WO2013134159A2 - Sapphire laminates - Google Patents

Sapphire laminates Download PDF

Info

Publication number
WO2013134159A2
WO2013134159A2 PCT/US2013/028938 US2013028938W WO2013134159A2 WO 2013134159 A2 WO2013134159 A2 WO 2013134159A2 US 2013028938 W US2013028938 W US 2013028938W WO 2013134159 A2 WO2013134159 A2 WO 2013134159A2
Authority
WO
WIPO (PCT)
Prior art keywords
sapphire
sheet
plane
glass
sheets
Prior art date
Application number
PCT/US2013/028938
Other languages
French (fr)
Other versions
WO2013134159A3 (en
Inventor
Christopher D. Prest
Dale N MEMERING
David A. Pakula
Richard Hung Minh Dinh
Vincent Yan
Original Assignee
Apple Inc.
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
Application filed by Apple Inc. filed Critical Apple Inc.
Priority to KR1020147024390A priority Critical patent/KR20140129072A/en
Priority to CN201380011629.XA priority patent/CN104159738B/en
Priority to KR1020167025331A priority patent/KR101930606B1/en
Priority to JP2014560135A priority patent/JP6095132B2/en
Priority to EP13711768.5A priority patent/EP2822760A2/en
Publication of WO2013134159A2 publication Critical patent/WO2013134159A2/en
Publication of WO2013134159A3 publication Critical patent/WO2013134159A3/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B17/00Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/06Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
    • B32B17/10Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C27/00Joining pieces of glass to pieces of other inorganic material; Joining glass to glass other than by fusing
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/10Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
    • C04B35/111Fine ceramics
    • C04B35/115Translucent or transparent products
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B37/00Joining burned ceramic articles with other burned ceramic articles or other articles by heating
    • C04B37/001Joining burned ceramic articles with other burned ceramic articles or other articles by heating directly with other burned ceramic articles
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B37/00Joining burned ceramic articles with other burned ceramic articles or other articles by heating
    • C04B37/008Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of an organic adhesive, e.g. phenol resin or pitch
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B37/00Joining burned ceramic articles with other burned ceramic articles or other articles by heating
    • C04B37/04Joining burned ceramic articles with other burned ceramic articles or other articles by heating with articles made from glass
    • C04B37/047Joining burned ceramic articles with other burned ceramic articles or other articles by heating with articles made from glass by means of an interlayer consisting of an organic adhesive, e.g. phenol resin or pitch
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/10Inorganic compounds or compositions
    • C30B29/16Oxides
    • C30B29/20Aluminium oxides
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B33/00After-treatment of single crystals or homogeneous polycrystalline material with defined structure
    • C30B33/06Joining of crystals
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74Physical characteristics
    • C04B2235/76Crystal structural characteristics, e.g. symmetry
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74Physical characteristics
    • C04B2235/78Grain sizes and shapes, product microstructures, e.g. acicular grains, equiaxed grains, platelet-structures
    • C04B2235/787Oriented grains
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/34Oxidic
    • C04B2237/343Alumina or aluminates
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/52Pre-treatment of the joining surfaces, e.g. cleaning, machining
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/70Forming laminates or joined articles comprising layers of a specific, unusual thickness
    • C04B2237/704Forming laminates or joined articles comprising layers of a specific, unusual thickness of one or more of the ceramic layers or articles

