Abstract:
A glazing panel has a coating stack comprising in sequence at least a base antireflective layer, an infra-red reflecting layer, a top antireflective layer and a top coat layer comprising at least one material selected from the group consisting of nitrides, oxynitrides, carbides, oxycarbides and carbonitrides of the elements of groups IVb, Vb and VIb of the periodic table.

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
     This application is the entry into the U.S. National Stage of PCT Application No. PCT/EP2004/050073, filed Feb. 3, 2004, claiming priority from European Application EP 03003397.1 filed Feb. 14, 2003, the disclosures of both of which are hereby incorporated by reference. 
     BACKGROUND 
     This invention relates to glazing panels and particularly, but not exclusively, to solar control and/or low emissivity glazing panels which are intended to undergo heat treatment following application to the glazing substrate of an optical filter in the form of a coating stack. 
     The invention relates more particularly to cases where a coating stack is applied to the glazing by a vacuum deposition technique, for example by sputtering or magnetron sputtering. 
     Multiple factors must be considered when designing coating stacks for glazing applications. These incdude not only the desired opto-energetic performance of the coated glazing panel but also, for example, the abrasion resistance of the coating stack (to facilitate handling and processing), the stability and chemical durability of the coating stack (to facilitate storage under various conditions) and the tolerances of the control of the manufacturing process (to facilitate acceptable manufacturing yields and consistency between product runs). 
     It is known to apply a top coat to a coating stack particularly in an attempt to increase the abrasion resistance and/or chemical durability of a coatings stack The use of metallic layers (for example of chromium, nickel chromium or zinc) or dielectric layers (for example titanium oxide, silicon oxide, zinc oxide, silicon nitride, aluminium nitride) has been proposed in this context. However, many known non-metallic top coats suffer from insufficient chemical durability, whilst known metallic top coats can have a number of disadvantages. 
     SUMMARY 
     The present invention provides glazing panels, a method of manufacturing glazing panels and use of a top coat layer as defined in the independent claims. Preferred embodiments are defined in the dependent claims. 
     The present invention may provide an advantageous combination of good: 
     chemical durability, especially where the top coat comprises a nitride or an oxynitride 
     humidity resistance, particularly when the top coat comprises titanium nitride 
     stability of manufacturing parameters 
     heat treatability 
     The top coat layer is preferably the outermost, exposed layer of the coating stack. 
     The coating layers are preferably deposited by a vacuum deposition technique, particularly magnetron sputtering. 
     One advantage of the top coats of the present invention may be a combination of particularly good chemical durability during storage, for example prior to heat treatment and/or assembly, with a facility to control the manufacturing tolerances and production process. This may be combined with an ability to provide thermal protection to other parts of the coating stack during heat treatment With known metallic top coats: 
     Small variations in the thickness of a metallic top coat can significantly affect the properties of the heat treated coated glazing panel and/or the heat treatment conditions that must be used, especially if the metal is relatively difficult to oxidise during heat treatment. 
     If a highly reactive metal is used then this will partially oxidise in air during storage prior to heat treatment of the glazing panel. The extent of this oxidation may be difficult to control as it may depend upon the ambient temperature, the humidity and other storage conditions and even the temperature of the glazing panel when it first enters the atmosphere at the exit of a vacuum coating line (the glazing panel temperature will generally be lower for thicker substrates). 
     Consequently, It can be difficult to control the manufacturing tolerances and precise condition of an intermediate coated glazing panel that arrives to be heat treated. The significant difference in refractive index and/or extinction coefficient between a metal top coat before and after heat treatment may also renders the control of the thickness and heat treatment conditions critical to avoid unacceptable variations in properties such as light transmittance, energy transmittance and colour in the heat treated glazing panel. 
