EP4676882A1 - Gel de silice humide et aérogel - Google Patents

Gel de silice humide et aérogel

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Publication number
EP4676882A1
EP4676882A1 EP23783645.7A EP23783645A EP4676882A1 EP 4676882 A1 EP4676882 A1 EP 4676882A1 EP 23783645 A EP23783645 A EP 23783645A EP 4676882 A1 EP4676882 A1 EP 4676882A1
Authority
EP
European Patent Office
Prior art keywords
silica
silica aerogel
wet gel
less
sheet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP23783645.7A
Other languages
German (de)
English (en)
Inventor
Reaz CHOWDHURY
Mohammad ARIFUZZAMAN
Kellen KITZMAN
Kari B. Myli
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cardinal CG Co
Original Assignee
Cardinal CG Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US18/181,342 external-priority patent/US20230286810A1/en
Application filed by Cardinal CG Co filed Critical Cardinal CG Co
Publication of EP4676882A1 publication Critical patent/EP4676882A1/fr
Pending legal-status Critical Current

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Classifications

    • C—CHEMISTRY; METALLURGY
    • C01—INORGANIC CHEMISTRY
    • C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B33/00—Silicon; Compounds thereof
    • C01B33/113—Silicon oxides; Hydrates thereof
    • C01B33/12—Silica; Hydrates thereof, e.g. lepidoic silicic acid
    • C01B33/14—Colloidal silica, e.g. dispersions, gels, sols
    • C01B33/155—Preparation of hydroorganogels or organogels
    • C—CHEMISTRY; METALLURGY
    • C01—INORGANIC CHEMISTRY
    • C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B33/00—Silicon; Compounds thereof
    • C01B33/113—Silicon oxides; Hydrates thereof
    • C01B33/12—Silica; Hydrates thereof, e.g. lepidoic silicic acid
    • C01B33/14—Colloidal silica, e.g. dispersions, gels, sols
    • C01B33/157—After-treatment of gels
    • C01B33/158—Purification; Drying; Dehydrating
    • C01B33/1585—Dehydration into aerogels
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/66—Units comprising two or more parallel glass or like panes permanently secured together
    • E06B3/67—Units comprising two or more parallel glass or like panes permanently secured together characterised by additional arrangements or devices for heat or sound insulation or for controlled passage of light
    • E06B3/6715—Units comprising two or more parallel glass or like panes permanently secured together characterised by additional arrangements or devices for heat or sound insulation or for controlled passage of light specially adapted for increased thermal insulation or for controlled passage of light