Definitions

  • the present application relates generally to sapphire and, more particularly, to thin sapphire laminates.
  • Corundum is a crystalline form of aluminum oxide and is found in various different colors, all of which are generally commonly referred to as sapphire except for red corundum which is commonly known as ruby and pinkish-orange corundum which is known as padparadscha. Transparent forms of corundum are considered precious stones or gems. Generally, corundum is extraordinarily hard with pure corundum defined to have 9.0 Mohs and, as such, is capable of scratching nearly all other minerals. For the present purposes, the terms "corundum” and “sapphire” may be used interchangeably to refer generally to the crystalline form of aluminum oxide.
  • corundum due to certain characteristics of corundum, including its hardness and transparent characteristics, among others, it may be useful in a variety of different applications. However, the same characteristics that are beneficial for particular applications commonly increase both the cost and difficulty in processing and preparing the sapphire for those applications. As such, beyond costs associated with it being a precious stone, the costs of preparing the corundum for particular uses is often prohibitive. For example, the sapphire's hardness makes cutting and polishing the material both difficult and time consuming when conventional processing techniques are implemented. Further, conventional processing tools such as cutters experience relatively rapid wear when used on corundum.
  • One embodiment may take the form of a sapphire structure having a first sapphire sheet with a first sapphire plane type forming the major surface and a second sapphire sheet having a second different sapphire plane type forming the major surface.
  • the first and second sapphire sheets are fused together to form the sapphire.
  • Another embodiment may take the form of a sapphire laminate having a first sapphire sheet and a second sapphire sheet fused to the first sapphire sheet.
  • the first and second sapphire sheets have the same crystal orientation with respect to their major surfaces, but different crystal orientations with respect to their edges. That is, the first and second sapphire sheets may have a common sapphire plane forming the major surface and different sapphire planes forming the secondary surfaces.
  • Yet another embodiment may take the form of a glass structure having a glass sheet and a sapphire sheet adhered to the glass sheet.
  • the glass structure is less than or approximately equal to 1 mm thick.
  • Still another embodiment may take the form of a method of manufacturing a laminate structure.
  • the method includes lapping and polishing a first side of a sapphire sheet and adhering the sapphire sheet to a glass sheet.
  • the method also includes lapping and polishing a second side of the sapphire sheet and chemically strengthening the glass sheet.
  • another embodiments may include the use of a sapphire outer surface with a glass inner surface for the display of a consumer electronics device, where the two sapphire surfaces are laminated together with the glass providing support for the display and the sapphire providing scratch resistance and durability advantages.
  • FIG. 1 illustrates an electronic device having a sapphire cover plate.
  • FIG. 2. illustrates two sheets of sapphire each having a different plane on the major surface prior to joining them together to form a sapphire structure.
  • FIG. 3 illustrates the two sheets of sapphire of FIG. 2 joined together to form a sapphire structure.
  • FIG. 4 is a flow chart illustrating the steps for creating the sapphire structure with two sapphire sheets.
  • FIG. 5 illustrates two sheets of sapphire each having the same plane on the major surface but being oriented differently so that different planes are adjacent each other on the edge surface.
  • FIG. 6 illustrates the two sheets of sapphire of FIG. 5 joined together to form a sapphire structure.
  • FIG. 7 illustrates a sapphire sheet and a glass sheet prior to laminating the glass sheet with the sapphire sheet.
  • Fig. 8 illustrates a sapphire structure having a glass sheet in between two sapphire sheets.
  • Sapphire laminates are discussed herein that take advantage of the characteristics of sapphire.
  • sapphire is anisotropic and the crystalline structure of sapphire has multiple different planes. Although each plane exhibits significant hardness over other minerals, some planes may have additional, different characteristics.
  • C- plane sapphire may be harder than other sapphire planes
  • A-plane sapphire may have a higher modulus of rupture than other planes.
  • R-plane and M-plane sapphire may provide other advantages.
  • two sapphire sheets having different sapphire planes are fused together to take advantage of the different characteristics of the different planes.
  • a secondary orientation of the sapphire sheets is controlled so that the edges may have different planes.
  • a sapphire sheet maybe laminated over another material.
  • a sapphire sheet may be adhered to a glass sheet.
  • sapphire structures and/or sapphire laminates on glass allow creation of sheets of approximately one millimeter or less in thickness.
  • the use of glass may provide cost savings over using sapphire, as sapphire is generally more expensive to obtain and/or process than glass.
  • the sapphire laminate provides increased hardness to prevent wear, scratching and/or damage to the glass. Turning to FIG.
  • a sapphire structure or laminate may be implemented.
  • a sapphire laminate 102 may be utilized as a cover glass and/or back plate of the device 100.
  • a sapphire laminate may be utilized as a cover and/or lens for a camera of the device.
  • the sapphire laminates may be utilized in various different devices. For example, they may be used for windows, mirrors, cover glass, lenses and so forth in cameras, computers, mobile devices, watches, display devices, touch screens and clocks among other things.
  • FIG. 2 illustrates two sapphire sheets prior to fusing or adhering the sheets together.
  • Each sheet may have a different plane in the major surface of the sheet.
  • a top sheet 104 may be a C-plane sheet and a lower sheet 106 may be an A-plane sheet.
  • the C- plane may provide increased hardness, while the A-plane may provide a higher modulus of rupture.
  • the combination of the two sheets may improve the hardness of the A-plane sheet and the strength of the C-plane sheet to provide an improved sapphire sheet over a sapphire sheet having only a single plane in the major surface.
  • FIG. 3 shows the two sapphire sheets combined together to form the sapphire structure 108.
  • FIG. 4 is a flowchart illustrating a method 1 10 for fusing two sapphire sheets together.
  • a first side of a first sapphire sheet is lapped and polished (Block 1 12).
  • a first side of a second sheet is then lapped and polished (Block 1 14).
  • the first sides of the first and second sapphire sheets are polished to help reduce the likelihood of any defects or incongruities that may influence the optical properties of the sheets.
  • the lapped and polished sides of the first and second sapphire sheets are then fused together to form a sapphire laminate (Block 1 16).
  • the fusing of the sapphire sheets may occur at, near or above the melting temperature of sapphire.
  • the two sheets may be adhered together using an adhesive instead of being fused.
  • the adhesive may have an index of refraction approximately equal to or near that of sapphire to help eliminate or reduce any refraction that may occur as light passes through from one sapphire sheet, through the adhesive and into the other sapphire sheet.
  • the exposed surfaces of the sapphire laminate may be lapped and polished (Block 118). Both exposed surfaces of the sapphire laminate may be lapped and polished simultaneously. That is, the sapphire laminate may be immersed in an abrasive and/or polishing slurry with a polishing pad on each side.
