Patent Application
20100209755
The present invention relates to a solar battery panel having a solar battery module that generates electricity from sunlight, and more particularly to a solar battery unit that can improve energy conversion efficiency.
The electric power generated by a solar battery module increases according to the amount of solar radiation. However, when the temperature of the solar battery module increases, the energy conversion efficiency decreases in proportion to the temperature increase. For this reason, a problem with the solar battery module has been that the solar battery module cannot obtain the maximum electric power in summer, the season in which the amount of solar radiation is greatest, because of the temperature increase of the solar battery module. In view of this problem, the following solar battery units have been proposed.
(1) A solar battery unit has a solar battery module in which a plurality of solar battery cells are laid over a glass substrate and integrated with one another, a flame-like holder for retaining the solar battery module, and a plurality of cooling fins made of aluminum and affixed to the back surface of the solar battery module. The holder has a plurality of vents so that air can flow to the cooling fins (see the following Patent Document 1).
(2) A solar battery unit has a solar battery module and a holder for retaining the solar battery module made of an aluminum alloy, and the holder has a plurality of coolant passages for the coolant that cools the solar battery module (see the following Patent Document 2).
[Patent Document 1] Japanese Published Unexamined Patent Application No. H09-83003
[Patent Document 2] Japanese Published Unexamined Patent Application No. 2000-114574
It may appear that the cooling fins as shown in the foregoing (1) and the holder provided with the coolant passages as shown in the foregoing (2) can release heat of the solar battery module sufficiently because they are made of aluminum or an aluminum alloy, which has high thermal conductivity. However, in reality, the heat of the solar battery module cannot be released sufficiently with the inventions described in the foregoing (1) and (2). The reason is as follows. In the surface of the holder and the cooling fin (heat dissipating member) made of aluminum and the like, there exist very small surface irregularities, and microscopically, the solar battery module and the heat dissipating member are not in close contact with each other. This means that an air layer 55, which has low thermal conductivity, [thermal conductivity of air: 0.0241 W/(m·K)] exists between a solar battery module 52 and a heat dissipating member 54, as shown in
In view of the foregoing circumstances, it is an object of the present invention to provide a solar battery unit that can release the heat of the solar battery module sufficiently and suppress the temperature increase of the solar battery module by inhibiting the presence of an air layer with a low thermal conductivity in a heat transfer passage, whereby the energy conversion efficiency can be improved remarkably.
In order to accomplish the foregoing object, the present invention provides a solar battery unit comprising: a solar battery module; and a heat dissipating means, provided on a back surface of the solar battery module, for releasing heat from the solar battery module, the solar battery unit being characterized in that a heat transfer sheet comprising expanded graphite is interposed between the solar battery module and the heat dissipating means, and the heat transfer sheet is attached in a compressed state to the solar battery module and the heat dissipating means.
When the heat transfer sheet is interposed between the solar battery module and the heat dissipating means as in the above-described configuration, the heat from the solar battery module can be transferred to the heat dissipating means through the heat transfer sheet. In this case, the heat transfer sheet comprising expanded graphite is capable of deforming because it is in a compressed state. As a result, the adhesion between the heat transfer sheet and the solar battery module and between the heat transfer sheet and the heat dissipating means improves, preventing the presence of an air layer, which has low thermal conductivity, between the solar battery module and the heat dissipating means. Thus, the heat of the solar battery module can be transmitted sufficiently to the heat dissipating means, so the temperature increase of the solar battery module is suppressed. As a result, the energy conversion efficiency of the solar battery unit can be improved remarkably.
It is desirable that the heat dissipating means be in a plate shape, and the heat transfer sheet be sandwiched between the heat dissipating means and the back surface of the solar battery module.
With the above-described configuration, the adhesion of the heat transfer sheet with the solar battery module and the heat dissipating means increases because of the self weight of the solar battery module. Accordingly, the above-described advantageous effects can be obtained with a simple method.
It is desirable that a cooling fin be formed on a surface of the heat dissipating means that is opposite a surface thereof being in contact with the heat transfer sheet.
The just-described configuration can further improve the cooling efficiency of the solar battery unit because of the presence of the cooling fin formed on the heat dissipating means.
It is desirable that a coolant passage for passing coolant be provided in the heat dissipating means.
The just-described configuration makes it possible to further improve the cooling efficiency of the solar battery unit because of the presence of the coolant flowing through the coolant passage.