Definitions

  • the present invention relates to a precursor material for a silica wet gel and methods of making silica wet gel.
  • the present invention also relates to silica wet gel and methods of making silica wet gel.
  • the present invention also relates to silica aerogel and methods of making silica aerogel.
  • the present invention relates to silica aerogel sheets and methods of making silica aerogel sheets.
  • the present invention relates to an article having a glass sheet and a silica aerogel sheet and methods of making such an article.
  • the present invention relates to an insulating glazing unit having a silica aerogel sheet between glass sheets and methods of making such an insulating glazing unit.
  • the present invention relates to a laminated glass assembly having a silica aerogel sheet between glass sheets and methods of making such a laminated glass assembly.
  • Silica aerogels are themially insulating materials, but traditionally they have had limited applications in windows and other glazings because they have not traditionally achieved the right combination of mechanical, thermal and optical properties to be fully acceptable for all such applications.
  • researchers have experimented with many different precursor recipes and methods in the hope of producing silica aerogel with an optimum combination of mechanical, thermal and optical properties but have been unsuccessful. While some recipes and methods led to certain properties being optimized, other properties were compromised.
  • silica wet gel silica aerogel and methods of making such materials that can be used to form an enhanced silica aerogel sheet having a desirable combination of mechanical, thermal and/or optical properties. It would be particularly desirable to provide silica aerogel that has high visible transmission and low haze. Further, it would be desirable to provide an article comprising a glass sheet and an enhanced silica aerogel sheet. It would also be desirable to provide an insulating glazing unit comprising an enhanced silica aerogel sheet. Similarly, it would be desirable to provide a laminated glass assembly comprising an enhanced silica aerogel sheet. It would also be desirable to provide methods of making high quality silica aerogel that are commercially feasible and do not require expensive or excessive processing.
  • FIG. 1 is a flow chart depicting a method of making silica wet gel in accordance with certain embodiments of the present invention
  • FIG. 2 is a flow chart depicting a method of making silica aerogel in accordance with certain embodiments
  • FIG. 3 is a flow chart depicting a method of making a silica aerogel sheet in accordance with certain embodiments
  • FIG. 4 is a schematic, broken-away, cross-sectional side view of an article having a glass sheet and a silica aerogel sheet in accordance with certain embodiments;
  • FIG. 5 is a flow chart depicting a method of making an article having a glass sheet and a silica aerogel sheet in accordance with certain embodiments
  • FIG. 6 illustrates perspective views of a mold tray being used in a method of making a silica aerogel sheet according to certain embodiments
  • FIG. 7 is a flow chart depicting another method of making an article having a glass sheet and a silica aerogel sheet in accordance with certain embodiments
  • FIG. 8 illustrates perspective views of a sidewall mold being used in a method of making a silica aerogel sheet according to certain embodiments
  • FIG. 9 is a schematic, partially broken-away, cross-sectional side view of an insulating glazing unit in accordance with certain embodiments.
  • FIG. 10 is a schematic, partially broken-away, cross-sectional side view of a laminated glass assembly in accordance with certain embodiments;
  • FIG. 11 is a schematic illustration of a setup for measuring the shadow projection of a silica aerogel sheet in accordance with certain embodiments.
  • FIG. 12 includes a distortion image and corresponding SSIM obtained from a silica aerogel sheet sample.
  • FIG. 13 is a graph showing linear shrinkage versus haze properties for silica aerogel sheet samples obtained from three different solvents.
  • FIG. 14 is a graph showing solvent remaining versus haze properties for silica aerogel sheet samples obtained from three different solvents.
  • FIG. 15 is a graph showing bending stress versus strain properties for silica aerogel sheet samples obtained from three different solvents.
  • Certain embodiments include a method of making a silica aerogel.
  • the method comprises steps of (a) synthesizing a silica wet gel from methyl silicate 51, (b) aging the silica wet gel for an aging time period until structural changes of the silica wet gel no longer occur, (c) subjecting the silica wet gel to solvent extraction with methanol for an extraction time period, and (d) drying the silica wet gel to form a silica aerogel having a linear shrinkage value of 3% or less (e.g., 2.7% or less), a visible transmission greater than 98% and a haze value of 2.5% or less (e.g., 2.0% or less or 1.5% or less).
  • the step of drying the silica wet gel forms the silica aerogel such that less than 3% (e.g., less than 2.0%) methanol remains within the silica aerogel. Also, in some cases, the step of drying the silica wet gel forms the silica aerogel with a maximum resilience at complete breaking point of greater than 300 J/m 3 (e.g., greater than 400 J/m 3 ).
  • the aging step comprises aging the silica wet gel at room temperature. Further, the aging time period can be at least 7 days (168 hours). Also, the extraction time penod can be less than 24 hours.
  • the step of synthesizing the silica aerogel from methyl silicate 51 comprises steps of (a) preparing a first solution by mixing methyl silicate 51 and methanol, (b) preparing a second solution by mixing ammonium hydroxide and water, (c) mixing the first solution and the second solution together to form a precursor material, and (d) allowing components in the precursor material to react to form silica wet gel.
  • the precursor material can have a weight percent ratio of the methyl silicate 51 : water of between 0.25: 1 and 2:1, such as a weight percent ratio of the methyl silicate 51 :water of between 0.5:1 and 1: 1.
  • silica aerogel synthesized from methyl silicate 51.
  • the silica aerogel can have a visible transmission of at least 98% and a haze value of 2.5% or less, and further includes at least one of the following features (A) through (E):
  • the silica aerogel includes at least two, at least three, at least four or perhaps all of the features (A) through (E). In some cases, the silica aerogel has a haze value of 1.75% or less.
  • the silica aerogel can be prepared by a method comprising the steps of: (a) preparing a first solution by mixing methyl silicate 51 and methanol, (b) preparing a second solution by mixing ammonium hydroxide and water, (c) mixing the first solution and the second solution together to form a precursor material, (d) allowing components in the precursor material to react to form silica wet gel, (e) aging the silica wet gel for an aging time period until structural changes of the silica wet gel no longer occur, (1) subj ecting the silica wet gel to solvent extraction with methanol for an extraction time period, and (g) drying the silica wet gel to form the silica aerogel.
  • the precursor material can have a weight percent ratio of the methyl silicate 51 :water of between 0.25: 1 and 2: 1, such as a weight percent ratio of the methyl silicate 5 Ewater of between 0.5: 1 and 1: 1.
  • the step of drying the silica wet gel forms the silica aerogel with a linear shrinkage value of 2.7% or less.
  • silica aerogels having lower haze still may suffer from other undesirable optical defects.
  • One common optical defect is the appearance of optical distortion lines caused by structural non-uniformities within the silica aerogel.
  • Applicant has noted that as haze is reduced in the silica aerogel, optical distortion lines may become more visible.
  • Applicant developed silica wet gels that can be used to form enhanced silica aerogels, such as silica aerogel sheets, having few to no optical distortion lines while also maintaining other desirable properties.
  • Applicant has also developed methods of making silica aerogels, such as silica aerogel sheets, that have desirable properties.
  • the silica aerogel sheets are devoid of structural non-uniformities that create optical distortion lines visible to the naked eye.
  • the enhanced silica aerogel sheets can achieve an exceptional, surprising combination of optical, thermal and/or mechanical properties, which makes them highly advantageous for use in window applications.
  • the precursor material comprises a silica precursor, such as silicon alkoxide or alkoxysilane.
  • the precursor material serves as an intermediate product that is used to form silica wet gel.
  • silica wet gel refers to a material that is obtained by allowing components of a precursor material including silicon alkoxide to react to form a wet gel.
  • sica aerogel refers to a material that is obtained by removing liquid from a silica wet gel and replacing the liquid with a gas or vacuum.
  • the precursor material comprises (or consists essentially of or consists of) silicon alkoxide, solvent, water and base catalyst.
  • the silicon alkoxide, solvent, water and base catalyst are provided within selected weight percent ranges.
  • Applicant has identified a “sweet spot” of weight percent ranges for the precursor material that can be used to form silica wet gel, which in turn can be used to form silica aerogel having a surprising combination of optical, mechanical and/or thermal properties.
  • hydrolysis hydrolysis
  • condensation condensation
  • nucleation Several reactions take place during silica wet gel synthesis: hydrolysis, condensation, nucleation and growth. These various reactions can have different reaction rates depending on the components used for the precursor material.
  • the reaction rates affect mechanical, thermal and optical properties of a resulting silica aerogel.
  • the resulting aerogel is highly sensitive to variations in precursor material components and percentage of components.
  • the hydrolysis reaction rate is determined by the amount of catalyst in the precursor material.
  • the hydrolysis reaction is also exothermic, so it imparts heat to the precursor material, which in turn accelerates the condensation reaction rate. As a consequence, too much catalyst can accelerate the condensation reaction rate. Accelerated condensation reaction rates are undesirable since they can lead to an accelerated nucleation rate and an accelerated growth rate.