  • the sapphire structure may also be mechanically modified to help reduce the likelihood of chipping or fracturing. (Block 120). For example, the edges may be beveled or chamfered. Further, the sapphire structure may be treated with oleophobic coating and/or printed with ink (Block 122).
  • one or more steps may be omitted and/or the order that the steps are performed may be changed.
  • the resulting sapphire laminate may achieve both superior hardness and strength due to the use of multiple planes.
  • the combination of these characteristics may allow the sapphire laminate to be handled at thicknesses less than one millimeter with a reduced likelihood of breakage.
  • each sapphire sheet may have a thickness of approximately one millimeter to help reduce the likelihood of breakage through handling prior to creation of the sapphire laminate.
  • the hardness and strength provided by the laminate may permit further handling with a reduced risk of breakage.
  • the thinner laminate may be useful to help reduce the depth or thickness of products implementing the sapphire laminate.
  • FIG. 5 illustrates another embodiment that takes the form of two sheets having the same plane of sapphire in their major surfaces.
  • the term major surface refers to the predominate plane of a sheet (e.g., the top or bottom surface of a sapphire sheet).
  • two A-plane sheets of sapphire 130, 132 are shown.
  • the A-plane sheets 130, 132 may be rotated relative to each other so that the edges 134, 136 are oriented to different planes.
  • the top sheet may have a C- plane along a right edge and the bottom sheet may have an M-plane along the right side.
  • a long axis of the top sheet 130 may be oriented in the C-plane, whereas the long axis of the bottom sheet 132 may be oriented in the M-plane.
  • a longitudinal axis of the sheets (as well as the axial axis) may be oriented at specific angles relative to the crystalline structure of the sapphire.
  • the edge of the sheets may not directly align with the crystalline structure.
  • the edge may be offset 10 degrees from the C-plane.
  • edges may have different sapphire planes that may fracture along different lines and further may provide different hardness and strength characteristics, it is believed that the edges may be more resistant to breakage. More specifically, if one plane is more resistant to chipping while another is preferable for strength considerations, lamination of the sheets together provides an edge that may advantageously have reduced chipping and increased strength.
  • FIG. 6 shows the sapphire structure 138 after the two sheets have been fused together.
  • FIG. 7 illustrates yet another embodiment with a sapphire sheet 140 and a glass sheet 142.
  • One side 144 of the sapphire sheet 140 is lapped and polished.
  • the glass sheet may also be polished.
  • the polished side of the sapphire is then adhered to the glass sheet with adhesive.
  • An adhesive having an index of refraction that is in between the index of refraction of sapphire and the index of refraction of glass may be used to help reduce any optical effects that may occur at or along the interface between the sapphire and the glass.
  • LOCAs liquid optically clear adhesives
  • a sapphire laminate may be applied to a steel back plate, a plastic back plate or other material.
  • a thin hard bond achievable using epoxies and LOCAs may still be desired.
  • the second side of the sapphire (e.g., the exposed side of the sapphire) may then be further lapped and polished.
  • the glass may also be lapped and polished.
  • the lapping and polishing of glass and sapphire may be done in a single double-lapping procedure. As glass is softer than the sapphire, it will generally be thinned more quickly than the sapphire during the lapping process. To counteract the quicker lapping of the glass, in some embodiments, the glass layer may initially be much thicker than the sapphire, or the lapping pads may be of a different material. After lapping and polishing the combined sapphire and glass, the total thickness may be less than approximately one millimeter.
  • the total thickness may be less than or approximately one millimeter or less (e.g., approximately 0.9, 0.8, 0.7, 0.6, 0.5, or 0.4 millimeters or less).
  • Lapping the glass and the sapphire sheets together may minimize the yield challenges associated with lapping and polishing a thin sapphire sheet alone. That is, sapphire sheets may be less susceptible to damage when lapped together with the glass.
  • a computer numerical control process may be performed on the sapphire laminated glass prior to lapping and polishing. Additionally, an edge polish may be performed for the adhesive and joint to smooth the joint and to further eliminate any visible effects resulting from the joinder of the glass and the sapphire.
  • the glass may be chemically strengthened.
  • the chemical strengthening may be performed prior to or after the glass and the sapphire are adhered together, since the sapphire will be mostly unaffected by the glass chemical strengthening process.
  • the glass may be chemically strengthened after the glass has been polished.
  • a minor re-polish may be performed after the chemical strengthening.
  • the glass and the sapphire may be mechanically modified, for example, to have chamfered edges.
  • Utilizing a glass substrate for the sapphire may provide increased resiliency for the sapphire. That is, the glass may help reduce the likelihood of breakage of the sapphire sheet by reinforcing the sapphire. Additionally, the use of the glass substrate may allow for thinner sheets of sapphire to be utilized which may provide cost savings as less sapphire will be used on a per device basis and more sapphire sheets may be harvested from the boule as they may be sliced thinner.
  • Fig. 8 illustrates a sapphire structure 150 having a glass sheet 152 in between two sapphire sheets 154, 156.
  • the sapphire structure 150 may be configured to serve in a variety of different capacities.
  • the sapphire structure 150 may serve as a cover glass in a consumer electronic device, such as a smart phone, a tablet computer, a camera, and so forth.
  • the sapphire structure may be approximately 1 .4 mm, 1 .3 mm, 1 .2 mm, 1 .1 mm, 1 .0 mm, or thinner.
  • the various sheets may be adhered together in any suitable manner to form the structure.
  • the sapphire sheets 154, 156 may have the same crystallographic orientation in their major surfaces. That is, each of the sapphire sheets may each be C-plane or A-plane sapphire. Although, in alternative embodiments, the sapphire sheets may each have different orientations in their major surface. For example, a first sheet 154 may be C-plane sapphire and the second sheet 156 may be A-plane sapphire.
  • a secondary orientation of the sapphire sheets may vary with respect to each other to take advantage of the unique characteristics of the different planes of sapphire.
  • the first sheet 154 may have a secondary orientation that provides chipping resistance
  • the second sheet 156 may have an orientation that is advantageous for strength.
  • the secondary orientations may be selected to provide specific characteristics to a particular side or edge of the sapphire structure, as discussed above.
  • the secondary orientation may be offset an angle from the edge of the structure in some embodiments. That is, the crystallographic orientation of the sapphire sheets may be at an angle relative to the edge of the structure. For example, it may be offset an angle approximately 45 degrees from the long side of the structure. It should be appreciated that the offset angle may be any suitable angle between 0 and 90 degrees.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Structural Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Metallurgy (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Inorganic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Laminated Bodies (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)

