CN201992891U - Composite ceramic solar heat-collecting solid plate - Google Patents
Composite ceramic solar heat-collecting solid plate Download PDFInfo
- Publication number
- CN201992891U CN201992891U CN2010206792980U CN201020679298U CN201992891U CN 201992891 U CN201992891 U CN 201992891U CN 2010206792980 U CN2010206792980 U CN 2010206792980U CN 201020679298 U CN201020679298 U CN 201020679298U CN 201992891 U CN201992891 U CN 201992891U
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- Prior art keywords
- solid
- conventional ceramic
- solid plane
- ceramic
- plane conventional
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- Expired - Fee Related
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S70/00—Details of absorbing elements
- F24S70/30—Auxiliary coatings, e.g. anti-reflective coatings
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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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/20—Solar thermal
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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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/40—Solar thermal energy, e.g. solar towers
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Photovoltaic Devices (AREA)
- Building Environments (AREA)
Abstract
The utility model provides a composite ceramic solar heat-collecting solid plate, which is in a rectangle shape. The rectangle solid plate is formed by a base plate and a heat-absorbing layer, wherein the base plate is an ordinary solid plane ceramic plate. The upper surface of the ordinary solid plane ceramic plate is coated with a sintered vanadium-titanium black porcelain heat-absorbing layer with tiny holes on the rough surface. The composite ceramic solar heat-collecting solid plate is easy to manufacture, and solar thermal collector manufactured by the composite ceramic solar heat-collecting solid plate is low in cost.
Description
Technical field
The utility model relates to solar utilization technique, is that a kind of composite ceramic solar can the thermal-arrest solid slab.
Background technology
At present, heating is used for fields such as domestic water, heating, refrigeration to the water in the hollow sheeting cavity to absorb solar energy with composite ceramic solar energy hollow sheeting, its advantage is better than existing all solar energy heating devices, simultaneously, can absorb solar energy to air heat in the cavity by hollow sheeting with composite ceramic solar, the kinetic energy generating that produces when rising with the heat energy of hot-air and hot-air, or the hot-air in the hollow sheeting cavity is sent into purposes such as indoor more advantage is arranged.But, the present application people finds in repetition test and in constantly studying, can still there be deficiency in this composite ceramic solar by hollow sheeting: for example, when needs when ceramic solar ventiduct is built in desert area, need to build large-sized solar ventiduct, composite ceramic solar energy hollow sheeting is subjected to the restriction of ceramic production technology, the height in duct and width all can not reach requirement, the manufacture craft of making macropore composite ceramic solar energy hollow sheeting is very complicated, is difficult on the technology realize, simultaneously, the thermal capacity of composite ceramic solar energy hollow sheeting is bigger, in solar ventiduct, absorb heat energy, thereby consume the energy in the solar ventiduct, influence the wind-force of solar ventiduct.Above-mentioned deficiency easily makes the cost of manufacture of solar ventiduct higher relatively, and makes implementer's case quite complicated.
The utility model content
The purpose of this utility model is, provides a kind of composite ceramic solar can the thermal-arrest solid slab, and it is easy to make, and is with low cost with the solar thermal collector that it is made.