  • the three-dimensional polymer structure will have unduly large particle sizes. Larger particle sizes create more scattering of light, which in turn leads to undesirable properties such as increased haze and reduced visible transmission. All of these variabilities make silica wet gel and aerogel synthesis unpredictable.
  • the precursor material comprises silicon alkoxide, solvent, water and catalyst. Applicant has identified a “sweet spot” of weight percentage ranges for these components.
  • the precursor material comprises (or consists essentially of or consists of) silicon alkoxide at a weight percent greater than or equal to 15% and less than or equal to 24%, solvent at a weight percent of greater than or equal to 60% and less than or equal to 68%, water at a weight percent of greater than or equal to 15% and less than or equal to 17%, and catalyst at a weight percent of greater than or equal to 0.08% and less than or equal to 0.2%.
  • the silica wet gel material comprises (or consists essentially of or consists of) silicon alkoxide precursor at a weight percent greater than or equal to 15.28% and less than or equal to 19%, solvent at a weight percent of greater than or equal to 65.16% and less than or equal to 68.52%, water at a weight percent of greater than or equal to 15.68% and less than or equal to 16.04%, and catalyst at a weight percent of greater than or equal to 0.15% and less than or equal to 0.17%.
  • the silica wet gel has a specified weight percent ratio of silicon alkoxide precursor: water.
  • the silica wet gel has a weight percent ratio of the silicon alkoxide precursor: water of between 0.25: 1 and 2: 1, such as a weight percent ratio of the silicon alkoxide precursor: water of between 0.5:1 and 1: 1.
  • the precursor material comprises methyl silicate 51 as the silicon alkoxide.
  • methyl silicate 51 provides desirable results.
  • MS-51 provides desirable results because it is pre-hydrolyzed.
  • a hydrolysis reaction in the precursor material is absent, which leads to a lower condensation rate and thus a lower nucleation rate.
  • Lower nucleation rates allow the formation of a three-dimensional polymer structure with smaller particle sizes.
  • the resulting silica aerogel therefore has less scattering of light and therefore reduced haze and increased transmissivity.
  • aerogel particle size is desirably less than 5 nm to have the lowest possible light scattering and thus acceptable haze and transmissivity.
  • the precursor material has a weight percent ratio of the methyl silicate 51 : water of between 0.25: 1 and 2: 1, such as a weight percent ratio of the methyl silicate 51 :water of between 0.5:1 and 1:1.
  • a weight percent ratio of the methyl silicate 51 :water of between 0.5:1 and 1:1 Applicant has discovered that precursor materials having methyl silicate 51 : water within the listed weight percent ratios can be used to form silica wet gels and therefore silica aerogels materials having numerous desirable and unexpected properties.
  • the precursor material comprises methanol as the solvent.
  • methanol as the solvent
  • the resulting silica aerogel has less haze and less optical distortion than with other solvents.
  • the precursor material comprises ammonium hydroxide as the catalyst.
  • ammonium hydroxide as the catalyst, the resulting silica aerogel has less haze and less optical distortion than with other catalysts.
  • the precursor material comprises (or consists essentially of or consists of) methyl silicate 51, methanol, water and ammonium hydroxide.
  • the precursor material comprises (or consists essentially of or consists of) methyl silicate 51 at a weight percent of greater than or equal to 15% and less than or equal to 24%, methanol at a weight percent of greater than or equal to 60% and less than or equal to 68%, water at a weight percent of greater than or equal to 15% and less than or equal to 17%, and ammonium hydroxide at a weight percent of greater than or equal to 0.08% and less than or equal to 0.2%.
  • the precursor material comprises (or consists essentially of or consists of) methyl silicate 51 at a weight percent of greater than or equal to 15.28% and less than or equal to 19%, methanol at a weight percent of greater than or equal to 65.16% and less than or equal to 68.52%, water at a weight percent of greater than or equal to 15.68% and less than or equal to 16.04%, and ammonium hydroxide at a weight percent of greater than or equal to 0. 15% and less than or equal to 0.17%.
  • FIG. 1 illustrates a method 200A according to certain embodiments.
  • the method 200A comprises a step 205 of preparing a first solution by mixing a silicon alkoxide and a solvent, a step 210 of preparing a second solution by mixing a catalyst and water, a step 215 of mixing the first solution and the second solution together to form a precursor material, and a step 220 of allowing components of the precursor material to react to form silica wet gel.
  • step 205 comprises preparing a first solution by mixing methyl silicate 51 and methanol and step 210 comprises preparing a second solution by mixing ammonium hydroxide and water. Further, step 215 comprises mixing the first solution and the second solution together to form a precursor material having components within specific weight percentages.
  • the first solution comprises (or consists essentially of or consists of) methyl silicate 51 at a weight percent of greater than or equal to 15% and less than or equal to 30% and methanol at a weight percent of greater than or equal to 60% and less than or equal to 90%.
  • the second solution comprises (or consists essentially of or consists of) ammonium hydroxide at a weight percent of greater than or equal to 0.5% and less than or equal to 1.0% and water at a weight percent of greater than or equal to 99% and less than 100%.
  • the precursor material has a weight percent ratio of the methyl silicate 51 :water of between 0.25: 1 and 2: 1, such as between 0.5: 1 and 1 :1.
  • the precursor material is devoid of N,N-dimethylformamide. This can optionally be the case for the precursor material in any embodiment of the present disclosure.
  • FIG. 2 illustrates a method 200B according to certain embodiments.
  • the method 200B comprises steps 205 through 220 of making silica wet gel, as described elsewhere herein, a step 222 of aging the silica wet gel for a period of time, and a step 225 of drying the silica wet gel to form silica aerogel.
  • Applicant has developed methods that preserve dimensional stabilities of the silica wet gel during drying. This in turn leads to silica aerogel with superior optical, thermal and/or mechanical properties.
  • the aging step 222 includes keeping the silica wet gel in an airtight environment for a selected period of time.
  • the aging process allows structural transformation to occur in the three-dimensional particles polymeric structure of the silica wet gel that enhance the mechanical strength of the structure.
  • One exemplary significant structural transformation that takes place during aging is a decrease in spherical silica particle diameter.
  • Another exemplary structural transformation is a decrease in pore size. Pore size is a size of pore spaces between spherical silica particles. Pore sizes are often recorded in terms of average pore size.
  • Another exemplary structural transformation is a strengthening of the necking point between two spherical silica particles. The necking point is the point where two adjacent spherical silica particles adjoin.
  • the selected time period is a time period in which the aging process reaches saturation. Once saturation has occurred, no further structural transformation of the wet gel occur. Applicant has discovered that optimal properties are obtained when the selected time period is a time period of at least 7 days (168 hours), at least 8 days (192 hours), at least 9 days (216 hours) or at least 10 days (240 hours). Additionally, warping of the silica wet gel often takes place during subsequent processes. For example, in many cases, silica wet gel shrinks during drying. However, Applicant has found that a time period of at least 7 days helps prevent warping such as shrinking.
  • the silica wet gel is dried in step 225 using a conventional aerogel drying method.
  • the silica wet gel is placed in either a freeze dryer, a supercritical dryer, or an ambient dryer.
  • the step 225 of drying the silica wet gel comprises either a freeze-drying process, a supercritical drying process, or an ambient drying process.
  • the silica wet gel is dried using a supercritical drying method (also known as critical point drying).
  • supercritical drying involves a solvent exchange.
  • the silica wet gel is placed in a solvent bath so that water initially inside the silica wet gel is replaced with the solvent in the bath.
  • the silica wet gel is then placed in a pressure vessel along with liquid carbon dioxide.
  • the pressure vessel may be filled with, and emptied of, liquid carbon dioxide multiple times, so as to remove the organic solvent and leave liquid carbon dioxide in its place.
  • the liquid carbon dioxide is then heated past its critical temperature and pressure and removed, thereby leaving silica aerogel.
  • the silica wet gel can be placed in a methanol solvent bath for
  • the total time period in which the hydrophilic silica wet gel is in the solvent bath can be less than 20 hours, such as less than 17 hours. This is desirable as longer solvent processing time can lead to deterioration in optical properties. Additionally, a shorter solvent processing time is advantageous for commercial production.
  • the silica wet gel is dried using an ambient drying method.
  • ambient drying involves drying the flexible gel layer under ambient conditions (e.g., at a temperature in a range of from about 50 degrees to about 85 degrees Fahrenheit, and more typically in a range of from 68 degrees to 72 degrees Fahrenheit).
  • the liquid in the silica wet gel is allowed to slowly evaporate under controlled conditions, leaving silica aerogel.
  • the controlled conditions ensure that the evaporation is slow enough so that the silica network of the gel does not collapse during the drying.
  • the dryer is configured to establish a controlled environment in its interior. This may involve a controlled temperature, a controlled pressure, a controlled airflow, a controlled humidity, or any combination thereof.
  • the silica wet gel is dried using a freeze-drying method.
  • the silica wet gel is frozen and then put into a vacuum chamber.
  • the solvent is then removed to leave silica aerogel.
  • Any suitable freeze-drying technique known in the art may be used.
  • the silica wet gel can be placed into a household freezer, liquid nitrogen, or in a cryogenic mixture (e.g., a dry-ice/solvent mixture, such as a dry-ice and acetone bath).
  • the silica aerogel is provided in the form of a silica aerogel sheet. This is in contrast to aerogel in flowable granular or otherwise particulate form.