Abstract

Various sapphire and laminate structures are discussed herein. One embodiment may take the form of a sapphire structure having a first sapphire sheet with a first sapphire plane type forming the major surface and a second sapphire sheet having a second different sapphire plane type forming the major surface. The first and second sapphire sheets are fused together to form the sapphire structure.

Description

SAPPHIRE LAMINATES
Cross-Reference to Related Applications
This application claims priority to U.S. Provisional Patent Application No. 61/607,401 , filed March 6, 2012, and entitled, "Sapphire Laminates," the contents of which are incorporated herein by reference in their entirety.
Technical Field
The present application relates generally to sapphire and, more particularly, to thin sapphire laminates.
Background
Corundum is a crystalline form of aluminum oxide and is found in various different colors, all of which are generally commonly referred to as sapphire except for red corundum which is commonly known as ruby and pinkish-orange corundum which is known as padparadscha. Transparent forms of corundum are considered precious stones or gems. Generally, corundum is extraordinarily hard with pure corundum defined to have 9.0 Mohs and, as such, is capable of scratching nearly all other minerals. For the present purposes, the terms "corundum" and "sapphire" may be used interchangeably to refer generally to the crystalline form of aluminum oxide.
As may be appreciated, due to certain characteristics of corundum, including its hardness and transparent characteristics, among others, it may be useful in a variety of different applications. However, the same characteristics that are beneficial for particular applications commonly increase both the cost and difficulty in processing and preparing the sapphire for those applications. As such, beyond costs associated with it being a precious stone, the costs of preparing the corundum for particular uses is often prohibitive. For example, the sapphire's hardness makes cutting and polishing the material both difficult and time consuming when conventional processing techniques are implemented. Further, conventional processing tools such as cutters experience relatively rapid wear when used on corundum.
Summary
Various sapphire structure and laminate structures are discussed herein. One embodiment may take the form of a sapphire structure having a first sapphire sheet with a first sapphire plane type forming the major surface and a second sapphire sheet having a second different sapphire plane type forming the major surface. The first and second sapphire sheets are fused together to form the sapphire. Another embodiment may take the form of a sapphire laminate having a first sapphire sheet and a second sapphire sheet fused to the first sapphire sheet. The first and second sapphire sheets have the same crystal orientation with respect to their major surfaces, but different crystal orientations with respect to their edges. That is, the first and second sapphire sheets may have a common sapphire plane forming the major surface and different sapphire planes forming the secondary surfaces.
Yet another embodiment may take the form of a glass structure having a glass sheet and a sapphire sheet adhered to the glass sheet. The glass structure is less than or approximately equal to 1 mm thick.
Still another embodiment may take the form of a method of manufacturing a laminate structure. The method includes lapping and polishing a first side of a sapphire sheet and adhering the sapphire sheet to a glass sheet. The method also includes lapping and polishing a second side of the sapphire sheet and chemically strengthening the glass sheet.
Further still, another embodiments may include the use of a sapphire outer surface with a glass inner surface for the display of a consumer electronics device, where the two sapphire surfaces are laminated together with the glass providing support for the display and the sapphire providing scratch resistance and durability advantages.
While multiple embodiments are disclosed, still other embodiments of the present invention will become apparent to those skilled in the art from the following Detailed Description. As will be realized, the embodiments are capable of modifications in various aspects, all without departing from the spirit and scope of the embodiments. Accordingly, the drawings and detailed description are to be regarded as illustrative in nature and not restrictive.
Brief Description of the Drawings
FIG. 1 illustrates an electronic device having a sapphire cover plate.
FIG. 2. illustrates two sheets of sapphire each having a different plane on the major surface prior to joining them together to form a sapphire structure.
FIG. 3 illustrates the two sheets of sapphire of FIG. 2 joined together to form a sapphire structure.
FIG. 4 is a flow chart illustrating the steps for creating the sapphire structure with two sapphire sheets. FIG. 5 illustrates two sheets of sapphire each having the same plane on the major surface but being oriented differently so that different planes are adjacent each other on the edge surface.
FIG. 6 illustrates the two sheets of sapphire of FIG. 5 joined together to form a sapphire structure.
FIG. 7. illustrates a sapphire sheet and a glass sheet prior to laminating the glass sheet with the sapphire sheet.
Fig. 8 illustrates a sapphire structure having a glass sheet in between two sapphire sheets.
Detailed Description
Sapphire laminates are discussed herein that take advantage of the characteristics of sapphire. In particular, sapphire is anisotropic and the crystalline structure of sapphire has multiple different planes. Although each plane exhibits significant hardness over other minerals, some planes may have additional, different characteristics. For example, while C- plane sapphire may be harder than other sapphire planes, A-plane sapphire may have a higher modulus of rupture than other planes. R-plane and M-plane sapphire may provide other advantages.
In some embodiments, two sapphire sheets having different sapphire planes are fused together to take advantage of the different characteristics of the different planes. In other embodiments, a secondary orientation of the sapphire sheets is controlled so that the edges may have different planes. In other embodiments a sapphire sheet maybe laminated over another material. For example, in one embodiment, a sapphire sheet may be adhered to a glass sheet.