     Fine adjustment and control of the manufacturing tolerance of the thickness of the top coats of the present invention may be less critical to the variations of properties of the glazing panel; this may facilitate higher manufacturing yields and/or throughput. Furthermore, where the refractive indexes and/or extinction coefficients of the top coats of the present invention are reasonably similar both before and after heat treatment (for example with a variation in refractive index at 550 nm of less than 1, 0.8, 0.6. 0.5, 0.4, 0,3 or 0.2 due to heat treatment and/or a variation in extinction coefficient at 550 nm of less than 1,5; 1,4, 1,3, 1,2, 1, 0.8, 0.6. 0.5, 0.4, 0,3 or 0.2 due to heat treatment), the tolerance of one or more properties, for example, luminous transmittance, energy transmittance, luminous reflection, colour in reflection, colour in transmittance, may be less prone to significant variation as a function of the manufacturing tolerances and storage time and conditions of the intermediate product prior to heat treatment. The present invention may also facilitate the use of a substantially identical coating stack on glazing substrates of different thickness (for example, 2 mm, 4 mm, 6 mm, 8 mm thick glass sheets) which require different conditions for correct heat treatment. 
     The use of a nitride or oxynitride top coat according to certain embodiments of the present invention may facilitate deposition control; this may especially be the case when a vacuum coater used to manufacture the glazing panels has been exposed to the atmosphere for maintenance and must be purged of air and/or water vapour contamination. Given that air is about 80% nitrogen, air contamination may be less disruptive to deposition of these materials. The effect of air and/or water vapour contamination on deposition in a reactive nitrogen and/or oxygen containing atmosphere is less significant than equivalent contamination in an inert (eg argon) sputtering atmosphere used for the deposition of metal layers as, in the latter case, the contaminants are the only reactive species present in the deposition atmosphere. 
     Where the glazing panel carries a coating stack having a single silver or other infra-red reflecting metal layer and having, for example, the structure: 
     Glass 
     base antirefective dielectric layer 
     optional nucleation or barrier layer 
     infra red reflective metal layer 
     optional barrier layer 
     top antireflective dielectric layer 
     top coat layer 
     the base antireflective dielectric layer preferably has an optical thickness in the range of 50 nm to 80 nm whilst the combination of the top antireflective dielectric layer and the top coat layer preferably has an optical thickness in the range 50 nm to 100 nm. 
     Where the glazing panel carries a coating stack having a double silver or other infra-red reflecting metal layer and having, for example, the structure: 
     Glass 
     base antireflective dielectric layer 
     optional nucleation or barrier layer 
     infra red reflective metal layer 
     optional barrier layer 
     central antireflective dielectric layer 
     optional nucleation or barrier layer 
     infra red reflective metal layer 
     optional barrier layer 
     top antireflective dielectric layer 
     top coat layer 
     the base antireflective dielectric layer preferably has an optical thickness In the range of 35 nm to 80 nm, the central antireflective dielectric layer preferably has an optical thickness in the range 130 nm to 180 nm and the combination of the top antireflective dielectric layer and the top coat layer preferably has an optical thickness in the range 40 nm to 80 nm. 
     The top coat layer may have a geometrical thickness of greater than or to equal to 10 Å, 15 Å, 20 Å or 25 Å; it may have a geometrical thickness of less than or equal to 100 Å, 80 Å, 70 Å, 60 Å or 50 Å. The top coat layer preferably has a geometrical thickness in the range 15 to 50 Å, more preferably 20 to 40 Å particularly where it comprises a nitride or an oxynitride of titanium. Such thicknesses may provide an optimisation for providing a desired corrosion resistance whilst simultaneously providing a top coating layer which will provide desired characteristics, for example refractive index and/or extinction coefficient, after heat treatment. 
     The filter stack may comprise one or more barrier layers underlying and/or overlying the infra red reflecting layer, as is known in the art. Barriers of, for example, one or more of the following material may be used. Ti, Zn, Cr, “stainless steel”, Zr, Nb, Ni, NiCr, NiTi, ZnTi and ZnAl. Such barriers may be deposited, for example, as metallic layers or as sub-oxides (i.e. partially oxidised layers). Alternatively, nitrided barrier layers may also be used. Each barrier layer may consist of a single layer or may comprise two or more sub-layers which together form the barrier layer. The barrier layer may comprise a first barrier layer in substantially metallic form, e.g. comprising nickel and chromium, and an overlying second barrier layer of a different composition from the first barrier layer (e.g. comprising titanium) which is in a form selected from the group consisting of oxides, sub-stoichiometric oxides, nitrides, sub-stoichiometric nitrides, oxynitrides and sub-stoichiometric oxynitrides. 
     Each antireflective dielectric layer may consist of a single layer or may comprise two or more sub-layers which together form the antireflective dielectric layer. The top antireflective dielectric layer, or at least portion of the top antireflective dielectric layer which contacts the top coat layer may be of a material other than silicon nitride and/or other than aluminium nitride, it may comprise an oxide, for example an oxide comprising zinc and tin and/or zinc and aluminium. 
