CN109056562A - A kind of new type solar energy aviation deck - Google Patents
A kind of new type solar energy aviation deck Download PDFInfo
- Publication number
- CN109056562A CN109056562A CN201810637410.5A CN201810637410A CN109056562A CN 109056562 A CN109056562 A CN 109056562A CN 201810637410 A CN201810637410 A CN 201810637410A CN 109056562 A CN109056562 A CN 109056562A
- Authority
- CN
- China
- Prior art keywords
- solar panels
- aluminum alloy
- bottom plate
- against pressure
- alloy bottom
- 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
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 38
- 239000004744 fabric Substances 0.000 claims abstract description 4
- 230000000694 effects Effects 0.000 abstract description 3
- 230000007613 environmental effect Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 4
- 238000005286 illumination Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01C—CONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
- E01C11/00—Details of pavings
- E01C11/24—Methods or arrangements for preventing slipperiness or protecting against influences of the weather
-
- 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
- H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
- H02S40/30—Electrical components
- H02S40/34—Electrical components comprising specially adapted electrical connection means to be structurally associated with the PV module, e.g. junction boxes
-
- 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)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Power Engineering (AREA)
- Road Signs Or Road Markings (AREA)
Abstract
The present invention provides a kind of new type solar energy aviation decks, including solar panels, tread plate against pressure, aluminum alloy bottom plate, current-collecting terminals, conducting wire, battery, aluminum alloy bottom plate surface is equipped with groove corresponding with the tread plate against pressure and solar panels, tread plate against pressure is embedded in the groove of aluminum alloy bottom plate, tread plate against pressure has multiple and interlaced at fenestral fabric, solar panels have muti-piece, solar panels are set in grid, solar panels are fixedly connected in the groove of aluminum alloy bottom plate, opening corresponding with current-collecting terminals is offered in the middle part of aluminum alloy bottom plate, current-collecting terminals are fixedly connected on solar panels through opening, current-collecting terminals are connect with battery by conducting wire.The more energy efficient environmental protection of solar energy resources can be maximally utilised using solar panels, tread plate against pressure, aluminum alloy bottom plate, tread plate against pressure can play better antiskid effect and ensure safety.
Description
Technical field
The present invention is applied to helideck field, especially a kind of new type solar energy aviation deck.
Background technique
The structure of helideck mainly has mixed mud structure, steel construction, aluminium alloy structure, is mainly used to fire-fighting emergent rescue
And business flying, because helideck builds the building less illumination daylighting region blocked around code requirement well so can benefit
Illumination resource is more, and the deck used on helideck at present does not have the ability using illumination resource, must so having
A kind of aviation deck that can utilize solar energy resources is provided, the optimization energy is more energy-saving and environmentally friendly using structure.
Summary of the invention
A kind of new type solar energy aviation deck, including solar panels, tread plate against pressure, aluminum alloy bottom plate, current-collecting terminals, lead
Line, battery, the aluminum alloy bottom plate surface are equipped with groove corresponding with the tread plate against pressure and the solar panels, institute
It states tread plate against pressure to be embedded in the groove of the aluminum alloy bottom plate, the tread plate against pressure has multiple and interlaced at grid
Shape structure, the solar panels have muti-piece, and the solar panels are set in the grid, and the solar panels are fixedly connected on
In the groove of the aluminum alloy bottom plate, opening corresponding with the current-collecting terminals, institute are offered in the middle part of the aluminum alloy bottom plate
It states current-collecting terminals to be fixedly connected on the solar panels through the opening, the current-collecting terminals and the battery pass through institute
State conducting wire connection.
The solar panels are that small-size flaky structure is embedded on aluminum alloy bottom plate, are passed through between each small-size flaky structure
Conducting wire is connected in series, and the solar panels on all aluminum alloy bottom plates connect last output end with current-collecting terminals by welding on plate
It connects.