The invention also provides a solar battery unit comprising: a solar battery module; and a heat dissipating means, provided on a back surface of the solar battery module, for releasing heat from the solar battery module, the solar battery unit being characterized in that the heat dissipating means comprises a heat transfer sheet comprising expanded graphite, and the heat transfer sheet is attached in a compressed state to the solar battery module.
It is not essential to provide a heat dissipating means separately as described above, but it is also possible to employ a configuration in which the heat transfer sheet comprising expanded graphite also serves as the heat dissipating means. The reason is that the heat transfer sheet has a small heat capacity so that it can dissipate heat by radiation. With such a configuration, the weight of the solar battery unit itself can be reduced because the heat transfer sheet comprising expanded graphite is much lighter in weight than a heat dissipating means made of, for example, aluminum. As a result, workability in shipping and installing of the solar battery unit is improved, and moreover, the cost of the solar battery unit can be reduced because the parts count of the solar battery unit reduces.
It should be noted that an air layer exists between the heat transfer sheet and the solar battery module unless the heat transfer sheet is attached in a compressed state to the solar battery module. For this reason, it is necessary that the heat transfer sheet be attached in a compressed state to the solar battery module or affixed by an adhesive agent, a tackiness agent, or the like.
It is desirable that the pressure to the heat transfer sheet be from 0.5 MPa to 10.0 MPa.
The reason is as follows. If the pressure to the heat transfer sheet is less than 0.5 MPa, the deformation of the heat transfer sheet is insufficient, so the adhesion of the heat transfer sheet with the solar battery module or with the heat transfer sheet becomes insufficient. Consequently, the presence of an air layer with a low thermal conductivity may not be prevented between the solar battery module and the heat dissipating means. As a consequence, the energy conversion efficiency of the solar battery unit may not be improved sufficiently. On the other hand, if the pressure exceeds 10.0 MPa, the solar battery module may be damaged.
It is desirable that the heat transfer sheet have a bulk density of 1.0 Mg/m3 or lower.
The reason is as follows. If the bulk density of the heat transfer sheet exceeds 1.0 Mg/m3, the flexibility of the heat transfer sheet lowers, although the thermal conductivity and strength of the heat transfer sheet increase. As a consequence, the adhesion of the heat transfer sheet with the solar battery module or with the heat dissipating means may become poor, and the cooling efficiency of the solar battery module may decrease.
The invention also provides a solar battery unit comprising: a solar battery module; and a heat dissipating means, provided on a back surface of the solar battery module, for releasing heat from the solar battery module, the solar battery unit being characterized in that the heat dissipating means comprises a heat transfer sheet comprising expanded graphite, and the heat transfer sheet is affixed to the solar battery module.
With such a configuration, heat dissipation by the heat transfer sheet is made possible by merely affixing the heat transfer sheet to the solar battery module, and moreover, the weight of the solar battery unit itself can be reduced. An adhesive agent or a tackiness agent may be used when affixing the heat transfer sheet and the solar battery module to each other. However, if the viscosity of the agent is too high, the surface irregularities of the solar battery module cannot be filled, and an air layer may form between the solar battery module and the heat transfer sheet. For this reason, it is desirable that the viscosity of the adhesive agent or the tackiness agent be 1000 Pa·s or less. If the thermal conductivity of the adhesive agent or the tackiness agent is too low, the heat dissipation capability may be insufficient. For this reason, it is desirable that the thermal conductivity of the adhesive agent or the tackiness agent be 0.5 W/(m·K) or higher.
It is desirable that the just-described heat transfer sheet have a bulk density of from 1.0 Mg/m3 to 2.0 Mg/m3.
The reason is as follows. If the bulk density of the heat transfer sheet is less than 1.0 Mg/m3, the thermal conductivity of the heat transfer sheet is so low that the cooling efficiency of the solar battery module may be too low, or the strength of the heat transfer sheet is so poor that the workability in fitting the heat transfer sheet may be too poor. On the other hand, if the bulk density of the heat transfer sheet exceeds 2.0 Mg/m3, the flexibility of the heat transfer sheet may become poor.
It is desirable that the heat transfer sheet have a thickness of from 0.1 mm to 3.0 mm.
The reason is as follows. If the thickness of the heat transfer sheet exceeds 3.0 mm, the heat transfer capability of the heat transfer sheet will be low, although the strength of the heat transfer sheet will be high. As a consequence, the cooling efficiency of the solar battery module may become poor. On the other hand, if the thickness of the heat transfer sheet is less than 0.1 mm, the strength of the heat transfer sheet may become poor, although the heat transfer capability of the heat transfer sheet will be high. As a consequence, the workability in fitting the heat transfer sheet may become poor.