The utility model to achieve these goals, be achieved through the following technical solutions: a kind of composite ceramic solar energy thermal-arrest solid slab, it is rectangular, this rectangle is made of soleplate and heat-sink shell, soleplate is a solid plane conventional ceramic plate, the upper surface of solid plane conventional ceramic plate cover sintering rough surface, be covered with the vanadium-titanium black ceramic heat-sink shell of small hole.The thickness of solid plane conventional ceramic plate is the 2-8 millimeter, and the thickness of vanadium-titanium black ceramic heat-sink shell is the 0.1-0.5 millimeter.The length direction both sides of solid plane conventional ceramic plate are provided with the dull and stereotyped and second solid plane conventional ceramic side flat board of the first solid plane conventional ceramic side respectively, the upper surface of solid plane conventional ceramic plate, first solid plane conventional ceramic side inner surface dull and stereotyped and the second solid plane conventional ceramic side flat board all cover the vanadium-titanium black ceramic heat-sink shell of sintering, and solid plane conventional ceramic plate, the first solid plane conventional ceramic side flat board and the second solid plane conventional ceramic side flat board are one.Solid plane conventional ceramic plate, first solid plane conventional ceramic side thickness dull and stereotyped and the second solid plane conventional ceramic side flat board are the 3-12 millimeter, and the thickness of the vanadium-titanium black ceramic heat-sink shell on the inner surface of the upper surface of solid plane conventional ceramic plate, the first solid plane conventional ceramic side flat board and the second solid plane conventional ceramic side flat board is the 0.05-0.5 millimeter.The thickness of the solid surface plate of conventional ceramic is 2 millimeters, and the thickness of vanadium-titanium black ceramic heat-sink shell is 0.5 millimeter.Solid plane conventional ceramic plate, the first solid plane conventional ceramic side flat board and the second solid plane conventional ceramic side slab-thickness are 5 millimeters, and the thickness of vanadium-titanium black ceramic heat-sink shell is 0.3 millimeter.
Advantage of the present utility model is: above-mentioned composite ceramic solar energy thermal-arrest solid slab, can overcome all deficiencies of prior art, the difficulty of manufacture craft is significantly reduced, thereby production cost is declined to a great extent, and can make bigger arbitrary dimension as required, minimal thickness can be accomplished 2 millimeters, this thickness is that all ceramic solar energy heat-collection plates are not all accomplished in the prior art, so various solar thermal collectors or solar ventiduct with the making of the utility model composite ceramic solar energy thermal-arrest solid slab, can make cost reach the low-level limit, for large scale collection solar energy provides cost low, long service life, be easy to make the robust techniques guarantee of installation.When making solar ventiduct with the utility model composite ceramic solar energy thermal-arrest solid slab, self power consumption is extremely low, raw material is easy to get, manufacture craft is simplified and advantage such as easy construction because it has, so, the cost of manufacture of solar ventiduct only is about 7% of a prior art, is higher than service life about prior art 30-60%.
Can also can make physical therapy apparatus by the thermal-arrest solid slab with the utility model composite ceramic solar, adopt heating element heater that composite ceramic solar can be heated by the thermal-arrest solid slab, the vanadium-titanium black ceramic heat-sink shell is infrared radiation outwards.
Description of drawings
Accompanying drawing 1 is one of a utility model embodiment structural representation; Accompanying drawing 2 is two structural representations of the utility model embodiment.
The specific embodiment
The contrast accompanying drawing is described further the utility model.
It among the figure composite ceramic solar energy thermal-arrest solid slab, it is a kind of rectangular slab, it can also do rectangularity or square, this rectangle is made of soleplate and heat-sink shell, soleplate is a solid plane conventional ceramic plate 1, the upper surface of solid plane conventional ceramic plate 1 cover sintering rough surface, be covered with the vanadium-titanium black ceramic heat-sink shell 2 of small hole.
The preferred scheme of the utility model is: the thickness of solid plane conventional ceramic plate 1 is the 2-8 millimeter, and the thickness of vanadium-titanium black ceramic heat-sink shell 2 is the 0.1-0.5 millimeter, and this is to reach the technical scheme that the utility model purpose is saved cost, endothermic effect the best most.
One of Scheme Choice of the present utility model is: on the basis of scheme shown in Figure 1, making the thickness of solid plane conventional ceramic plate 1 is 2 millimeters, the thickness of vanadium-titanium black ceramic heat-sink shell 2 is 0.5 millimeter, and this scheme is as the far infrared radiation plate, and its manufacturing cost is lower by about 80% than prior art.