The tread plate against pressure is that fenestral fabric is embedded on aluminum alloy bottom plate, and the grid interval of tread plate against pressure is hollow
Partial position is that the level height of the installation site of solar panels and tread plate against pressure is higher than the level height of solar panels,
It prevents when takeoff and landing or when apron operations personnel's operation damages solar panels by pressure, while tread plate against pressure can also prevent the rainy day
Apron operations personnel, which occur to break away in apron operations, causes safety accident.
The aluminum alloy bottom plate and solar panels, tread plate against pressure are inner embedded integrated structure, that is, solar panels, against pressure
Tread plate is embedded on aluminum alloy bottom plate, aluminum alloy bottom plate be also pin-connected panel deck by one piece one piece be spliced to form one it is straight
Rise the platform of machine landing.
The beneficial effects of the present invention are: being capable of land productivity to greatest extent using solar panels, tread plate against pressure, aluminum alloy bottom plate
With the more energy efficient environmental protection of solar energy resources, tread plate against pressure can play better antiskid effect and ensure safety.
Detailed description of the invention
Fig. 1 is a kind of new type solar energy aviation deck level structural schematic diagram of the present invention；
Fig. 2 is a kind of new type solar energy aviation of the invention deck three-dimensional structure diagram.
Figure label: 1, solar panels；2, tread plate against pressure；3, aluminum alloy bottom plate；4, current-collecting terminals；5, conducting wire；6, it stores
Battery.
Specific embodiment
As shown in Figs. 1-2, Fig. 1 is a kind of new type solar energy aviation deck level structural schematic diagram of the present invention, a kind of novel
Solar energy aviation deck, including solar panels 1, tread plate against pressure 2, aluminum alloy bottom plate 3, current-collecting terminals 4, conducting wire 5 and battery
6。
Wherein, solar panels 1 are that small-size flaky structure is embedded on aluminum alloy bottom plate 3, between each small-size flaky structure
It is connected in series by conducting wire 5, the solar panels 1 on all aluminum alloy bottom plates 3 connect last output end and pass through with current-collecting terminals 4
It is welded on plate, tread plate 2 against pressure is that fenestral fabric is embedded on aluminum alloy bottom plate 3, and the grid interval of tread plate 2 against pressure is hollow
Partial position is the level height of the installation site of solar panels 1 and tread plate against pressure 2 than the level height of solar panels 1
Height, prevents when takeoff and landing or when apron operations personnel's operation damages solar panels 1 by pressure, while tread plate against pressure 2 can also be prevented
Only rainy day apron operations personnel, which occur to break away in apron operations, causes safety accident aluminum alloy bottom plate 3 and solar panels 1, against pressure
Tread plate 2 is inner embedded integrated structure, that is, solar panels 1, tread plate against pressure 2 is embedded on aluminum alloy bottom plate 3, aluminium alloy bottom
Plate 3 is also the platform for being spliced to form a helicopter landing that pin-connected panel deck passes through one piece one piece.
Further, structure catenation principle of the invention is illustrated below in conjunction with Fig. 2, as shown in Fig. 2, Fig. 2 is this hair
A kind of bright new type solar energy aviation deck three-dimensional structure diagram, wherein the top is that tread plate 2 against pressure is molten with latticed structure
It connects in aluminum alloy bottom plate 3, vacant position is for installing sheet solar panels 1, the sun among latticed tread plate 2 against pressure
Energy plate 1 on the solar panels 1 in groove fixation and the interlocking of aluminum alloy bottom plate 3 and 3 center of aluminum alloy bottom plate by being welded with
Current-collecting terminals 4 and the battery 6 on the accumulator stand that aluminum alloy bottom plate 3 is equipped with by conducting wire 5 and aluminum alloy bottom plate lower part
Connection.
The beneficial effects of the present invention are: can be to greatest extent using solar panels 1, tread plate against pressure 2, aluminum alloy bottom plate 3
Ground utilizes the more energy efficient environmental protection of solar energy resources, and tread plate 2 against pressure can play better antiskid effect and ensure safety.