As discussed above, the present invention exhibits a significant advantage of improving the energy conversion efficiency of a solar battery unit remarkably because the heat of the solar battery module can be released sufficiently and the temperature increase of the solar battery module can be suppressed by inhibiting the presence of an air layer with a low thermal conductivity in a heat transfer passage.
Next, embodiments of the present invention will be described with reference to the drawings.
A heat transfer sheet of the present invention is used for cooling a solar battery module, which is a heat generating body, and it is characterized in that the thermal resistance is reduced and the heat transfer capability is improved by generally employing one of the following configurations.
(1) The heat transfer sheet is disposed in a compressed state between the solar battery module and a heat dissipating member (heat dissipating means) such as a heat sink.
(2) The heat transfer sheet that serves as a heat dissipating member is affixed to the back surface of the solar battery module.
(3) The heat transfer sheet that serves as a heat dissipating member is disposed on the back surface of the solar battery module in a compressed state.
The thermal resistance is the value obtained by dividing the temperature difference between two distant points in a member that is supplied with heat from a heat generating body by the amount of the heat generated by the heat generating body. With reference to
Here, the details of the configuration of each of the solar battery units shown in the foregoing (1) to (3) will be described.
The heat transfer sheet used for the solar battery unit of this configuration is made of expanded graphite formed into a sheet shape, the expanded graphite formed by immersing natural graphite, kish graphite, or the like in a liquid such as sulfuric acid and nitric acid and thereafter heat-treated at 400° C. or higher. The thickness of The heat transfer sheet is formed so as to have a thickness of from 0.1 mm to 3.0 mm and a bulk density of 0.3 Mg/m3 to 1.0 Mg/m3.
The expanded graphite is in a caterpillar-like form or in a fibrous form, in other words, one in which its axial length is longer than its radial length. For example, the axial length may be about 1 mm and the radial length may be about 300 μm. Filaments of the expanded graphite fiber as described above are entangled with one another inside the heat transfer sheet of the present invention.
The heat transfer sheet of the present invention may be formed of expanded graphite alone as described above, but it is possible that a binder such as a phenolic resin or a rubber component may be contained therein in a small amount (for example, about 5%). Moreover, the method of forming the heat transfer sheet of the present invention from expanded graphite as described above is not particularly limited.
Here, the purpose of the present invention is accomplished by interposing the heat transfer sheet between the solar battery module and the heat dissipating member such as a heat sink. However, it is believed that the purpose of the present invention is more accomplished by restricting the bulk density of the heat transfer sheet. Accordingly, discussion is now made from the viewpoint of the bulk density of the heat transfer sheet.
An expanded graphite sheet formed of expanded graphite shows higher thermal conductivity in a plane direction but lower flexibility when its bulk density increases. For this reason, the bulk density of the expanded graphite sheet is adjusted according to its uses. Usually, the one used as a heat transfer sheet is constructed to have a high bulk density (for example, 1.3 Mg/m3 or higher) because the heat conduction capability is viewed as important. On the other hand, the one used as a wall heat insulating material or an electro-magnetic wave shielding material is constructed to have a low bulk density (for example, 1.0 Mg/m3 or lower).
Considering the case that an expanded graphite sheet is used for the heat transfer sheet of the present invention, it is desirable that the expanded graphite sheet be constructed while viewing the flexibility as important and also taking the heat conduction capability into consideration. The reason is as follows. If the heat transfer sheet lacks heat conduction capability, the heat transfer sheet cannot exhibit its intrinsic function sufficiently, so the heat of the solar battery module cannot be transmitted to the heat dissipating member sufficiently. On the other hand, if the heat transfer sheet lacks flexibility, it cannot prevent the presence of the air layer with low thermal conductivity in the heat transfer passage, so likewise the heat of the solar battery module cannot be transmitted to the heat dissipating member sufficiently.
It should be noted that the flexibility is viewed more important than the heat conduction capability for the following reason. If the bulk density of the expanded graphite sheet is not very low (i.e., not less than 0.3 Mg/m3), the thermal conductivity across the thickness becomes 5 W/(m·K) or higher, so the purpose of the present invention can be met sufficiently. On the other hand, so if an air layer is present in the heat transfer passage, heat transmission will be hindered considerably since the thermal conductivity of the air is extremely low [0.0241 W/(m·K)], so the purpose of the present invention cannot be met.