  • the aerogel sheet is preferably self-supporting, i.e., once fully synthesized and formed, the sheet can retain sheet form without being adhered to glass or another support. This can optionally be the case for any embodiment of the present disclosure involving a silica aerogel sheet.
  • Certain embodiments provide a method of making a silica aerogel sheet. FIG.
  • FIG. 3 illustrates a method 200C comprising steps 205 through 220 of making silica wet gel as described elsewhere herein, a step 230 of depositing the silica wet gel onto a mold tray to form a silica wet gel sheet, a step 232 of aging the silica wet gel sheet for a period of time, and a step 235 of drying the silica wet gel sheet to form a silica aerogel sheet.
  • the step 235 of drying the silica wet gel sheet can take place while the sheet is on the mold tray or after it is removed from the mold tray.
  • the silica aerogel sheet is an enhanced sheet having desirable and unexpected properties.
  • the silica aerogel sheet desirably has low haze.
  • the haze can optionally be less than 2.5%, such as less than 2%.
  • the silica aerogel sheet has a haze of less than or equal to 1 .75%. This preferably is the case for any embodiment involving a silica aerogel sheet.
  • Haze can be measured in well-known fashion, e.g., using a BYK HazeGard plus instrument. Reference is made to ASTM D 1003-00: Standard Test method for Haze and Luminous Transmittance of Transparent Plastics, the contents of which are incorporated herein by reference.
  • the silica aerogel sheet desirably has few to no optical distortion lines (“ODL ”)
  • ODL optical distortion lines
  • Applicant developed a method for assessing severity of ODL that involves calculating a global structural similarity index measure (“SSIM”) for a silica aerogel sheet sample.
  • SSIM global structural similarity index measure
  • the ODL is assessed in the following manner.
  • a silica aerogel sheet sample 500 is provided.
  • the sheet sample 500 has a size of 5x5 inches.
  • the silica aerogel sheet sample 500 is placed between a light source 510 and a projection screen 520.
  • the projection screen 520 is a flat matte white paper having a size of 15 inches by 15 inches.
  • the silica aerogel sheet sample 500 is placed at a distance DI of 12 inches from the light source 510 and at a distance D2 of 8 inches from the projection screen 520.
  • the sheet sample 500 and the projection screen 520 are parallel to each other, with the light source centered on a sightline axis passing through a center of the sheet sample 500.
  • the light source 510 is a full spectrum LED with eight individual white light bulbs replicating a daylight spectrum.
  • One suitable light source 510 is a fiber-coupled cold white LED (model number MCWHF2 k ) obtained from Thorlabs Inc. (a company having its headquarters in Newton, New Jersey, U.S.A.).
  • a projection 530 of the sample is provided on the projection screen 520. Any optical distortion shows up on the projection 530 as a shadow (i.e., a shadow projection).
  • a DSLR camera 540 is placed at a distance D3 of 14 inches from a center point of the projection screen 520, aimed at the distortion image 530, and at an angle of 70 degrees from a line perpendicular to the sightline axis.
  • One suitable DSLR camera 540 is a Canon Powershot SX540HS, 20.3 MegaPixel 1/2.3 in CMOS sensor with a 4.3 - 214 mm zoom lens obtained from Canon USA (a company having its headquarters in Melville, New York, U.S.A.).
  • the optical zoom on the camera 540 is adjusted to capture a window of an image of the shadow projection 530 at the highest resolution possible. This captured image is the distortion image. Note that because the camera 540 is at an angle to the projection screen 520, the shadow projection 530 is slightly trapezoidal (similar to the keystone effect in projectors). The distortion image therefore captures the largest rectangular window that can be cropped from the shadow projection 530.
  • the optical zoom on the camera 540 is adjusted to capture a window of an image of the projection screen 520 alone (i.e., without the shadow projection 530) at the highest resolution possible.
  • This captured image is the reference image.
  • the reference image captures the same size window that is captured for the distortion image.
  • a global SSIM is calculated by comparing the distortion image to a reference image.
  • the global SSIM is a measure of the total differences between the distortion image and the reference image.
  • the present invention uses the method described in Z. Wang, A. C. Bovik, H. R. Sheikh and E. P. Simoncelli, "Image quality assessment: From error visibility to structural similarity," IEEE Transactions on Image Processing, vol. 13, no. 4, pp. 600-612, Apr. 2004, the entire contents of which are incorporated herein by reference.
  • the global SSIM is calculated using the following formula:
  • the global SSIM can be calculated using a software program or index calculating code.
  • the global SSIM can be calculated using a Matlab implementation of the SSIM index disclosed at the entire contents of which are incorporated herein by reference.
  • the calculated global SSIM ranges from 0.00 to 1.00, with 0.00 showing the lowest structural similarity and 1.00 showing the highest structural similarity.
  • silica aerogel sheets produced from recipes described herein provide distortion images with a global SSIM of greater than 0.80.
  • sheets having a global SSIM of greater than 0.80 advantageously provide low ODL.
  • these particular recipes surprisingly do so without being substantially sensitive to the drying process or other downstream processes used to form the silica aerogel sheet.
  • the silica aerogel sheet has a calculated global SSIM of greater than 0.80. This can optionally be the case for any embodiment of the present disclosure involving a silica aerogel sheet.
  • the silica aerogel sheet can have a calculated global SSIM of greater than 0.82, greater than 0.85, greater than 0.87, greater than 0.90, greater than 0.91, greater than 0.92 or greater than 0.93.
  • the silica aerogel sheet is devoid of structural non-uniformities that create optical distortion lines visible to the naked eye.
  • the distortion image produced for such a silica aerogel sheet preferably is also devoid of optical distortion lines visible to the naked eye. This is preferably the case for any embodiment involving a silica aerogel sheet, optionally in combination with a visible transmission in the range noted in the next paragraph.
  • the silica aerogel sheet desirably has high visible transmission. In some cases, the silica aerogel sheet has a visible transmission of greater than 98%.
  • the term “visible transmission'’ is well known in the art and is used herein in accordance with its well-known meaning to refer to the percentage of all incident visible radiation that is transmitted through an object (e.g., through the aerogel sheet 300). Visible radiation constitutes the wavelength range of between about 380 nm and about 780 nm. Visible transmission, as well as visible reflection, can be determined in accordance with NFRC 300-2017, Standard Test Method for Determining the Solar and Infrared Optical Properties of Glazing Materials and Fading Resistance of Systems. The well-known and commercially available LBNL WINDOW 7.4 computer program can be used in calculating these and other reported optical properties.
  • the silica aerogel sheet can also have desirable transmitted color characterized by “a” and “b” color coordinates that are each between -2 and 2. This can optionally be the case for any embodiment of the present disclosure involving a silica aerogel sheet, preferably in combination with visible transmission and haze levels in the ranges noted above.
  • the present discussion of color properties is reported using the w ell-know n color coordinates of “a” and “b.” In more detail, the color coordinates are indicated herein using the subscript h (i.e., a and b ) to represent the conventional use of the well-known Hunter Lab Color System (Hunter methods/units, Ill. D65, 10 degree observer).
  • the present color properties can be calculated as specified in “Insight on Color,” “Hunter L, a, b Color Scale,” Applications Note, Vol. 8, No. 9, 06/08 (2008), the relevant teachings of which are incorporated herein by reference.
  • the silica aerogel sheet can have a low bulk density.
  • the silica aerogel sheet has a bulk density of less than 150 mg/cc.
  • the silica aerogel sheet has a bulk density of less than 140 mg/cc, such as less than 130 mg/cc, or even less than 125 mg/cc.
  • the silica aerogel sheet has a bulk density of higher than 70 mg/cc.
  • the silica aerogel sheet has a bulk density of higher than 80 mg/cc, such as higher than 85 mg/cc, or even higher than 95 mg/cc.
  • the silica aerogel sheet has a bulk density of between 100 mg/cc and 150 mg/cc, such as 120 mg/cc.
  • the density of the silica aerogel sheet can optionally be in this range for any embodiment of the present disclosure, preferably in combination with visible transmission and haze levels in the ranges noted above (e.g., Tvis greater than 98% together with haze of less than 2.5%, less than 2%, or less than 1.75%).
  • Bulk density is calculated by weighing the aerogel sheet and then calculating the volume using the weight along with the dimensions of the aerogel sheet.
  • the silica aerogel sheet can also have low thermal conductivity.
  • the silica aerogel sheet can have a thermal conductivity of less 20 mW/m*K, such as less than 13 mW/m*K in air (or less than 10 mW/m*K in inert gas such as argon).
  • the thermal conductivity of the silica aerogel sheet can optionally be in one or both of these ranges for any embodiment of the present disclosure. Thermal conductivity can be determined using a conventional heat flow meter, such as the well-known TA Instruments Fox 200 heat flow meter, which is commercially available from Waters Corporation (New Castle, Delaware, U.S.A.).
  • the silica aerogel sample can have a flexural modulus of less than 750 kPa and perhaps less than or equal to 720 kPa, 700 kPa, 680kPa or 650 kPa.
  • the flexural modulus of a material is a mechanical property that measures a material’s stiffness or resistance to bending and is defined as the ratio of stress to strain in flexural deformation. It is determined from the slope of a stress-strain curve produced by a flexural test on an aerogel sample having dimensions of 74.5mm in length, 14.5 mm in width and 3.2 mm in thickness.
  • the flexural test is performed in accordance with ASTM D790: Standard Test Methods for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Material, the contents of which are incorporated herein by reference.
