究院 | Field unmanned flight's platform with solar charging device |
| CN108033031B (en) * | 2018-01-11 | 2023-08-15 | 辽宁通用航空研究院 | Outdoor unmanned flying platform with solar charging device |
| CN110104195A (en) * | 2019-05-14 | 2019-08-09 | 广东电网有限责任公司 | A kind of unmanned plane automatic charging system with solar panel |
| CN111731519A (en) * | 2020-03-04 | 2020-10-02 | 蓝箭航天空间科技股份有限公司 | Landing support mechanism for recovering spacecraft and spacecraft |
| CN111731519B (en) * | 2020-03-04 | 2020-11-24 | 蓝箭航天空间科技股份有限公司 | Landing support mechanism for recovering spacecraft and spacecraft |
| CN113460252A (en) * | 2020-03-30 | 2021-10-01 | 自然资源部第二海洋研究所 | Multifunctional ocean engineering corollary equipment |
| CN113968351A (en) * | 2021-12-03 | 2022-01-25 | 国网湖北省电力有限公司咸宁供电公司 | Charging station for power transmission and distribution line inspection unmanned aerial vehicle |
| CN114426105A (en) * | 2022-03-02 | 2022-05-03 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
| CN114426105B (en) * | 2022-03-02 | 2022-10-04 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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Application publication date: 20170804 |