     The invention has particular utility in relation to glazing panels which, 
     when heat-treated will give a colour in reflection such that: 
     a* is between +2 and −10, preferably between 0 and −7; and 
     b* is between+2 and −15, preferably between 0 and −10; 
     or which 
     when heat-treated and assembled with a sheet of clear glass as double glazing units with the coating positioned inside the double glazing unit at position  2  (interior surface of exterior sheet of glass) or position  3  (interior surface of interior sheet of glass) will give a colour in reflection seen from the outside such that: 
     a* is between 0 and −7, preferably between 0 and −4; and 
     b* is between +2 and −10, preferably between 0 and −7. 
     Preferably, the glazing panels, when heat treated and presented in the form of monolithic glazing and/or in the form of assembled double glazing units provide a substantially neutral colour in reflection. 
     The combination of properties that may be provided by the present invention have particular advantages in relation to heat treatable and heat treated glazing panels. Nevertheless, the invention may also be used in respect of glazings which are not heat treated. The term “heat treatable glazing panel” as used herein means that the glazing panel carrying the coating stack is adapted to undergo a bending and/or thermal tempering and/or thermal hardening operation without the haze of the so treated glazing panel exceeding 0.5, and preferably without the haze exceeding 0.3. The term “substantially haze free heat treated glazing panel” as used herein means a glazing panel which has been bent and/or thermally tempered and/or thermally hardened and has a haze that does not exceed 0.5 and which preferably does not exceed 0.3. The thermal treatment may involve rising the temperature of the glazing panel to a temperature exceeding 400° C., 450° C., 500° C., 550° C., 600° C., 650° C. or 700° C. 
     Heat treatment may provoke an increase in the luminous transmittance (TL) of the glazing panel. Such an increase in TL may be advantageous in ensuring that TL is sufficiently high for the glazing panel to be used in high light transmittance glazings, for example, in vehicle windscreens or in architectural applications where the monolithic coated glazing panel is desired to have a TL greater than about 55%, 60%, 65%, 70%, 75%, 80% 85% or 90% or in double glazing units where the double glazing unit is desired to have a TL greater than about 55%, 60%, 65%, 70%, 75%, 80% or 85%. TL may increase in absolute terms during heat treatment by, for example, greater than about 2.5%, greater than about 3%, greater than about 4%, greater than about 5%, greater than about 8% or greater than about 10%. 
     The coating stack of the glazing panel of the present invention may be such that if applied to a clear sheet of 4 mm glass it would give a TL measured with Illuminant C of greater than about 55%, 60%, 65%, 70%, 75%, 80% 85% or 90% and/or an energetic transmittance (TE) (System Moon  2 ) of greater than about 35%, 40%, 50%, 55% or 60%. The coating stack may be responsible for a reduction of the TL of the glazing panel with in the range 10 to 20%. The energetic transmittance (System Moon  2 ) of the glazing panel may be greater than 40%, 45%, 50%, 55%, 60% or 65%. Such properties or combinations of properties may be particularly useful when the glazing panel is intended for use in low emissivity applications. 
     The coating stack of the glazing panel of the present invention may be such that if applied to a clear sheet of 4 mm glass it would give a combination of TL measured with Illuminant C and (TE) (System Moon  2 ) such that: 
     TL is greater than or equal to 70% and TE is less than or equal to 50%; or 
     TL is greater than or equal to 60% and TE is less than or equal to 42%; or 
     TL is greater than or equal to 50% and TE is less than or equal to 35%; or 
     TL is greater than or equal to 40% and TE is less than or equal to 30%. 
     Such a combination of properties may be useful where the glazing panel is intended for solar control applications. 
     The top coat layer of the present invention may undergo some transformation or oxidation when stored in air, for example prior to an intended heat treatment operation. For example, where the top coat layer is initially deposited in the form of titanium nitride or titanium oxynitride, at least the superficial portion of the top coat layer which is exposed to air during storage may oxidise to titanium oxide. A similar effect may occur with other top coat layers of the invention. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       Examples of the present invention will now be described with reference to  FIG. 1  and  FIG. 2  which are cross-sections through glazing panels prior to a bending and tempering operation (for ease of representation, the relative thicknesses of the glazing panel and coating layers are not shown to scale). 
     