  • ASTM D790 Standard Test Methods for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Material, the contents of which are incorporated herein by reference.
  • the silica aerogel sheet can have an average pore size of less than 30 nm, such as less than or equal to 26 nm. This can optionally be the case for any embodiment of the present disclosure that involves the silica aerogel sheet.
  • the average pore size can be determined using a Quantachrome “autosorb-iQ” gas absorption analyzer, which is commercially available from Anton Paar (Graz, Austria) along with calculating average pore size using density functional theory (DFT) calculations.
  • DFT density functional theory
  • the silica aerogel sheet can also have a specific surface area of at least 800 m 2 /g, such as greater than or equal to 850 m 2 /g or perhaps greater than or equal to 900 m 2 /g.
  • a specific surface area can also be determined using a Quantachrome “autosorb-iQ” gas absorption analyzer, which is commercially available from Anton Paar (Graz, Austria) along with calculating specific surface area using density functional theory (DFT) calculations.
  • the silica aerogel sheet can also have a linear shrinkage (X/Y direction) of less than 3%, such as less than 2.7%, less than 2.5%, less than 2% or perhaps less than 1.75%.
  • Linear shrinkage can be determined by taking an image of a silica wet gel sample before drying and an image of the silica aerogel sample after drying. The images can be taken with a regular camera with a known scale. The images can be analyzed with image J software and the final length of the silica aerogel can be determined with respect to the known initial length before drying.
  • the silica aerogel sheet can also have less than 3% solvent remaining after drying, such as less than 2.5%, less than 2% or less that 1.75%.
  • the silica aerogel sample can also have a maximum strain at complete breaking point of at least 2.5%, such as at least 3%, at least 3.1% or perhaps at least 3.2%.
  • Maximum strain % at complete breaking point is the highest deformation value obtained from the x-axis of a stress-strain (s-s) curve for an aerogel sample.
  • the flexural stress-strain (s-s) curve is produced by a flexural test performed in accordance with ASTM D790: Standard Test Methods for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Material, the contents of which are incorporated herein by reference.
  • the silica aerogel sample can have a maximum resilience at complete breaking point of greater than 400 J/m 3 , such as 425 J/m 3 .
  • Maximum resilience is determined by calculating a maximum area under the flexural stress-strain (s-s) curve for the aerogel sample.
  • Exemplary silica aerogel sheets were prepared as outlined below. Additionally, comparative exemplary silica aerogel sheets were attempted. Properties for silica aerogel sheets obtained were also measured using methods described herein and tabulated in Tables 1-3.
  • Example #1 was prepared according to the following steps:
  • A Preparing a first solution by mixing 5.5 mL MS-51 and 37.0 mL methanol.
  • the first solution included MS-51 at a weight percent of 18.2% and methanol at a weight percent of 81.8%.
  • the mixed solution included MS-51 at a weight percent of 15.28%, methanol at a weight percent of 68.52%, water at a weight percent of 16.04% and ammonium hydroxide at a weight percent of 0.16%.
  • the mixed solution had a MS-51 : water weight ratio of 0.95: 1.
  • Example #2 was prepared according to the following steps:
  • A Preparing a first solution by mixing 6.2 mL MS-51 and 36.5 mL methanol.
  • the first solution included MS-51 at a weight percent of 20.3% and methanol at a weight percent of 79.7%.
  • Example #3 was prepared according to the following steps: A. Preparing a first solution by mixing 7.0 mL MS-51 and 36.0 mL methanol. The first solution included MS-51 at a weight percent of 22.6% and methanol at a weight percent of 77.4%.
  • the mixed solution included MS-51 at a weight percent of 19.00%, methanol at a weight percent of 65.16%, water at a weight percent of 15.68% and ammonium hydroxide at a weight percent of 0.16%.
  • the mixed solution had a MS-51 : water weight ratio of 1.2: 1.
  • Steps D through J were repeated as performed in Example #1 .
  • Properties for the resulting silica aerogel sheet are shown in Table 2.
  • Example #4 ten silica aerogel sheet samples were prepared according to steps of Example #3. Properties obtained for the resulting silica aerogel sheets are shown in Table 3. Further, haze versus shrinkage properties are shown in FIG. 13, haze versus solvent remaining properties are shown in FIG. 14 and stress versus strain properties are shown in FIG. 15.
  • Comparative Example #1 was prepared according to the following steps:
  • TMOS Preparing a first solution by mixing 6.4 mL TMOS and 37.0 mL methanol.
  • the first solution included TMOS at a weight percent of 18.3% and methanol at a weight percent of 81.8%.
  • Example #1 Mixing the first solution and second solution together to form a mixed solution.
  • the mixed solution included TMOS at a weight percent of 15.28%, methanol at a weight percent of 68.52%, water at a weight percent of 16.04% and ammonium hydroxide at a weight percent of 0. 16%.
  • Steps D and E were repeated as performed in Example #1.
  • the mixed solution in Comparative Example #1 did not form a silica wet gel. As such, a silica aerogel sheet was not obtained.
  • Comparative Example #2 was prepared according to the following steps:
  • A Preparing a first solution by mixing 6.9 mL MTMS and 37.0 mL methanol.
  • the first solution included MTMS at a weight percent of 18.3% and methanol at a weight percent of 81.8%.
  • the mixed solution included MTMS at a weight percent of 15.28%, methanol at a weight percent of 68.52%, water at a weight percent of 16.04% and ammonium hydroxide at a weight percent of 0.16%.
  • Steps D and E were repeated as performed in Example #1.
  • the mixed solution in Comparative Example #2 also did not form a silica wet gel, and thus a silica aerogel sheet was not obtained.
  • Comparative Example #3 was prepared according to the following steps:
  • A Preparing a first solution by mixing 7.0 mL TEOS and 37.0 mL methanol.
  • the first solution included TEOS at a weight percent of 18.3% and methanol at a weight percent of 81.8%.
  • Example C Mixing the first solution and second solution together to form a mixed solution.
  • the mixed solution included TEOS at a weight percent of 15.28%, methanol at a weight percent of 68.52%, water at a weight percent of 16.04% and ammonium hydroxide at a weight percent of 0.16%.
  • Steps D and E were repeated as performed in Example #1.
  • the mixed solution in Comparative Example #3 also did not form a silica wet gel, and thus a silica aerogel sheet was not obtained.
  • Comparative Example #4 was prepared according to the following steps:
  • A Preparing a first solution by mixing 9.9 mL MS-51 and 37.3 mL methanol.
  • the first solution included MS-51 at a weight percent of 28.5% and methanol at a weight percent of 71.5%.
  • the mixed solution included MS-51 at a weight percent of 26%, methanol at a weight percent of 66.70%, water at a weight percent of 7.2% and ammonium hydroxide at a weight percent of 0.16%.
  • the mixed solution had a MS-51: water weight ratio of 3.6: 1.
  • Comparative Example #5 was prepared according to the following steps:
  • A Preparing a first solution by mixing 2.3 mL MS-51 and 38.0 mL methanol.
  • the first solution included MS-51 at a weight percent of 8.2% and methanol at a weight percent of 91.8%.
  • the mixed solution included MS-51 at a weight percent of 6.1%, methanol at a weight percent of 69.1%, water at a weight percent of 25% and ammonium hydroxide at a weight percent of 0.16%.
  • the mixed solution also included a MS-51: water weight ratio of 0.2: 1. Steps D through J were repeated as performed in Example # 1.
  • the mixed solution in Comparative Example #5 also did not form a silica wet gel, and thus a silica aerogel sheet was not obtained.
  • Table 1 [0087] As shown in Table 1, optimal results were obtained with the recipe of Example 1 when using a precursor material having methyl silicate 51 as the silicon alkoxide. When TMOS, MTMS and TEOS were used, silica wet gels were not obtained.
  • FIG. 13 shows that use of methanol yields silica aerogel sheets having a linear shrinkage of less than 3% and a haze of less than 1.5%.
  • FIG. 13 also shows that use of ethanol or IPA yields silica aerogel sheets having a greater linear shrinkage and greater haze percentage than when methanol is used.
  • FIG. 13 also confirms that a lower linear shrinkage percentage correlates to a lower haze percentage in the resulting aerogel sheets.
  • FIG. 14 shows that use of methanol as the solvent in the solvent exchange yields silica aerogel sheets having a solvent remaining weight percentage of less than 3% and a haze of less than 1.5%.
  • FIG. 14 shows that use of ethanol or IPA as a solvent yields silica aerogel having a greater solvent remaining weight percentage and a greater haze percentage than when methanol is used.
  • FIG. 14 also confirms that a lower solvent remaining weight percentage correlates to a lower haze percentage in the resulting aerogel.
  • FIG. 15 shows that use of methanol as the solvent in the solvent exchange yields a silica aerogel sample having a complete breaking point at a 3.24% strain.
  • FIG. 15 shows that use of ethanol or IPA as the solvent yields silica aerogel samples having a complete breaking point at a lower % strain.
  • the silica aerogel sample obtained using methanol had better resilience than samples obtained using ethanol or IPA.
  • one group of embodiments involves a precursor material having a weight percent ratio of the methyl silicate 51 :water in the range of between 0.25: 1 and 2: 1, and where the resulting silica aerogel sheet having a visible transmission of greater than or equal to 98% and a haze of less than or equal to 1.5%.
  • This can optionally be in combination with the resulting silica aerogel sheet having a density in a range of from about 100 mg/cc to about 200 mg/cc.
  • FIG. 4 illustrates an article 10 comprising a glass sheet 12 and a silica aerogel sheet 300.
  • the silica aerogel sheet 300 is adhered to or otherwise carried or mounted alongside the glass sheet 12.
  • the silica aerogel sheet 300 can have any of the features and properties discussed elsewhere herein.
  • the silica aerogel sheet 300 preferably is adhered to a surface 14 of the glass sheet 12.
  • the aerogel sheet 300 is “adhered to” a surface of a glass sheet, this does not require a separate adhesive, though an adhesive can optionally be used. It also does not require the aerogel to contact the glass; there may be a coating or layer therebetween.