These are only the preferred embodiment of the present invention, is not intended to restrict the invention, for those skilled in the art
For member, the invention may be variously modified and varied.All within the spirits and principles of the present invention, it is made it is any modification,
Equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (4)
1. a kind of new type solar energy aviation deck, it is characterised in that: including solar panels, tread plate against pressure, aluminum alloy bottom plate, collection
Electric terminal, conducting wire, battery, the aluminum alloy bottom plate surface are equipped with corresponding with the tread plate against pressure and the solar panels
Groove, the tread plate against pressure is embedded in the groove of the aluminum alloy bottom plate, and the tread plate against pressure has multiple and mutual
It is staggered into fenestral fabric, the solar panels have muti-piece, and the solar panels are set in the grid, the solar panels
It is fixedly connected in the groove of the aluminum alloy bottom plate, is offered in the middle part of the aluminum alloy bottom plate corresponding with the current-collecting terminals
Opening, the current-collecting terminals are fixedly connected on the solar panels through the opening, the current-collecting terminals and the storage
Battery is connected by the conducting wire.
2. a kind of new type solar energy aviation deck according to claim 1, which is characterized in that the multiple solar panels it
Between be connected in series by the conducting wire.
3. a kind of new type solar energy aviation deck according to claim 1, which is characterized in that the height of the tread plate against pressure
Degree is greater than the height of the solar panels.
4. a kind of new type solar energy aviation deck according to claim 1, which is characterized in that the solar panels are small-sized
Laminated structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810637410.5A CN109056562A (en) | 2018-06-20 | 2018-06-20 | A kind of new type solar energy aviation deck |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810637410.5A CN109056562A (en) | 2018-06-20 | 2018-06-20 | A kind of new type solar energy aviation deck |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109056562A true CN109056562A (en) | 2018-12-21 |
Family
ID=64821090
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810637410.5A Pending CN109056562A (en) | 2018-06-20 | 2018-06-20 | A kind of new type solar energy aviation deck |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109056562A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200981966Y (en) * | 2006-12-19 | 2007-11-28 | 台瑞机场设备技术(上海)有限公司 | Deck for jointing and combining type parking apron |
| CN201990911U (en) * | 2011-03-24 | 2011-09-28 | 任俊花 | Deck for parking apron of roof overhead helicopter |
| KR20130034083A (en) * | 2011-09-28 | 2013-04-05 | 삼성중공업 주식회사 | Helideck having solar cell |
| CN203218293U (en) * | 2013-04-23 | 2013-09-25 | 中雅智能科技江苏有限公司 | Reinforced photovoltaic assembly framework |
| RU2533857C1 (en) * | 2013-07-03 | 2014-11-20 | Артем Владимирович Пигин | Air transport system |
| CN104917275A (en) * | 2015-06-10 | 2015-09-16 | 成都赋阳技术开发有限公司 | Vessel supplied with power by utilizing solar energy and wind energy |
| CN205123658U (en) * | 2015-10-29 | 2016-03-30 | 宁波东盛集成电路元件有限公司 | Solar panel |
-
2018
- 2018-06-20 CN CN201810637410.5A patent/CN109056562A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200981966Y (en) * | 2006-12-19 | 2007-11-28 | 台瑞机场设备技术(上海)有限公司 | Deck for jointing and combining type parking apron |
| CN201990911U (en) * | 2011-03-24 | 2011-09-28 | 任俊花 | Deck for parking apron of roof overhead helicopter |
| KR20130034083A (en) * | 2011-09-28 | 2013-04-05 | 삼성중공업 주식회사 | Helideck having solar cell |
| CN203218293U (en) * | 2013-04-23 | 2013-09-25 | 中雅智能科技江苏有限公司 | Reinforced photovoltaic assembly framework |
| RU2533857C1 (en) * | 2013-07-03 | 2014-11-20 | Артем Владимирович Пигин | Air transport system |
| CN104917275A (en) * | 2015-06-10 | 2015-09-16 | 成都赋阳技术开发有限公司 | Vessel supplied with power by utilizing solar energy and wind energy |
| CN205123658U (en) * | 2015-10-29 | 2016-03-30 | 宁波东盛集成电路元件有限公司 | Solar panel |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20181221 |