Further, handling and processing sapphire sheets that are approximately one millimeter or less is difficult as it requires increased care to prevent breakage. More particularly, handling sapphire sheets less than approximately 0.5 millimeters (such as 0.4 millimeter sheets) typically results in increased breakage of the sapphire sheets. In accordance with techniques discussed herein, sapphire structures and/or sapphire laminates on glass allow creation of sheets of approximately one millimeter or less in thickness. Moreover, in the case of laminating glass with sapphire, the use of glass may provide cost savings over using sapphire, as sapphire is generally more expensive to obtain and/or process than glass. The sapphire laminate provides increased hardness to prevent wear, scratching and/or damage to the glass. Turning to FIG. 1 , an example electronic device 100 is illustrated in which a sapphire structure or laminate may be implemented. For example, a sapphire laminate 102 may be utilized as a cover glass and/or back plate of the device 100. Additionally, or alternatively, a sapphire laminate may be utilized as a cover and/or lens for a camera of the device. It should be appreciated that the sapphire laminates may be utilized in various different devices. For example, they may be used for windows, mirrors, cover glass, lenses and so forth in cameras, computers, mobile devices, watches, display devices, touch screens and clocks among other things.
FIG. 2 illustrates two sapphire sheets prior to fusing or adhering the sheets together. Each sheet may have a different plane in the major surface of the sheet. For example, a top sheet 104 may be a C-plane sheet and a lower sheet 106 may be an A-plane sheet. The C- plane may provide increased hardness, while the A-plane may provide a higher modulus of rupture. Thus, the combination of the two sheets may improve the hardness of the A-plane sheet and the strength of the C-plane sheet to provide an improved sapphire sheet over a sapphire sheet having only a single plane in the major surface. FIG. 3 shows the two sapphire sheets combined together to form the sapphire structure 108.
FIG. 4 is a flowchart illustrating a method 1 10 for fusing two sapphire sheets together. Initially, a first side of a first sapphire sheet is lapped and polished (Block 1 12). A first side of a second sheet is then lapped and polished (Block 1 14). The first sides of the first and second sapphire sheets are polished to help reduce the likelihood of any defects or incongruities that may influence the optical properties of the sheets. The lapped and polished sides of the first and second sapphire sheets are then fused together to form a sapphire laminate (Block 1 16). The fusing of the sapphire sheets may occur at, near or above the melting temperature of sapphire. In some embodiments, the two sheets may be adhered together using an adhesive instead of being fused. In embodiments where adhesive is utilized, the adhesive may have an index of refraction approximately equal to or near that of sapphire to help eliminate or reduce any refraction that may occur as light passes through from one sapphire sheet, through the adhesive and into the other sapphire sheet.
Once the two sheets are joined together to form the sapphire laminate, the exposed surfaces of the sapphire laminate may be lapped and polished (Block 118). Both exposed surfaces of the sapphire laminate may be lapped and polished simultaneously. That is, the sapphire laminate may be immersed in an abrasive and/or polishing slurry with a polishing pad on each side. The sapphire structure may also be mechanically modified to help reduce the likelihood of chipping or fracturing. (Block 120). For example, the edges may be beveled or chamfered. Further, the sapphire structure may be treated with oleophobic coating and/or printed with ink (Block 122).
It should be appreciated that in some embodiments, one or more steps may be omitted and/or the order that the steps are performed may be changed. For example, in one embodiment, there is not post lamination lapping. That is, the individual sheets may be fully finished prior to lamination.
The resulting sapphire laminate may achieve both superior hardness and strength due to the use of multiple planes. The combination of these characteristics may allow the sapphire laminate to be handled at thicknesses less than one millimeter with a reduced likelihood of breakage. In one example, each sapphire sheet may have a thickness of approximately one millimeter to help reduce the likelihood of breakage through handling prior to creation of the sapphire laminate. After the sapphire laminate has been formed, it may be lapped and polished to a thickness less than one millimeter. The hardness and strength provided by the laminate may permit further handling with a reduced risk of breakage. The thinner laminate may be useful to help reduce the depth or thickness of products implementing the sapphire laminate.
FIG. 5 illustrates another embodiment that takes the form of two sheets having the same plane of sapphire in their major surfaces. As used herein, the term major surface refers to the predominate plane of a sheet (e.g., the top or bottom surface of a sapphire sheet). In particular, two A-plane sheets of sapphire 130, 132 are shown. In this embodiment the A-plane sheets 130, 132 may be rotated relative to each other so that the edges 134, 136 are oriented to different planes. For example, the top sheet may have a C- plane along a right edge and the bottom sheet may have an M-plane along the right side. That is, a long axis of the top sheet 130 may be oriented in the C-plane, whereas the long axis of the bottom sheet 132 may be oriented in the M-plane. As such, a longitudinal axis of the sheets (as well as the axial axis) may be oriented at specific angles relative to the crystalline structure of the sapphire. In some embodiments, the edge of the sheets may not directly align with the crystalline structure. For example, the edge may be offset 10 degrees from the C-plane.
Providing a diversity of planes along the edge may help improve the resilience of the edge of the sapphire structure. For example, as the edges may have different sapphire planes that may fracture along different lines and further may provide different hardness and strength characteristics, it is believed that the edges may be more resistant to breakage. More specifically, if one plane is more resistant to chipping while another is preferable for strength considerations, lamination of the sheets together provides an edge that may advantageously have reduced chipping and increased strength. FIG. 6 shows the sapphire structure 138 after the two sheets have been fused together.