  • the aerogel is supported by the glass surface, and in some preferred embodiments the aerogel does contact the glass surface.
  • a variety of known glass types can be used for the glass sheet 12, including soda-lime glass, borosilicate glass or aluminosilicate glass. In some cases, it may be desirable to use “white glass,” a low iron glass, etc. For some applications, it may be desirable to use tinted glass for the glass sheet 12. Moreover, there may be applications where the glass sheet 12 is formed of extremely thin, flexible glass, such as glass sold under the trademark Willow glass by Coming Inc. (Coming, New York, U.S.A.). If desired, the glass sheet 12 may be formed of a chemically strengthened glass, such as glass sold under the trademark Gorilla glass by Coming Inc. In certain embodiments, the glass sheet is part of a window, door, skylight, or other glazing.
  • the glass sheet 12 is replaced with a sheet formed of a polymer, such as polycarbonate, acrylic, or PVC.
  • a polymer such as polycarbonate, acrylic, or PVC.
  • Various other polymer materials e.g., transparent polymers
  • Glass sheets of various sizes can be used. Commonly, large-area glass sheets are used.
  • the glass sheet 12 can have a major dimension (e.g., a length or width) of at least about 0.1 meter, preferably at least about 0.5 meter, more preferably at least about 1 meter, perhaps more preferably at least about 1.5 meters (e.g., between about 2 meters and about 4 meters), and in some cases at least about 3 meters.
  • the glass sheet 12 is ajumbo glass sheet having a length and/or width that is between about 3 meters and about 10 meters, e.g., a glass sheet 12 having a width of about 3.5 meters and a length of about 6.5 meters.
  • the glass sheet 12 can have a thickness of about 1 -8 mm. In some cases, the glass sheet 12 has a thickness of between about 2.3 mm and about 4.8 mm, and perhaps more preferably between about 2.5 mm and about 4.8 mm. In one particular embodiment, the glass sheet 12 has a thickness of about 3 mm.
  • FIGs. 5-6 illustrate a method 200D wherein the silica wet gel is first deposited onto and then dried in a mold tray.
  • the method 200D comprises steps 205 through 235 of forming a silica aerogel sheet as described elsewhere herein, a step 240 of removing the silica aerogel sheet from the mold tray, and a step 245 of adhering the silica aerogel sheet to a glass sheet to form the article.
  • FIG. 6 illustrates the method 200D of forming a silica aerogel sheet using a mold tray 600.
  • the mold tray 600 has a base 605 and a plurality of sidewalls 610.
  • silica wet gel 99 is poured into the mold tray 600.
  • the silica wet gel 99 is dried using a conventional drying method described herein to form a silica aerogel sheet 300 having a size and dimension defined by the mold tray 600.
  • the dried silica aerogel sheet 300 is removed from the mold tray 600.
  • the silica wet gel 99 is removed from the mold tray 600 before using a conventional drying method.
  • the step 245 comprises placing the silica aerogel sheet in contact with the glass sheet, and the silica aerogel sheet adheres to the glass sheet through van der Waals forces.
  • the step 245 comprises adhering the silica aerogel sheet to a glass sheet by an optical adhesive, optionally such that portions of the silica aerogel sheet are devoid of the optical adhesive.
  • the optical adhesive can optionally be located only at a perimeter of the silica aerogel sheet.
  • FIG. 7 illustrates the method 200E of forming a silica aerogel sheet directly onto a substrate using a sidewall mold.
  • the method 200E comprises steps 205 through 220 of forming silica wet gel as described elsewhere herein, a step 250 of depositing the silica wet gel directly onto a glass sheet that includes a sidewall mold, a step 255 of drying the silica wet gel to form a silica aerogel sheet, and a step 260 of removing the sidewall mold from the glass sheet, leaving the silica aerogel sheet adhered to the glass sheet.
  • the aerogel fabrication method can include various techniques, such as method 200D shown in FIG. 5 and described with reference thereto, or method 200E as shown in FIG. 7 and described with reference thereto. Another option is to use a rapid supercritical extraction technique.
  • U.S. Patent No. 8,080,591 the salient teachings of which are incorporated herein by reference.
  • FIG. 9 illustrates an insulating glazing unit 40 according to certain embodiments comprising a first glass sheet 100, a second glass sheet 110 and a between-pane space 50.
  • the between-pane space 50 is located between the two glass sheets.
  • the glass sheets 100, 110 can have any of the features described for a glass sheet elsewhere herein.
  • one or both glass sheets 100, 110 are replaced with sheets formed of a polymer, such as polycarbonate, acrylic or PVC.
  • Various other polymer materials may be used in such alternative embodiments.
  • the insulating glazing unit further comprises a silica aerogel sheet 300 within the between-pane space 50.
  • the silica aerogel sheet 300 can have any of the features and properties described elsewhere herein.
  • the silica aerogel sheet 300 is a single aerogel sheet. In such cases, there is only one silica aerogel sheet 300 in the between-pane space 50.
  • the single aerogel sheet 300 can, for example, have a major dimension (e.g., a length or width) of at least 0.375 meter, preferably at least about 0.75 meter, or in some cases at least about 1.125 meters (e.g., between about 1.5 meters and about 3 meters).
  • the silica aerogel sheet 300 comprises plurality of silica aerogel sheets. In such cases, there are a plurality of silica aerogel sheets in the between-pane space 50. A plurality of aerogel sheets may thus collectively define the silica aerogel sheet 300.
  • multiple aerogel sheets When multiple aerogel sheets are used, they can be arranged in a tiled configuration between the two glass panes 100, 110. When a tiled configuration is used, multiple aerogel sheets preferably are arranged in a non-overlapping manner so as to cover a majority (i.e., greater than 50%, preferably at least 75%) of the area of an adjacent interior glass surface 120, 130.
  • the silica aerogel sheet 300 is formed by one or multiple aerogel sheets, it preferably covers more than 60% (e.g., more than 70%, more than 80%, or even more than 90%) of an adjacent interior glass surface 120, 130. A coverage within any one or more (e.g., all) of these ranges can optionally be used in any embodiment of the present disclosure.
  • the silica aerogel sheet 300 consists of a single aerogel sheet. This can optionally be the case for any embodiment of the present disclosure involving a silica aerogel sheet.
  • the silica aerogel sheet 300 comprises a plurality of aerogel sheets
  • those sheets can have any desired shape and tiling arrangement.
  • the aerogel sheets can be square, rectangular, or hexagonal in shape.
  • edges of each aerogel sheet are aligned both vertically and horizontally with edges of adjacent aerogel sheets.
  • the size of the silica aerogel sheets is not particularly limited. In some cases, all of the silica aerogel sheets have the same dimensions. In other cases, some of the silica aerogel sheets have different dimensions (e.g., a greater length) compared to some of the other silica aerogel sheets.
  • each of the silica aerogel sheets has a length and a width of at least 10 cm. For each of the silica aerogel sheets, the length, the width, or both are preferably less than 1 meter.
  • silica aerogel sheets Such dimensions allow the silica aerogel sheets to be scaled-up so as to cover large areas between two glass sheets of an insulating glazing unit, while still allowing the silica aerogel sheets to be dried using a small high-pressure vessel. Larger or smaller silica aerogel sheets may alternatively be used.
  • the between-pane space 50 contains a gaseous atmosphere, preferably comprising a thermally insulative gas, such as argon, kry pton, or both.
  • a gaseous atmosphere preferably comprising a thermally insulative gas, such as argon, kry pton, or both.
  • the gaseous atmosphere comprises a mix of argon and air (e.g., 90% argon and 10% air).
  • the gaseous atmosphere comprises a mix of krypton and air.
  • the gaseous atmosphere comprises a mix of argon, krypton, and air.
  • the gaseous atmosphere is just air.
  • a gas gap G is provided in the between-pane space 50 alongside the silica aerogel sheet 300.
  • the gas gap G can have a width in a range of from 9 to 14 mm and it contains a gaseous atmosphere comprising argon, air, or both.
  • between-pane space has a width W in a range of from 14 to 21 mm, the gaseous atmosphere comprises argon, and the width of the gas gap G is from 10.5 to 13.5 mm.
  • the spacer 60 may be a conventional metal channel spacer, e.g., formed of stainless steel or aluminum. Or it can comprise polymer and metal, or just polymer (e.g., foam). The spacer can alternatively be an integral part of a sash, frame, etc. so as to maintain the IG unit in the desired configuration.
  • the spacer 60 can be adhered to the two glass sheets 100, 110 by one or more beads of sealant as is conventional and well-known to skilled artisans.
  • the spacer 60 is shown with a primary sealant 55 on opposite sides of the spacer 60 and a secondary sealant 58 provided on an outside wall of the spacer 60.
  • Another option is to omit the secondary sealant and provide a single deposit of sealant along both sides of the spacer and on the outside wall of the spacer.
  • Various other known sealant arrangements/sy stems can alternatively be used.
  • the spacer may be omitted while one or more beads of sealant (optionally together with a moisture vapor barrier) are provided about the perimeter of the unit so as to encompass the silica aerogel sheet 300.
  • the silica aerogel sheet 300 does not contact the spacer 60.
  • the aerogel sheet 300 may be separated (i. e. , spaced-apart) from the spacer 60 by about 1 mm to about 5 mm (e.g., about 2-4 mm, such as about 3 nun).
  • the sealant 55, 58 between the spacer 60 and the two adjacent glass sheets 100, 110 can also be spaced from the silica aerogel sheet 300.
  • the first glass sheet 100 has opposed surfaces 120, 125, which preferably are opposed major surfaces (or “opposed faces”).
  • the second glass sheet 110 has opposed surfaces 130, 135, which preferably are opposed major surfaces.
  • surfaces 120 and 130 are interior surfaces facing a between-pane space 50
  • surfaces 125 and 135 are exterior surfaces, e.g., such that surface 135 is an exterior surface exposed to an outdoor environment (and thus exposed to periodic contact with rain). This, however, is not required.
  • the second glass sheet 110 is an outboard pane that defines both a #1 surface (i.e., surface 135) and a #2 surface (i.e., surface 130), while the first glass sheet 100 is an inboard pane that defines both a #3 surface (i.e., surface 120) and a #4 surface (i.e., surface 125).