    
    
     DETAILED DESCRIPTION 
     EXAMPLE 1 
       FIG. 1  shows a single Ag layer, heat treatable, coating layer deposited on a glass substrate by magnetron sputtering and having the following sequential structure: 
     
       
         
               
               
               
               
             
               
               
               
               
               
             
           
               
                   
                   
               
               
                   
                 Reference 
                 Geometrical 
                 Atomic 
               
               
                   
                 number 
                 thickness 
                 ratios 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                 Glass substrate 
                 10 
                 4 
                 mm 
                   
               
               
                 Base antireflective layer 
                 11 
               
               
                 comprising: ZnSnOx 
                 12 
                 230 
                 Å 
                 Zn/Sn ≈ 2 
               
               
                 ZnSnOx 
                 13 
                 120 
                 Å 
                 Zn/Sn ≈ 17 
               
               
                 Ag (infra red reflective layer) 
                 14 
                 95 
                 Å 
               
               
                 NiCr heat treatment barrier layer 
                 15 
                 10 
                 Å 
               
               
                 Ti deposition barrier layer 
                 16 
                 20 
                 Å 
               
               
                 Top antireflective layer 
                 17 
               
               
                 comprising: 
               
               
                 ZnSnOx 
                 18 
                 130 
                 Å 
                 Zn/Sn ≈ 17 
               
               
                 ZnSnOx 
                 19 
                 210 
                 Å 
                 Zn/Sn ≈ 2 
               
               
                 Top coat layer comprising TiN 
                 20 
                 25 
                 Å 
               
               
                   
               
             
          
         
       
     
     In this type of structure, the Ag layer acts to reflect incident infra red radiation and in order to fulfil this role must be maintained as silver metal rather than silver oxide and must not be contaminated by adjacent layers. The dielectric antireflective layers which sandwich the Ag layer serve to reduce the reflection of the visible portion of the spectrum which the Ag layer would otherwise provoke. The heat treatment barrier serves to prevent degradation of the Ag layer during heat treatment of the glazing panel; it is usually at least partially oxidised in this process. The deposition barrier serves to prevent oxidation of the heat treatment barrier during sputtering of the overlying dielectric antireflective layer in an oxidising atmosphere; this barrier is at least partially oxidised during this process. 
     Properties of the glazing panel prior and subsequent to heat treatment process are: 
     
       
         
               
               
               
             
           
               
                   
               
               
                   
                 Prior to heat 
                 Following heat 
               
               
                 Property 
                 treatment see Note 1 below   
                 treatment see Note 2 below   
               
               
                   
               
             
             
               
                 TL (Illuminant C) 
                   77% 
                 87% 
               
               
                 TE (System Moon 2) 
                 57.5% 
                 67% 
               
               
                 haze 
                 0.08 
                 0.16 
               
               
                 a* reflectance 
                 −4 
                 −3 
               
               
                   
                 (coated side) 
                 (coated side) 
               
               
                 b* reflectance 
                 −17 
                 −12 
               
               
                   
                 (coated side) 
                 (coated side) 
               
               
                 RE (System Moon 2) 
                   20% 
                 22% 
               
               
                   
                 (coated side) 
                 (coated side) 
               
               
                   
               
               
                   Note 1 Measured for monolithic glazing panel with coating prior to heat treatment 
               
               
                   Note 2 Measured following a tempering heat treatment process at 680° C. (furnace temperature) for 8 minutes Heat treatment preferably causes substantially complete oxidation of the titanium nitride top coat layer. 
               