FIG. 7 illustrates yet another embodiment with a sapphire sheet 140 and a glass sheet 142. One side 144 of the sapphire sheet 140 is lapped and polished. The glass sheet may also be polished. The polished side of the sapphire is then adhered to the glass sheet with adhesive. An adhesive having an index of refraction that is in between the index of refraction of sapphire and the index of refraction of glass may be used to help reduce any optical effects that may occur at or along the interface between the sapphire and the glass. Generally, a thin and hard bond is desired to be achieved by the optically clear adhesive. Some epoxies and liquid optically clear adhesives ("LOCAs") may be used as adhesives.
Although the embodiment is discussed as a sapphire laminate on glass, it should be appreciated that a sapphire laminate may be applied to a steel back plate, a plastic back plate or other material. In these embodiments, a thin hard bond achievable using epoxies and LOCAs may still be desired.
The second side of the sapphire (e.g., the exposed side of the sapphire) may then be further lapped and polished. The glass may also be lapped and polished. The lapping and polishing of glass and sapphire may be done in a single double-lapping procedure. As glass is softer than the sapphire, it will generally be thinned more quickly than the sapphire during the lapping process. To counteract the quicker lapping of the glass, in some embodiments, the glass layer may initially be much thicker than the sapphire, or the lapping pads may be of a different material. After lapping and polishing the combined sapphire and glass, the total thickness may be less than approximately one millimeter. In some embodiments, the total thickness may be less than or approximately one millimeter or less (e.g., approximately 0.9, 0.8, 0.7, 0.6, 0.5, or 0.4 millimeters or less). Lapping the glass and the sapphire sheets together may minimize the yield challenges associated with lapping and polishing a thin sapphire sheet alone. That is, sapphire sheets may be less susceptible to damage when lapped together with the glass.
A computer numerical control process may be performed on the sapphire laminated glass prior to lapping and polishing. Additionally, an edge polish may be performed for the adhesive and joint to smooth the joint and to further eliminate any visible effects resulting from the joinder of the glass and the sapphire.
In some embodiments, the glass may be chemically strengthened. The chemical strengthening may be performed prior to or after the glass and the sapphire are adhered together, since the sapphire will be mostly unaffected by the glass chemical strengthening process. Generally, the glass may be chemically strengthened after the glass has been polished. In some embodiments, a minor re-polish may be performed after the chemical strengthening. Further, the glass and the sapphire may be mechanically modified, for example, to have chamfered edges.
Utilizing a glass substrate for the sapphire may provide increased resiliency for the sapphire. That is, the glass may help reduce the likelihood of breakage of the sapphire sheet by reinforcing the sapphire. Additionally, the use of the glass substrate may allow for thinner sheets of sapphire to be utilized which may provide cost savings as less sapphire will be used on a per device basis and more sapphire sheets may be harvested from the boule as they may be sliced thinner.
Fig. 8 illustrates a sapphire structure 150 having a glass sheet 152 in between two sapphire sheets 154, 156. The sapphire structure 150 may be configured to serve in a variety of different capacities. For example, the sapphire structure 150 may serve as a cover glass in a consumer electronic device, such as a smart phone, a tablet computer, a camera, and so forth. In some implementations, it may be advantageous for the sapphire structure to be thin. As such, it may be approximately 1 .5 mm or thinner. For example, the sapphire structure may be approximately 1 .4 mm, 1 .3 mm, 1 .2 mm, 1 .1 mm, 1 .0 mm, or thinner. Additionally, the various sheets may be adhered together in any suitable manner to form the structure.
In some embodiments, the sapphire sheets 154, 156 may have the same crystallographic orientation in their major surfaces. That is, each of the sapphire sheets may each be C-plane or A-plane sapphire. Although, in alternative embodiments, the sapphire sheets may each have different orientations in their major surface. For example, a first sheet 154 may be C-plane sapphire and the second sheet 156 may be A-plane sapphire.
Further, as discussed above, a secondary orientation of the sapphire sheets may vary with respect to each other to take advantage of the unique characteristics of the different planes of sapphire. For example, the first sheet 154 may have a secondary orientation that provides chipping resistance, whereas the second sheet 156 may have an orientation that is advantageous for strength. It should be appreciated that the secondary orientations may be selected to provide specific characteristics to a particular side or edge of the sapphire structure, as discussed above. Additionally, it should be appreciated that the secondary orientation may be offset an angle from the edge of the structure in some embodiments. That is, the crystallographic orientation of the sapphire sheets may be at an angle relative to the edge of the structure. For example, it may be offset an angle approximately 45 degrees from the long side of the structure. It should be appreciated that the offset angle may be any suitable angle between 0 and 90 degrees.
The foregoing describes some example embodiments of sapphire structure and laminates. Although the foregoing discussion has presented specific embodiments, persons skilled in the art will recognize that changes may be made in form and detail without departing from the spirit and scope of the embodiments. In particular, certain processes and/or treatments described above with respect one embodiment may be implemented with other embodiments. Accordingly, the specific embodiments described herein should be understood as examples and not limiting the scope thereof.