Composite ceramic solar energy thermal-arrest solid slab of the present utility model can also be made structure as shown in Figure 2, the length direction both sides of solid plane conventional ceramic plate 1 are provided with the dull and stereotyped 3 and second solid plane conventional ceramic side flat board 4 of the first solid plane conventional ceramic side respectively, the upper surface of solid plane conventional ceramic plate 1, the inner surface of the dull and stereotyped 3 and second solid plane conventional ceramic side flat board 4 of the first solid plane conventional ceramic side all covers the vanadium-titanium black ceramic heat-sink shell 2 of sintering, solid plane conventional ceramic plate 1, the dull and stereotyped 3 and second solid plane conventional ceramic side dull and stereotyped 4 of the first solid plane conventional ceramic side is an one, this scheme is to reduce the preferred version of manufacturing cost equally, and endothermic effect the best.
The utility model for the scheme that further improves service life, reduce manufacturing cost and provide is: the thickness of the dull and stereotyped 3 and second solid conventional ceramic side flat board 4 of described solid plane conventional ceramic plate 1, the first solid conventional ceramic side is the 3-12 millimeter, and the thickness of the vanadium-titanium black ceramic heat-sink shell 2 on the inner surface of the upper surface of solid plane conventional ceramic plate 1, the dull and stereotyped 3 and second solid plane conventional ceramic side flat board 4 of the first solid plane conventional ceramic side is the 0.05-0.5 millimeter.
Further scheme described in the utility model is: dull and stereotyped 4 thickness of the dull and stereotyped 3 and second solid plane conventional ceramic side of solid plane conventional ceramic plate 1, the first solid plane conventional ceramic side are 5 millimeters, the thickness of vanadium-titanium black ceramic heat-sink shell 2 is 0.3 millimeter, this be easy to make, with low cost and endothermic effect structure preferably.
Claims (6)
1. a composite ceramic solar can the thermal-arrest solid slab, it is characterized in that: it is rectangular, this rectangle is made of soleplate and heat-sink shell, soleplate is a solid plane conventional ceramic plate (1), the upper surface of solid plane conventional ceramic plate (1) cover sintering rough surface, be covered with the vanadium-titanium black ceramic heat-sink shell (2) of small hole.
2. a kind of composite ceramic solar energy thermal-arrest solid slab according to claim 1, it is characterized in that: the thickness of solid plane conventional ceramic plate (1) is the 2-8 millimeter, the thickness of vanadium-titanium black ceramic heat-sink shell (2) is the 0.1-0.5 millimeter.
3. a kind of composite ceramic solar energy thermal-arrest solid slab according to claim 1, it is characterized in that: the length direction both sides of solid plane conventional ceramic plate (1) are provided with the first solid plane conventional ceramic side flat board (3) and the second solid plane conventional ceramic side flat board (4) respectively, the upper surface of solid plane conventional ceramic plate (1), the inner surface of the first solid plane conventional ceramic side flat board (3) and the second solid plane conventional ceramic side flat board (4) all covers the vanadium-titanium black ceramic heat-sink shell (2) of sintering, solid plane conventional ceramic plate (1), the first solid plane conventional ceramic side flat board (3) and the second solid plane conventional ceramic side flat board (4) are one.
4. a kind of composite ceramic solar energy thermal-arrest solid slab according to claim 3, it is characterized in that: the thickness of solid plane conventional ceramic plate (1), the first solid plane conventional ceramic side flat board (3) and the second solid plane conventional ceramic side flat board (4) is the 3-12 millimeter, and the thickness of the vanadium-titanium black ceramic heat-sink shell (2) on the inner surface of the upper surface of solid plane conventional ceramic plate (1), the first solid plane conventional ceramic side flat board (3) and the second solid plane conventional ceramic side flat board (4) is the 0.05-0.5 millimeter.
5. a kind of composite ceramic solar energy thermal-arrest solid slab according to claim 1, it is characterized in that: the thickness of the solid surface plate of conventional ceramic (1) is 2 millimeters, the thickness of vanadium-titanium black ceramic heat-sink shell (2) is 0.5 millimeter.