Taking the above discussion into consideration, sufficient flexibility of the heat transfer sheet is ensured and thereby the ability to even out surface irregularities is imparted to the heat transfer sheet by restricting the bulk density of the heat transfer sheet to be 1.0 Mg/m3 or lower (desirably 0.9 Mg/m3 or lower, and particularly desirably 0.8 Mg/m3 or lower), so that it is possible to prevent an air layer from existing in the heat transfer passage.
Nevertheless, if the bulk density of the heat transfer sheet is less than 0.3 Mg/m3, the thermal conductivity of the heat transfer sheet in a plane direction will be so low that the cooling efficiency of the solar battery module may become too low, or the strength of the heat transfer sheet will be so poor that the workability in fitting the heat transfer sheet may become too poor, although the heat transfer sheet shows high flexibility.
For this reason, it is desirable that the bulk density of the heat transfer sheet be 0.3 Mg/m3 or higher.
Next, discussion is made from the viewpoint of the pressure to the heat transfer sheet. It is desirable that the pressure to the heat transfer sheet be from 0.3 MPa to 10.0 MPa.
The reason is as follows. If the pressure to the heat transfer sheet is less than 0.3 MPa, the deformation of the heat transfer sheet is insufficient, so the adhesion between the heat transfer sheet and the solar battery module or between the heat transfer sheet and the heat dissipating member cannot be improved sufficiently, and the presence of an air layer with a low thermal conductivity cannot be prevented in the heat transfer passage. As a consequence, the energy conversion efficiency of the solar battery unit may not be improved sufficiently. On the other hand, if the pressure exceeds 10.0 MPa, the solar battery module may be damaged.
Further, discussion is now made from the viewpoint of the thickness of the heat transfer sheet. It is desirable that the heat transfer sheet have a thickness of from 0.1 mm to 3.0 mm.
The reason is as follows. If the thickness of the heat transfer sheet exceeds 3.0 mm, the heat transfer capability of the heat transfer sheet will be low, although the strength of the heat transfer sheet will be high. As a consequence, the cooling efficiency of the solar battery module may become poor. On the other hand, if the thickness of the heat transfer sheet is less than 0.1 mm, the strength of the heat transfer sheet may become poor, although the heat transfer capability of the heat transfer sheet will be high. As a consequence, the workability in fitting the heat transfer sheet may become poor.
Next, the configuration of the solar battery unit shown in (1) will be described below with reference to
As illustrated in
When the above-described condition is reached, an air layer is prevented from forming between the solar battery module 2 and the heat transfer sheet 3 and between the heat transfer sheet 3 and the heat dissipating member 4, as illustrated in
In the above-described configuration, the heat transfer sheet 3 is merely sandwiched between the solar battery module 2 and the heat dissipating member 4, so the heat transfer sheet 3 can be easily replaced when it becomes necessary to replace the heat transfer sheet 3.
In addition, because the heat transfer sheet 3 prepared in the above-described manner has a thermal conductivity in a plane direction of about 50 to 200 W/(m·K), which is significantly higher than the thermal conductivity across the thickness, the temperature distribution of the heat transfer sheet 3 in a plane direction can be kept substantially uniform. As a result, it becomes possible to prevent heat spots from forming in the heat transfer sheet 3 and the solar battery module 2 as well as the heat dissipating member 4.
Moreover, the heat transfer sheet 3 and the heat dissipating member 4 do not need to be separate as long as the heat transfer sheet 3 can be disposed in such a state as to be sandwiched between the solar battery module 2 and the heat dissipating member 4. For example, the heat transfer sheet 3 may be affixed to the heat dissipating member 4 by an adhesive agent or the like.
The heat dissipating member 4 used in the solar battery unit described in the foregoing (1) is not essential, and it is possible to employ the configuration in which, as illustrated in
Here, it is desirable that the adhesive agent or the tackiness agent have a viscosity of 1000 Pa·s or less. The reason is that if the viscosity of the adhesive agent exceeds 1000 Pa·s, the surface irregularities of the solar battery module 2 cannot be filled with an adhesive agent or a tackiness agent and an air layer may form between the solar battery module 2 and the heat transfer sheet 3. In addition, in order to inhibit the heat transfer capability of the adhesive agent layer or the tackiness agent layer from deteriorating, it is desirable that the thermal conductivity thereof be 0.5 W/(m·K) or higher. Examples of such an adhesive agent or tackiness agent include a silicone grease and an epoxy resin.
