Transparent heat-mirror

• US 4,337,990 A
• Filed: 05/27/1976
• Issued: 07/06/1982
• Est. Priority Date: 08/16/1974
• Status: Expired due to Term

• Current Assignee: Massachusetts Institute of Technology
• Original Assignee: Massachusetts Institute of Technology
• Inventors: Fan, John C. C., Bachner, Frank J.
• Primary Examiner(s): Lee, John D.
• Application Number:
  US05/690,696
• Time in Patent Office: 2,231 Days
• Field of Search: 350/1, 350/164, 350/166, 350/1.1, 350/1.6, 350/1.7, 250/510, 126/270, 204/192 R, 204/192 C, 204/192 P
• US Class Current: 359/360
• CPC Class Codes: F24S 80/52 characterised by the material for preventing heat loss F24S80/56
• CPC Class Codes: F24S 80/56 characterised by means for preventing heat loss
• CPC Class Codes: G02B 5/282 reflecting for infrared and transparent for visible light, e.g. heat reflectors, laser protection
• CPC Class Codes: Y02B 10/20 Solar thermal
• CPC Class Codes: Y02E 10/40 Solar thermal energy, e.g. solar towers

Abstract

Transparent heat-mirrors are disclosed which are comprised of composite films. These films include a discrete and continuous layer of metallic silver sandwiched between a transparent, outer, protective, anti-reflection layer and a transparent, phase-matching layer. This combination of layers is chosen to provide high solar transmission with minimum loss of thermal radiation. Transparent heat-mirrors are useful in the collection and trapping of solar energy, and in other applications where it is desired or necessary to have high infrared reflectivity with high solar transmission.

Claims

1. A composite film consisting of three continuous and discrete layers, one of said layers being metallic silver in a thickness of from about 30 A to about 200 A and the other two layers being transparent and positioned on opposite sides of said metallic silver layer, each of said transparent layers having a thickness within the range of from about 150 A to about 500 A, and said transparent layers being ones which cooperate to provide the composite film with an integrated solar transmission, α

_eff, of at least about 0.5 and a ratio of integrated solar transmission to integrated heat reflectivity, α

_eff /ε

_eff, of at least about 5 where integrated solar transmission (α

_eff) and integrated heat reflectivity (ε

_eff) are defined as;

##EQU2## wherein Tr(λ

)=Transmission of heat-mirror at wavelength λ

R(λ

)=Reflectivity of heat-mirror at wavelength λ

A(λ

)=Solar energy spectrum

W_B (T_B,λ

)=Energy distribution for a blackbody at an operating temperature T_B.

2. A composite film of claim 1 wherein both of said transparent layers are layers of titanium dioxide.

3. In a transparent heat-mirror comprising a single, continuous, discrete layer of metallic silver having a thickness of from about 30 A to about 200 A and an outer, transparent, protective, anti-reflection coating on one side of said metallic silver layer having a thickness of from about 150 A to about 500 A:

the improvement of providing a transparent coating having a thickness of from about 150 A to about 500 A on the inner side of said metallic silver layer, said transparent coating on the inner side of said metallic silver layer being one which cooperates with said outer, transparent, anti-reflection coating to provide the transparent heat-mirror with an α

_eff of at least about 0.5 and an α

_eff /ε

_eff ratio of at least about 5.

4. The improvement of claim 3 wherein said transparent coating on the inner side of said metallic silver layer is a coating of a material selected from the group consisting of titanium dioxide, silicon dioxide, silicon monoxide, bismuth oxide, indium oxide, tin oxide, chromium oxide, zinc sulfide, and magnesium fluoride.

5. The improvement of claim 4 wherein said outer, transparent, protective, anti-reflection coating is formed from a material selected from the group consisting of titanium dioxide, silicon dioxide, silicon monoxide, bismuth oxide, indium oxide, tin oxide, chromium oxide, zinc sulfide, and magnesium fluoride.

6. The improvement of claim 3 wherein said transparent coating on the inner side of the metallic silver layer is a coating of titanium dioxide.

7. The improvement of claim 6 wherein the outer, transparent, protective, anti-reflection coating is formed from titanium dioxide.

8. The improvement of claim 7 wherein said outer, transparent, protective, anti-reflection coating and said transparent coating on the inner side of the metallic silver layer have substantially the same thickness.

9. An article comprising a transparent substrate having a composite film thereon, said composite film having a single, continuous, discrete layer of metallic silver having a thickness from about 30 A to about 200 A, said metallic silver layer being sandwiched between an outer, protective, transparent, anti-reflection layer and an inner, adherent, transparent layer each having a thickness of from about 150 A to about 500 A, said outer and inner transparent layers providing said composite film with an α

_eff of at least about 0.5 and an α

_eff /ε

_eff ratio of at least about 5.