6. a kind of composite ceramic solar energy thermal-arrest solid slab according to claim 3, it is characterized in that: solid plane conventional ceramic plate (1), the first solid plane conventional ceramic side flat board (3) and second solid plane conventional ceramic side flat board (4) thickness are 5 millimeters, and the thickness of vanadium-titanium black ceramic heat-sink shell (2) is 0.3 millimeter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010206792980U CN201992891U (en) | 2010-01-04 | 2010-12-24 | Composite ceramic solar heat-collecting solid plate |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010011306.9 | 2010-01-04 | ||
| CN201010011306 | 2010-01-04 | ||
| CN2010206792980U CN201992891U (en) | 2010-01-04 | 2010-12-24 | Composite ceramic solar heat-collecting solid plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201992891U true CN201992891U (en) | 2011-09-28 |
Family
ID=43997876
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010206792980U Expired - Fee Related CN201992891U (en) | 2010-01-04 | 2010-12-24 | Composite ceramic solar heat-collecting solid plate |
| CN2010106047573A Expired - Fee Related CN102062486B (en) | 2010-01-04 | 2010-12-24 | Composite ceramic solar heat-collection plate and solar groove-shaped air channel |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010106047573A Expired - Fee Related CN102062486B (en) | 2010-01-04 | 2010-12-24 | Composite ceramic solar heat-collection plate and solar groove-shaped air channel |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN201992891U (en) |
| WO (1) | WO2011079527A1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011160436A1 (en) * | 2010-06-23 | 2011-12-29 | Huang Jinxi | Solar heat collecting plate of composite black ceramic material and method for manufacturing the same |
| CN104309224B (en) * | 2014-10-13 | 2015-10-07 | 山东理工大学 | A kind of preparation method of nickel slag ceramic heat collecting plate |
| CN114324741B (en) * | 2020-09-30 | 2024-02-13 | 宝山钢铁股份有限公司 | Evaluation die and evaluation method for characteristic forming limit of roll-punched forming rib groove |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4266531A (en) * | 1978-11-13 | 1981-05-12 | Solar Southwest | Rooftop solar energy collector panel |
| CN87205485U (en) * | 1987-11-18 | 1988-09-21 | 王安 | Movable solar energy heat-collecting plate |
| ZA983208B (en) * | 1997-05-03 | 1998-10-22 | D D C Planungs Enwicklungs Und | Structural element for cladding roof or wall surfaces of a building and process for producing a structural element |
| CN101261051B (en) * | 2007-03-08 | 2010-10-06 | 曹树梁 | Black ceramic composite ceramic sun plate |
| CN100510570C (en) * | 2006-05-25 | 2009-07-08 | 山东天虹弧板有限公司 | Method for preparing composite hollow ceramic solar energy heat collection plate |
| CN101270725B (en) * | 2007-03-22 | 2010-06-23 | 曹树梁 | Ceramic solar ventiduct |
| CN101648815A (en) * | 2007-03-08 | 2010-02-17 | 曹树梁 | Vertical netty composite ceramic solar plate of black ceramic |
| CN101514106B (en) * | 2008-02-20 | 2012-08-22 | 曹树梁 | Trough-type ceramic solar plate |
| CN101592404B (en) * | 2008-05-26 | 2010-11-24 | 曹树梁 | Ceramic solar board with air heat insulating layer |
-
2010
- 2010-12-24 CN CN2010206792980U patent/CN201992891U/en not_active Expired - Fee Related
- 2010-12-24 CN CN2010106047573A patent/CN102062486B/en not_active Expired - Fee Related
- 2010-12-31 WO PCT/CN2010/002247 patent/WO2011079527A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO2011079527A1 (en) | 2011-07-07 |
| CN102062486A (en) | 2011-05-18 |
| CN102062486B (en) | 2012-12-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110928 Termination date: 20131224 |