             
          
         
       
     
     The colour co-ordinates of the examples are particularly suited to architectural double glazing units as they give a neutral appearance in reflection. 
     Samples according to Example 1 were subjected prior to tempering to a Cleveland Condensation resistance test and a Climatic Chamber test (Cycled condensation resistance test). 
     The Cleveland test consists of subjecting the coated glass to a water-saturated atmosphere at constant temperature. The samples have condensation continually forming on them and it is this condensation that may cause surface degradation. A test cabinet (Cleveland) is placed in a room with an ambient temperature of 23° C. ±3. Care is taken to ensure that draughts and solar irradiation do not interfere with the test cabinet. The samples are mounted in a holder which forms the roof of the test cabinet. The floor of the test cabinet acts as the receptacle for the quantity of water. The test cabinet is conditioned only by heating the demineralised water on the floor with heating resistances controlled by means of a thermocouple, keeping a temperature of the water of 50°C. ±2. The samples are subjected to the test during 24 hours. 
     The Climatic chamber test consists of subjecting the samples in an atmosphere maintained at 98% relative humidity to a continuous cycle of a) increasing temperature from 45° C. to 55° C. over the space of one hour and b) subsequently decreasing the temperature from 55° C. to 45° C. over the space of one hour. This cycle is repeated for a period of three days. The test may be carried out in a 500 litre Weiss chamber. 
     Samples that have been subjected to each test are inspected for: a) punctual defects (diameter &lt;0.5 mm) like needles, a limited density of which may be acceptable; b) large defects such as spots of corrosion a few mm in diameter which are unacceptable; c) dissolution of the coating which is unacceptable. 
     The following result were obtained: 
     
       
         
               
               
               
             
           
               
                   
               
               
                   
                   
                 Comparative example without 
               
               
                 Test 
                 Example 1 
                 top coat layer of Example 1 
               
               
                   
               
             
             
               
                 Cleveland 
                 No alteration 
                 More than 20 spots per dm2 some 
               
               
                   
                   
                 of which of diameter greater than 
               
               
                   
                   
                 1 mm 
               
               
                 Climatic chamber 
                 Less than 3 spots 
                 More than 20 spots per dm2 some 
               
               
                   
                 per dm2 of a 
                 of which of diameter greater than 
               
               
                   
                 diameter below 
                 1 mm 
               
               
                   
                 0.5 mm 
               
               
                 Suitable for long 
                 Yes 
                 Borderline 
               
               
                 duration storage 
               
               
                   
               
             
          
         
       
     
     It is anticipated that variations to example 1 in which the material of the top coat layer Is selected from an alternative as defined in the claims will have similar performances in the Cleveland and Climatic chamber tests. 
     The coating stack used in example 1 was also applied to other glass sheets having thicknesses of 4 mm, 6 mm and 8 mm. These sheets were stored in a variety of condition and for various durations (1 month for the 6 mm, 3 months for the 4 mm, 5 months for the 8 mm samples) prior to being tempered and then assembled into double glazing units. Typical properties of these glazings were: 
     
       
         
               
               
               
               
               
               
               
               
               
             
           
               
                   
               
               
                 Glass 
                 TL 
                 L 
                   
                   
                 R 
                 L 
                   
                   
               
               
                 Thickness 
                 (M) 
                 (M) 
                 a (M) 
                 b (M) 
                 (M) 
                 (DV) 
                 a (DV) 
                 b (DV) 
               
               
                   
               
             
             
               
                 4 mm 
                 88.0 
                 24.4 
                 −1.6 
                 −8.6 
                 3.5 
                 34.8 
                 −1.4 
                 −4.0 
               
               
                 6 mm 
                 87.8 
                 23.1 
                 −1.3 
                 −8.9 
                 3.7 
                 34.0 
                 −1.2 
                 −4.2 
               
               
                 8 mm 
                 86.4 
                 23.3 
                 −1.6 
                 −9.4 
                 3.6 
                 34.0 
                 −1.2 
                 −4.0 
               