Claims

CLAIMS: We claim:
1 . A sapphire structure comprising:
a first sapphire sheet having a first sapphire plane type forming the major surface; and
a second sapphire sheet having a second sapphire plane type forming the major surface, the second sapphire sheet fused to the first sapphire sheet to form the sapphire structure.
2. The sapphire structure of claim 1 , wherein the first sapphire sheet comprises a C-plane sheet.
3. The sapphire structure of claim 1 , wherein the second sapphire sheet comprises an A-plane sheet.
4. The sapphire structure of claim 1 , wherein at least one edge of the sapphire structure is parallel to a sapphire plane.
5. The sapphire structure of claim 1 , wherein at least one edge of the sapphire structure comprises a first sheet edge oriented at a first angle with respect to the crystal planes and a second sheet edge oriented at a second angle with respect to the crystal planes.
6. The sapphire structure of claim 5, wherein at least one edge of the sapphire structure is oriented parallel to a C-plane.
7. The sapphire structure of claim 1 , wherein the sapphire structure is less than 1 mm thick.
8. The sapphire structure of claim 1 , comprising a chamfered edge, wherein the chamfered edge comprises one of a rounded chamfer or an angled chamfer.
9. A sapphire structure comprising:
a first sapphire sheet; and
a second sapphire sheet fused to the first sapphire sheet, the first and second
sapphire sheets having a common sapphire plane type forming the major surface and wherein at least the matching edges of the two sheets have different crystal log raphic orientations.
10. The sapphire structure of claim 9, wherein the first and second sapphire sheets have one of a C-plane or A-plane oriented major surface.
1 1 . The sapphire structure of claim 9, wherein the at least one edge of the sapphire structure is oriented parallel to at least one of a C-plane, an A-plane or an m-plane.
12. A glass assembly comprising:
a glass sheet; and a sapphire sheet adhered to the glass sheet, wherein the assembly is less than or approximately equal to 1 mm thick.
13. The glass assembly of claim 12, wherein the sapphire sheet is adhered to a first side of the glass sheet, wherein the glass assembly further comprises a second sapphire sheet adhered to a second side of the glass sheet.
14. The glass assembly of claim 13, wherein the total thickness of the glass assembly is less than 1 .5 mm thick.
15. The glass assembly of claim 13, wherein the sapphire sheet and the second sapphire sheet have a common sapphire plane type forming the major surface.
16. The glass assembly of claim 15, wherein the sapphire sheet and the second sapphire sheet have one of a C-plane or A-plane oriented major surface.
17. The glass assembly of claim 13, wherein matching edges of the sapphire sheet and the second sapphire sheet have different crystal log raphic orientations.
18. A method of manufacturing a glass assembly comprising:
lapping and polishing a first side of a sapphire sheet;
adhering the sapphire sheet to a glass sheet;
lapping and polishing a second side of the sapphire sheet; and
chemically strengthening the glass sheet.
19. The method of manufacturing of claim 18 further comprising applying an oleophobic or ink mask coating on at least one of the glass or the sapphire sheets
20. The method of claim 18 further comprising polishing the glass sheet.
PCT/US2013/028938 2012-03-06 2013-03-04 Sapphire laminates WO2013134159A2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
KR1020147024390A KR20140129072A (en) 2012-03-06 2013-03-04 Sapphire laminates
CN201380011629.XA CN104159738B (en) 2012-03-06 2013-03-04 Sapphire layer is fit
KR1020167025331A KR101930606B1 (en) 2012-03-06 2013-03-04 Sapphire laminates
JP2014560135A JP6095132B2 (en) 2012-03-06 2013-03-04 Sapphire laminate
EP13711768.5A EP2822760A2 (en) 2012-03-06 2013-03-04 Sapphire laminates

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US61/407,401 2010-10-27
US201261407401P 2012-03-06 2012-03-06

Publications (2)

Publication Number Publication Date
WO2013134159A2 true WO2013134159A2 (en) 2013-09-12
WO2013134159A3 WO2013134159A3 (en) 2013-12-12

Family

ID=47989359

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2013/028938 WO2013134159A2 (en) 2012-03-06 2013-03-04 Sapphire laminates

Country Status (1)

Country Link
WO (1) WO2013134159A2 (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103645818A (en) * 2013-11-26 2014-03-19 浙江上城科技有限公司 Sapphire touch screen and producing method thereof
CN103777833A (en) * 2014-01-17 2014-05-07 贵阳嘉瑜光电科技咨询中心 Method for improving sensitivity of capacitive touch screen
WO2014078026A1 (en) * 2012-11-16 2014-05-22 Apple Inc. Laminated aluminum oxide cover component
WO2015077925A1 (en) * 2013-11-26 2015-06-04 浙江上城科技有限公司 Thermal compounding method for sapphire
WO2015099101A1 (en) * 2013-12-25 2015-07-02 京セラ株式会社 Electronic device and light-transmitting cover substrate for electronic devices
JP2015126319A (en) * 2013-12-26 2015-07-06 京セラ株式会社 Electronic apparatus
JP2015126322A (en) * 2013-12-26 2015-07-06 京セラ株式会社 Electronic apparatus
JP2016054289A (en) * 2014-08-18 2016-04-14 オプティツ インコーポレイテッド Wire bond sensor package and method
US9617639B2 (en) 2013-03-18 2017-04-11 Apple Inc. Surface-tensioned sapphire plate
US9750150B2 (en) 2013-03-18 2017-08-29 Apple Inc. Break resistant and shock resistant sapphire plate
US9745662B2 (en) 2013-03-15 2017-08-29 Apple Inc. Layered coatings for sapphire substrate
US11269374B2 (en) 2019-09-11 2022-03-08 Apple Inc. Electronic device with a cover assembly having an adhesion layer