10. An article of claim 9 wherein said transparent substrate comprises quartz.

11. An article of claim 9 wherein said transparent substrate comprises glass.

12. An article of claim 9 wherein both said outer, protective, transparent, anti-reflection layer and said inner, adherent, transparent layer are formed from titanium dioxide.

13. In the collection of solar energy by using an absorber to absorb radiation from the sun, the improvement of using a transparent, heat-mirror in combination with the absorber wherein said heat-mirror comprises a composite film formed from a single, continuous, discrete layer of metallic silver having a thickness of from about 30 A to about 200 A sandwiched between an outer, transparent, protective, anti-reflection coating and an inner, adherent, transparent coating, said inner and outer coatings providing the composite film with an α

_eff of at least 0.8 and an α

_eff /ε

_eff ratio of at least about 10.

14. A transparent heat-mirror consisting of a transparent substrate with a composite film, said composite film consisting of a single, continuous, discrete layer of metallic silver having a thickness of from about 30 A to about 200 A and two discrete layers of titanium dioxide located on opposite sides of said metallic silver layer and both having a thickness within the range of from about 150 A to about 500 A, said layers of titanium dioxide being sufficient to provide said transparent heat-mirror with an α

_eff of at least about 0.5 and an α

_eff /ε

_eff ratio of at least about 5.

15. In the formation of a composite film, which transmits visible light energy and reflects infrared light energy, on a substrate:

the improvement comprising respectively sputtering onto said substrate a first transparent layer, a silver layer, and a second transparent layer, under sputtering conditions which produce discrete layers in thicknesses which provide cooperation between said layers to provide a composite film having significantly increased visible light energy transmission compared to said silver layer alone and having high infrared light energy reflectivity.

16. The improvement of claim 15 wherein said first and said second transparent layers comprise titanium dioxide.

17. A composite film comprising a sputtered, continuous, discrete, silver layer sandwiched between two sputtered, continuous, discrete layers of titanium dioxide, said silver and titantium dioxide layers having thicknesses that cooperate to provide said composite film with significantly higher solar energy transmission compared to said silver layer alone and having high infrared reflectivity.

18. A composite film consisting of a layer of metallic silver sandwiched between layers of titanium dioxide, each of said layers being continuous, discrete and having a thickness of about 180 A.

19. A method of producing a composite film on a substrate, said composite film having high solar energy transmission and high infrared reflectivity, comprising:

sputtering a first, continuous, discrete, transparent layer over said substrate;

subsequently, sputtering a continuous, discrete, silver layer over said first layer; and

,

thereafter, sputtering a second, continuous, discrete, transparent, layer over said silver layer,

said first and said second transparent layers and said silver layer each being sputtered to a thickness so that all three layers cooperate to provide a composite film having significantly increased solar energy transmission compared to said silver layer alone and having high infrared reflectivity.

20. A method of claim 19 wherein the transparent layers are formed from materials in appropriate thicknesses and the silver layer has an appropriate thickness to provide a composite film having an integrated solar transmission, α

_eff, of at least about 0.5 and a ratio of integrated solar transmission to integrated heat reflectivity, α

_eff /ε

_eff, of at least about 5 where integrated solar transmission (α

_eff) and integrated heat reflectivity (ε

_eff) are defined as;

##EQU3## wherein TR(λ

)=Transmission of heat-mirror at wavelength λ

R(λ

)=Reflectivity of heat-mirror at wavelength λ

A(λ

)=Solar energy spectrum

W_B (T_B, λ

)=Energy distribution for a blackbody at an operating temperature T_B.

21. A method of claim 20 wherein said transparent layers are formed from a material selected from the group of titanium dioxide, silicon dioxide, silicon monoxide, bismuth oxide, tin oxide, indium oxide, chromium oxide, zinc sulfide and magnesium fluoride.

22. A method of claim 21 wherein said transparent layers have thicknesses of from about 150 A to about 500 A.

23. A method of claim 20 wherein said transparent layers are formed from titanium dioxide in thicknesses of from about 150 A to about 500 A.

24. A method of claim 23 wherein said transparent layers have thicknesses which are substantially the same.

25. A composite film on a substrate produced according to a method of claims 19, 20, 21, 22, 23, or 24.

26. A composite film on a substrate of claim 25 wherein the silver layer has a thickness of between about 30 A and about 200 A.