  • the IG unit 40 can optionally be mounted in a frame such that the #1 surface is exposed to an outdoor environment, while the #4 surface is exposed to an indoor environment (e.g., an environment inside a building).
  • the silica aerogel sheet 300 can be adhered to or otherwise mounted alongside either the #2 surface or the #3 surface of the insulating glazing unit 40. Another option is to have aerogel sheets on both the #2 and the #3 surfaces.
  • FIG. 9 illustrates just one embodiment where the silica aerogel sheet 300 is adhered to an interior surface 120 (e.g., the #3 surface) of the first glass sheet 100.
  • FIG. 9 shows a double-pane insulating glazing unit
  • other embodiments provide a triple-pane insulating glazing unit having a silica aerogel sheet 300 on the #2 surface, the #3 surface, the #4 surface, or the #5 surface.
  • silica aerogel sheets can optionally be provided on both the #3 surface and either the #4 or #5 surface.
  • Another option is to provide silica aerogel sheets on both the #2 surface (e.g., for applications where a low-emissivity or solar control coating is on the #3 surface) and the #4 or #5 surface.
  • the insulating glazing unit 40 includes only two glass panes 100, 110 and only one between-pane space 50.
  • the between-pane space 50 has a thickness W, which is measured from the interior surface 130 of the second glass pane 110 to the interior surface 120 of the first glass pane 100.
  • the silica aerogel sheet 300 does not occupy the entire thickness W of the between-pane space 50. In other cases, the silica aerogel sheet occupies the entire thickness of the between-pane space.
  • a ratio of the thickness T of the silica aerogel sheet 300 to the thickness W of the between-pane space 50 preferably is between 0.15 and 0.85.
  • the thickness W of the between-pane space 50 is at least 10 mm, optionally together with the thickness of the silica aerogel sheets 300 being greater than 2 mm but less than 8 mm.
  • the aerogel sheet 300 occupies less than 50% of the thickness W of the between-pane space 50 (e.g., less than 45%, less than 40%, or even less than 35% of the thickness W of the between-pane space 50).
  • the silica aerogel sheet 300 occupies a majority of the thickness W of the between-pane space 50.
  • the thickness T of the silica aerogel sheet 300 preferably is greater than 8 mm but less than 15 mm (e.g., about 10 mm), while the thickness of the gas gap G alongside the silica aerogel sheet 300 is optionally less than 5 mm (e.g., about 3 mm).
  • an insulating glazing unit 40 that includes both a silica aerogel sheet 300 and a low-emissivity coating 70.
  • the silica aerogel sheet 300 is provided on an interior surface of one glass sheet and the lo -emissivity coating 70 is provided on an interior surface of the other glass sheet.
  • FIG. 9 illustrates an embodiment that includes a silica aerogel sheet 300 on a #3 surface (i.e., surface 120) and an optional low- emissivity coating 70 on a #2 surface (i.e., surface 130).
  • a silica aerogel sheet is provided on a #2 surface (i.e., surface 130) and an optional low-emissivity coating is provided on a #3 surface (i.e., surface 120).
  • the optional low-emissivity coating 70 preferably includes at least one silver-inclusive fdm, which desirably contains more than 50% silver by weight (e.g., a metallic silver film).
  • the low-emissivity coating 70 includes three or more infrared-reflective films (e.g., silver-containing films). Low-emissivity coatings having three or more infrared-reflective films are described in U.S. Patent and Application Nos. 11/546,152 and 7,572,511 and 7,572,510 and 7,572,509 and 11/545,211 and 7,342,716 and 7,339,728, the teachings of each of which are incorporated herein by reference.
  • the low-emissivity coating 70 includes four silver layers.
  • the low-emissivity coating can be a “single silver” or “double silver” low-emissivity coating, which are well-known to skilled artisans.
  • Advantageous coatings of this nature are commercially available from, for example, Cardinal CG Company (Eden Prairie, Minnesota, U.S.A.).
  • an insulating glazing unit 40 that includes both a silica aerogel sheet 300 and an optional transparent conductive oxide coating 85.
  • the silica aerogel sheet 300 is provided on an interior surface of a glass sheet and a transparent conductive oxide coating 85 is provided on an exterior surface of a glass sheet.
  • FIG. 9 illustrates an embodiment where the silica aerogel sheet 300 is provided on a #3 surface (i.e., surface 120) and an optional transparent conductive oxide coating 85 is provided on a #4 surface (i.e., surface 125).
  • the optional transparent conductive oxide coating 85 can include indium tin oxide.
  • zinc aluminum oxide, SnO:Sb, sputtered SnO:F, or another known transparent conductive oxide is used.
  • transparent conductive oxide coating 85 comprises tin oxide together with antimony, fluorine, or another dopant.
  • the transparent conductive oxide coating 85 is a sputtered film.
  • the transparent conductive oxide coating 85 comprises a pyrolytic film that includes tin (e.g., comprising tin oxide together with antimony, fluorine, or another dopant).
  • the transparent conductive oxide coating 85 includes carbon nanotubes.
  • the transparent conductive oxide coating 85 is provided at a thickness of 10,000 A or less, such as between about 1,000 A and about 7,000 A, e.g., from 1,000 A to 1,750 A, such as about 1,300-1,600 A.
  • the transparent conductive oxide coating 85 it can optionally comprise a transparent conductive oxide film having a thickness of from 1,000 A to 1,750 A.
  • the transparent conductive oxide coating 85 can, for example, be a coating of the type described in any of U.S. Patent or Patent Application Nos. 9,862,640 or 10,000,965 or 10,000,411 or 16/740,006, the teachings of which concerning the transparent conductive oxide coating are hereby incorporated herein by reference. In the embodiment of FIG. 9, the illustrated transparent conductive oxide coating 85 can optionally be omitted.
  • the insulating glazing unit 40 includes both a transparent conductive oxide coating 85 and a low-emissivity coating 70. This, however, is not required in all embodiments.
  • the insulating glazing unit 40 includes the low- emissivity coating 70 but is devoid of the transparent conductive oxide coating 85.
  • FIG. 5 Other embodiments provide a method of making an insulating glazing unit.
  • the method can include either method 200D shown in FIG. 5 or method 200E as shown in FIG. 7 of making a glass sheet bearing a silica aerogel sheet.
  • the method further comprises an additional step of assembling the silica aerogel sheet together with the first and second glass sheets 100, 110 in forming the insulating glazing unit.
  • Exemplary IG unit assembly methods are described in U.S. Patent Application No. 63/480,715, the contents of which are incorporated herein by reference. More generally, the silica aerogel sheet 300 and the first and second glass sheets 100, 110 glass can be assembled as part of an insulating glazing unit using any suitable techniques.
  • the step of assembling the silica aerogel sheet as part of an insulating glazing unit can include a step of adhering the silica aerogel sheet to a surface of a glass sheet (e.g., through van der Waals forces, or by using an optical adhesive).
  • the silica aerogel sheet may be placed either manually or, more preferably, with robotics.
  • the silica aerogel sheet is adhered to a temporary surface for handling and placement.
  • the silica aerogel sheet can be picked up using electrostatic adhesion, e.g., using commercially available Stackit robots manufactured by Grabit, Inc. (Sunnyvale, California, U.S.A.) or using technology described in U.S. Patent Application No. 63/387,442, the contents of which are incorporated herein by reference.
  • FIG. 10 illustrates a laminated glass assembly 80 comprising a first glass sheet 100, a second glass sheet 110 and a silica aerogel sheet 300.
  • the laminated glass assembly 80 also includes a spacer.
  • the spacer is omitted and the laminated glass assembly 80 just has one or more beads of sealant 58 (optionally together with a foil moisture barrier, tape, or both) at the perimeter of the assembly.
  • the silica aerogel sheet 300 can have any of the features and properties discussed elsew here herein. Likewise, the silica aerogel sheet 300 of the laminated glass assembly 80 can have the same dimensions and material properties as the silica aerogel sheet 300 described elsewhere herein for the insulating glazing unit 40.
  • the laminated glass assembly 80 can also include a polymer interlayer 400.
  • the polymer interlayer 400 preferably is a tear-resistant polymer layer. In some cases, it is a sheet of ionoplast plastic. In other cases, it is a sheet of polyvinyl butyral (PVB).
  • PVB polyvinyl butyral
  • both glass sheets 100, 110 can be clear 3 mm soda-lime float glass and the polymer interlayer 400 can be 0.30-inch thick PVB. It is to be appreciated, however, that these details are by no means limiting.
  • FIG. 10 shows an embodiment having a single polymer interlayer 400.
  • the silica aerogel sheet 300 can be adhered directly to one of the two glass sheets 100, 110 (e.g., through van der Waals forces, or by using an optical adhesive).
  • the silica aerogel sheet is sandwiched between, and laminated to, the two polymer interlayers.
  • the polymer interlayers are each in contact with one of the glass sheets on opposite sides of the silica aerogel sheet.
  • the polymer interlay er(s) are omitted, and the silica aerogel sheet replaces the interlay er(s).
  • the method can include either method 200D show n in FIG. 5 or method 200E as shown in FIG. 7 of making a glass sheet bearing a silica aerogel sheet.
  • the method further comprises an additional step of assembling the silica aerogel sheet 300 together with the first and second glass sheets 100, 110 in forming the laminated glass assembly.
  • the silica aerogel sheet 300 and the two glass sheets 100, 110 can then be assembled together in forming the laminated glass assembly using suitable techniques.
  • the step of assembling the silica aerogel sheet as part of a laminated glass assembly can include a step of adhering the silica aerogel sheet to a surface of a glass sheet (e.g., through van der Waals forces, or by using an optical adhesive) as described elsewhere herein.
  • the silica aerogel sheet and glass sheet can then be assembled as part of a laminated glass assembly, using any suitable techniques.
  • the assembly process includes one or more steps described in U.S. Patent Nos. 7,117,914 and 7,143,800, the teachings of which are hereby incorporated herein by reference.