               
                   
               
             
          
         
       
     
     In which L, a and b are the colour coordinates on the Hunter scale, R is the resistance per square, (M) indicates properties of the tempered, monolithic glazing measured from the coated side i.e. coating in position  1  and (DV) indicates properties of a double glazing unit incorporating the tempered, coated glazing panel with a sheet of 4 mm clear glass, measured from the outside of the double glazing unit with the coating in position  3   
     This demonstrates the stability of these properties with respect of the glass thickness and the storage conditions. 
     EXAMPLE 2 
       FIG. 2  shows a double Ag layer, heat treatable, coating layer deposited on a glass substrate by magnetron sputtering and having the following sequential structure: 
     
       
         
               
               
               
               
             
               
               
               
               
               
             
           
               
                   
                   
               
               
                   
                 Reference 
                 Geometrical 
                 Atomic 
               
               
                   
                 number 
                 thickness 
                 ratios 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                 Glass substrate 
                 10 
                 2 
                 mm 
                   
               
               
                 Base dielectric 
                 11 
               
               
                 comprising: AIN 
                 12 
                 150 
                 Å 
               
               
                 ZnAlOx 
                 13 
                 160 
                 Å 
                 Al/Zn ≈ 0.1 
               
               
                 Ag 
                 14 
                 100 
                 Å 
               
               
                 ZnAl overlying barrier 
                 15 
                 10 
                 Å 
                 Al/Zn ≈ 0.1 
               
               
                 Central dielectric 
                 16 
                 790 
                 Å 
                 Al/Zn ≈ 0.05 
               
               
                 comprising ZnAlOx 
               
               
                 Ag 
                 17 
                 110 
                 Å 
               
               
                 ZnAl overlying barrier 
                 18 
                 14 
                 Å 
                 Al/Zn ≈ 0.1 
               
               
                 Top dielectric comprising: 
                 19 
               
               
                 ZnAlOx 
                 20 
                 170 
                 Å 
                 Al/Zn ≈ 0.05 
               
               
                 AIN 
                 21 
                 85 
                 Å 
               
               
                 Top coat layer comprising TiN 
                 22 
                 30 
                 Å 
               
               
                   
               
             
          
         
       
     
     in which ZnAlOx is a mixed oxide containing Zn and Al deposited in this example by reactively sputtering a target which is an alloy or mixture of Zn and Al in the presence of oxygen. The ZnAl barriers are similarly deposited by sputtering a target which is an alloy or mixture of Zn and Al in a substantially inert, oxygen free atmosphere. 
     At least a portion of the overlying barriers  15 ,  18  is oxidised during deposition of their overlying oxide layers. Nevertheless, a portion of these barriers preferably remains in metallic form, or at least in the form of an oxide that is not fully oxidised to provide a barrier for subsequent heat treatment of the glazing panel. 
     Properties of the glazing panel prior and subsequent to heat treatment process are: 
     
       
         
               
               
               
             
           
               
                   
               
               
                   
                 Prior to heat 
                 Following heat 
               
               
                 Property 
                 treatment see Note 1 below   
                 treatment see Note 2 below   
               
               
                   
               
             
             
               
                 TL (Illuminant A) 
                 55% 
                 76% 
               
               
                 TE (System Moon 2) 
                   
                 43% 
               
               
                 haze 
                 0.07 
                 0.35 
               
               
                   
                   
                 (including pvb haze) 
               
               
                 a* 
                 −9 
                 −7 
               
               
                   
                 (glass side) 
                 (glass side) 
               
               
                 b* 
                 +4 
                 −6 
               
               
                   
                 (glass side) 
                 (glass side) 
               
               
                 RE (System Moon 2) 
                   
                 34% 
               
               
                   
                   
                 (glass side) 
               
               
                   
               
               
                   Note 1 Measured for monolithic glazing panel with coating prior to heat treatment 
               
               
                   Note 2 Measured following a tempering heat treatment process at 650° C. (furnace temperature) for 10 minutes and lamination with a 0.76 mm layer of pvb and a 2 mm sheet of clear glass 
               