In addition, it is desirable that the heat transfer sheet 3 have a bulk density of from 1.0 Mg/m3 to 2.0 Mg/m3. The reason is as follows. If the bulk density of the heat transfer sheet 3 is less than 1.0 Mg/m3, the thermal conductivity of the heat transfer sheet 3 will be so low that the cooling efficiency of the solar battery module 2 may be too low, or the strength of the heat transfer sheet 3 will be so poor that the workability in fitting the heat transfer sheet may be too poor. On the other hand, if the bulk density of the heat transfer sheet exceeds 2.0 Mg/m3, the flexibility of the heat transfer sheet may become poor.
Further, from the viewpoint of the thickness of the heat transfer sheet 3, it is desirable that the heat transfer sheet 3 have a thickness of from 0.1 mm to 3.0 mm. The reason is the same as described in the section that has described the configuration of the solar battery unit shown in the foregoing (1).
It should be noted that both ends of the heat transfer sheet 3 do not necessarily have such a configuration as to be affixed to the frame 5, but they need not be affixed to the frame 5. For example, it is also possible to employ a configuration in which the heat transfer sheet 3 has the same width and length as those of the solar battery module 2 and the heat transfer sheet 3 may exist only on the back surface of the solar battery module 2. That said, with such a configuration, heat cannot be released from the frame 5, so it is preferable to employ the configuration in which both ends of the heat transfer sheet 3 are affixed to the frame 5.
A solar battery unit is configured to have the same configuration as described in the foregoing (2) except that, as illustrated in
It is desirable that the heat transfer sheet 3 have a bulk density of from 0.3 Mg/m3 to 1.0 Mg/m3 (desirably 0.9 Mg/m3 or lower, particularly desirably 0.8 Mg/m3 or lower). In addition, it is desirable that the pressure to the heat transfer sheet 3 be from 0.5 MPa to 10.0 MPa, and further, it is desirable that the heat transfer sheet 3 has a thickness of from 0.1 mm to 3.0 mm. The reason is the same as described in the section that has described the configuration of the solar battery unit shown in the foregoing (1).
(1) The heat dissipating member 4 is not limited to that described above. It may have a structure in which coolant passages 6 . . . for passing coolant such as water are provided in a main unit 4b, as illustrated in
(2) Generally, the heat transfer sheet 3 is rarely recycled. However, when recycling is taken into consideration, it is desirable to make the following restrictions.
When compressing the heat transfer sheet 3, it is desirable that the heat transfer sheet 3 be adjusted so that the compression ratio represented by the following equation (1) will be 50% or greater and the recovery ratio represented by the following equation (2) will be 5% or greater. With such a configuration, even when the heat transfer sheet 3 is compressed a plurality of times, the bulk density thereof after the pressure is removed is kept at less than 1.0 Mg/m3. Therefore, when the heat transfer sheet 3 is compressed in such a state as to be sandwiched between the solar battery module 2 and the heat dissipating member 4, the adhesion of the heat transfer sheet 3 with the solar battery module 2 and the heat dissipating member 4 can be kept high even after the heat transfer sheet 3 has been used a plurality of times. As a result, the thermal resistance can be kept small even after the heat transfer sheet 3 has been used a plurality of times. Thus, recyclability can be improved.
Compression ratio(%)=[(t1−t2)/t1]×100 (1)
In the above equation (1), t1 is the thickness (mm) of the heat transfer sheet after applying a pre-load (0.686 MPa±1%) for 15 seconds, and t2 is the thickness (mm) of the heat transfer sheet after applying a total pressure (34.3 MPa±1%) for 60 seconds.
Recovery ratio(%)=[(t3−t2)/(t1−t2)]×100 (2)
In the above equation (2), t1 is the thickness (mm) after applying a pre-load (0.686 MPa±1%) for 15 seconds, t2 is the thickness (mm) after applying a total pressure (34.3 MPa±1%) for 60 seconds, and t3 is the thickness after resetting the pressure to the pre-load and elapsing 60 seconds.
In particular, when the heat transfer sheet is adjusted so that the compression ratio represented by the above equation (1) is 55% or greater and the recovery ratio represented by the above equation (2) is 6% or greater, the heat transfer sheet can be kept more reliably in such a state that the bulk density is less than 1.0 Mg/m3, for example, less than 0.9 Mg/m3, after the pressure has been removed, so that the recyclability can be improved further.