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  • Chemical & Material Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Silicon Compounds (AREA)

Abstract

L'invention concerne un gel de silice humide, un aérogel de silice et des procédés qui peuvent être utilisés pour former une feuille d'aérogel de silice améliorée ayant moins de défauts optiques conjointement avec d'autres propriétés souhaitables.
EP23783645.7A 2023-03-09 2023-09-07 Gel de silice humide et aérogel Pending EP4676882A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US18/181,342 US20230286810A1 (en) 2022-03-09 2023-03-09 Silica wet gel and aerogel
PCT/US2023/073649 WO2024186358A1 (fr) 2023-03-09 2023-09-07 Gel de silice humide et aérogel

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Publication Number Publication Date
EP4676882A1 true EP4676882A1 (fr) 2026-01-14

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WO (1) WO2024186358A1 (fr)

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US20260084972A1 (en) * 2024-09-20 2026-03-26 AeroShield Materials, Inc. Systems, articles, and methods related to transparent insulation materials including aerogels

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US7117914B2 (en) 2003-03-20 2006-10-10 Cardinal Lg Company Non-autoclave laminated glass
US7143800B2 (en) 2003-03-20 2006-12-05 Cardinal Lg Company Non-autoclave laminated glass
US7384988B2 (en) 2003-08-26 2008-06-10 Union College Method and device for fabricating aerogels and aerogel monoliths obtained thereby
JP2005132641A (ja) * 2003-10-28 2005-05-26 Matsushita Electric Works Ltd シリカエアロゲルの製造方法
US7342716B2 (en) 2005-10-11 2008-03-11 Cardinal Cg Company Multiple cavity low-emissivity coatings
US7572511B2 (en) 2005-10-11 2009-08-11 Cardinal Cg Company High infrared reflection coatings
US7339728B2 (en) 2005-10-11 2008-03-04 Cardinal Cg Company Low-emissivity coatings having high visible transmission and low solar heat gain coefficient
US10000411B2 (en) 2010-01-16 2018-06-19 Cardinal Cg Company Insulating glass unit transparent conductivity and low emissivity coating technology
US10000965B2 (en) 2010-01-16 2018-06-19 Cardinal Cg Company Insulating glass unit transparent conductive coating technology
US9862640B2 (en) 2010-01-16 2018-01-09 Cardinal Cg Company Tin oxide overcoat indium tin oxide coatings, coated glazings, and production methods

Also Published As

Publication number Publication date
WO2024186358A1 (fr) 2024-09-12

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