             
          
         
       
     
     Heat treatment preferably causes substantially complete oxidation of the titanium nitride top coat layer. 
     Prior to heat treatment, the coating stack of Example 2 also performs well in the Cleveland and Climatic chamber tests. 
     Additional layers may be introduced above, below or between the film stacking arrangement if desired without departing from the invention. 
     GLOSSARY 
     Unless otherwise indicated by the context, the terms listed below have the following meanings in this specification: 
     
       
         
               
               
               
             
           
               
                   
               
             
             
               
                 a* 
                   
                 colour co-ordinate measured on the CIELab 
               
               
                   
                   
                 scale at normal incidence 
               
               
                 Ag 
                 silver 
                   
               
               
                 Al 
                 aluminium 
               
               
                 Al2O3 
                 aluminium 
               
               
                   
                 oxide 
               
               
                 AlN 
                 aluminium 
               
               
                   
                 nitride 
               
               
                 b* 
                   
                 colour co-ordinate measured on the CIELab 
               
               
                   
                   
                 scale at normal incidence 
               
               
                 Cr 
                 chromium 
               
               
                 haze 
                   
                 the percentage of transmitted light which in 
               
               
                   
                   
                 passing through the specimen deviates from 
               
               
                   
                   
                 the incident beam by forward scattering, as 
               
               
                   
                   
                 measured in accordance with the ASTM 
               
               
                   
                   
                 Designation D 1003-61 (Reapproved 1988). 
               
               
                 infra red 
                   
                 a material that has a reflectance higher than 
               
               
                 reflecting 
                   
                 the reflectance of sodalime glass in the band 
               
               
                 material 
                   
                 of wavelenghts between 780 nm and 50 
               
               
                   
                   
                 microns 
               
               
                 Na 
                 sodium 
               
               
                 Nb 
                 niobium 
               
               
                 NiCr 
                   
                 an alloy or mixture comprising nickel and 
               
               
                   
                   
                 chromium 
               
               
                 NiTi 
                   
                 an alloy or mixture comprising nickel and 
               
               
                   
                   
                 titanium 
               
               
                 RE 
                 energetic 
                 the solar flux (luminous and non-luminous) 
               
               
                   
                 reflection 
                 reflected from a substrate as a percentage of 
               
               
                   
                   
                 the incident solar flux 
               
               
                 selectivity 
                   
                 the ratio of the luminous transmittance to the 
               
               
                   
                   
                 solar factor i.e. TL/TE 
               
               
                 Si02 
                 silicon oxide 
               
               
                 Si3N4 
                 silicon nitride 
               
               
                 SnO2 
                 tin oxide 
               
               
                 Ta 
                 tantalum 
               
               
                 TE 
                 energetic 
                 the solar flux (luminous and non-luminous) 
               
               
                   
                 transmittance 
                 transmitted through a substrate as a 
               
               
                   
                   
                 percentage of the incident solar flux 
               
               
                 Ti 
                 titanium 
               
               
                 TL 
                 luminous 
                 the luminous flux transmitted through a 
               
               
                   
                 transmittance 
                 substrate as a percentage of the incident 
               
               
                   
                   
                 luminous flux 
               
               
                 Zn 
                 zinc 
               
               
                 ZnAl 
                   
                 an alloy or mixture comprising zinc and 
               
               
                   
                   
                 aluminium 
               
               
                 ZnAlOx 
                   
                 a mixed oxide containing zinc and 
               
               
                   
                   
                 aluminium 
               
               
                 ZnAlO y   
                   
                 a partially oxidised mixture comprising zinc 
               
               
                   
                   
                 and aluminium 
               
               
                 ZnO 
                 zinc oxide 
               
               
                 ZnTi 
                   
                 an alloy or mixture comprising zinc and 
               
               
                   
                   
                 titanium 
               
               
                 ZnTiOx 
                   
                 a mixed oxide containing zinc and titanium 
               
               
                 ZnTiO y   
                   
                 a partially oxidised mixture comprising zinc 
               
               
                   
                   
                 and titanium 
               
               
                 Zr 
                 zirconium