It is undesirable that the heat transfer sheet 3 have a compression ratio of less than 50% because the adhesion with the solar battery module 2 and the heat dissipating member 4 becomes poor. It is also undesirable that the heat transfer sheet 3 have a recovery ratio of less than 5% because the adhesion with the solar battery module 2 and the heat dissipating member 4 cannot be kept high when the heat transfer sheet is recycled so the heat transfer sheet cannot cope with recycling.
In addition, if the self weight of the solar battery module 2 is too great even when the heat transfer sheet 3 has a bulk density of less than 1.0 Mg/m3, the pressure applied to the heat transfer sheet 3 will be too high, so the solar battery module may be damaged (specifically, when the pressure exceeds 10.0 MPa).
By using the heat transfer sheet 3 having a bulk density of 0.9 Mg/m3 or lower and restricting the pressure applied to the heat transfer sheet 3 to be 1.5 MPa or lower as described above, the bulk density of the heat transfer sheet 3 after removing the pressure can be kept at 0.9 Mg/m3 or lower, the adhesion between the solar battery module 2 and the heat transfer sheet 3 and between the heat transfer sheet 3 and the heat dissipating member 4 can be improved, and moreover, the recoverability can be also maintained. As a result, the thermal resistance can be reduced by further increasing the adhesion of the heat transfer sheet 3 with the solar battery module 2 and with the heat dissipating member 4 while ensuring the recyclability of the heat transfer sheet 3.
In particular, by using the heat transfer sheet 3 having a bulk density of 0.8 Mg/m3 or lower and restricting the pressure applied to the heat transfer sheet 3 to be 1.0 MPa or lower, the bulk density of the heat transfer sheet 3 after removing the pressure can be kept at 0.8 Mg/m3 or lower, the adhesion of the heat transfer sheet 3 with the solar battery module 2 and with the heat dissipating member 4 can be improved, and moreover, the recoverability can be maintained.
In the case that the self weight of the solar battery module 2 is low, it is possible that the pressure applied to the heat transfer sheet 3 becomes so low (specifically, when the pressure becomes less than 0.5 MPa), resulting in poor adhesion between the solar battery module 2 and the heat transfer sheet 3 and between the heat transfer sheet 3 and the heat dissipating member 4, and consequently, the thermal resistance may not be reduced sufficiently. For this reason, in such a case, it is preferable to use a clamp 9 that can sandwich the solar battery module 2, the heat transfer sheet 3, and the heat dissipating member 4, as illustrated in
(3) An insulating sheet layer made of, for example, polyethylene terephthalate may be formed on the surface of the heat transfer sheet 3 in the case that insulation is necessary between the solar battery module 2 and the heat transfer sheet 3.
(4) The solar battery unit to which the heat transfer sheet 3 is attached can be prevented from deteriorating reliably when the heat transfer sheet 3 is treated so that the total amount of impurities contained, such as sulfur and iron contents, will be 10 ppm or less, in particular, the sulfur content will be 1 ppm or less.
(5) A resin film of polyethylene terephthalate or the like may be disposed between the heat transfer sheet 3 and the solar battery module 2 and/or between the heat transfer sheet 3 and the heat dissipating member 4. This configuration makes it possible to prevent the expanded graphite or the like detached from the heat transfer sheet 3 from scattering around the heat transfer sheet 3. In this case, the resin film to be used is not particularly limited as long as the resin film has almost the same thermal conductivity across the thickness as the heat transfer sheet 3 and a heat resistance of about 100° C.
An example of the present invention will be described below with reference to
As illustrated in
Two stainless steel plates (width L3=80 mm, length L4=115 mm, thickness=0.1 mm) 20a and 20b are affixed to the back surface of the solar battery module 1 by silicone grease (viscosity 330 Pa·s, thermal conductivity 0.9 W/(m·K)), which is not shown in the drawings, as illustrated in
The same configuration as described in the foregoing Example is employed, except that an aluminum plate 22 having the same dimensions as those of the heat transfer sheet 23 (the width, length, and the thickness thereof are identical to those of the heat transfer sheet of the foregoing example) is affixed to a stainless steel plate 20b (the stainless steel plate located on the right in
As shown in
Using the above-described test equipment, light was applied to the front side of the solar battery module 1 to continuously measure the temperatures of the front surfaces and the back surfaces in the portions of the solar battery module 1 that correspond to the Example and the Comparative Example by the thermocouples 18a to 18f. The results are shown in
As clearly seen from
The present invention can be applied to solar battery units.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2007-249962 | Sep 2007 | JP | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/JP2008/067400 | 9/26/2008 | WO | 00 | 3/24/2010 |