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5852622A (en) * 1988-08-30 1998-12-22 Onyx Optics, Inc. Solid state lasers with composite crystal or glass components
JP2849602B2 (en) * 1989-09-29 1999-01-20 京セラ株式会社 Joining method of single crystal sapphire
JP2777041B2 (en) * 1993-02-12 1998-07-16 京セラ株式会社 Watch cover glass
JP3333272B2 (en) * 1993-05-28 2002-10-15 シチズン時計株式会社 Method for manufacturing watch cover glass
JP3116317B2 (en) * 1993-11-18 2000-12-11 株式会社山武 Sapphire wafer bonding method
JP3207079B2 (en) * 1995-06-23 2001-09-10 京セラ株式会社 Portable communication device
US6012303A (en) * 1997-06-11 2000-01-11 Saphikon, Inc. Eutectic bonding of single crystal components
US5942343A (en) * 1997-10-16 1999-08-24 Raytheon Company Bonded sapphire, and method of making same
WO2000037720A1 (en) * 1998-12-22 2000-06-29 Japan Cell Co., Ltd. Bonding method of synthetic corundum, production method of synthetic corundum cell, and the synthetic corundum cell
US6858274B2 (en) * 1998-12-22 2005-02-22 Rion Co., Ltd. Synthetic corundum cell
GB2377115B (en) * 2000-12-29 2005-06-22 Nokia Mobile Phones Ltd A casing for a personal communication device, comprising precious metals, precious stones or ceramics
US20060162849A1 (en) * 2003-06-13 2006-07-27 Joo-Hwan Han Method of joining ceramics: reaction diffusion-bonding
JP4939232B2 (en) * 2004-11-29 2012-05-23 京セラ株式会社 Composite ceramic body, method for producing the same, microchemical chip, and reformer
WO2007143480A2 (en) * 2006-06-01 2007-12-13 Ceralink, Inc. Method of lamination using radio frequency heating and pressure
US7966785B2 (en) * 2007-08-22 2011-06-28 Apple Inc. Laminated display window and device incorporating same

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014078026A1 (en) * 2012-11-16 2014-05-22 Apple Inc. Laminated aluminum oxide cover component
US9718249B2 (en) 2012-11-16 2017-08-01 Apple Inc. Laminated aluminum oxide cover component
US9745662B2 (en) 2013-03-15 2017-08-29 Apple Inc. Layered coatings for sapphire substrate
US9617639B2 (en) 2013-03-18 2017-04-11 Apple Inc. Surface-tensioned sapphire plate
US9750150B2 (en) 2013-03-18 2017-08-29 Apple Inc. Break resistant and shock resistant sapphire plate
WO2015077925A1 (en) * 2013-11-26 2015-06-04 浙江上城科技有限公司 Thermal compounding method for sapphire
CN103645818A (en) * 2013-11-26 2014-03-19 浙江上城科技有限公司 Sapphire touch screen and producing method thereof
WO2015099101A1 (en) * 2013-12-25 2015-07-02 京セラ株式会社 Electronic device and light-transmitting cover substrate for electronic devices
JPWO2015099101A1 (en) * 2013-12-25 2017-03-23 京セラ株式会社 Electronic device and translucent cover substrate for electronic device
JP2015126322A (en) * 2013-12-26 2015-07-06 京セラ株式会社 Electronic apparatus
JP2015126319A (en) * 2013-12-26 2015-07-06 京セラ株式会社 Electronic apparatus
CN103777833B (en) * 2014-01-17 2017-01-04 贵阳嘉瑜光电科技咨询中心 A kind of method improving capacitance touch screen sensitivity
CN103777833A (en) * 2014-01-17 2014-05-07 贵阳嘉瑜光电科技咨询中心 Method for improving sensitivity of capacitive touch screen
JP2016054289A (en) * 2014-08-18 2016-04-14 オプティツ インコーポレイテッド Wire bond sensor package and method
US9666730B2 (en) 2014-08-18 2017-05-30 Optiz, Inc. Wire bond sensor package
US9893213B2 (en) 2014-08-18 2018-02-13 Optiz, Inc. Method of forming a wire bond sensor package
US11269374B2 (en) 2019-09-11 2022-03-08 Apple Inc. Electronic device with a cover assembly having an adhesion layer

Also Published As

Publication number Publication date
WO2013134159A3 (en) 2013-12-12

Similar Documents

Publication Publication Date Title
US10052848B2 (en) Sapphire laminates
WO2013134159A2 (en) Sapphire laminates
US20160270247A1 (en) Laminating sapphire and glass using intermolecular force adhesion
TW201313395A (en) Glass plate and glass plate manufacturing method
US8288918B2 (en) Composite substrate and manufacturing method thereof
US10207387B2 (en) Co-finishing surfaces
KR20140144212A (en) Reinforced glass article and touch sensor integrated-type cover glass
WO2013137329A1 (en) Glass substrate for cover glass for electronic device, and production method therefor
TW201433829A (en) A mobile electronic device comprising a multilayer sapphire cover plate
KR20190065377A (en) Polarizer, Polarizer, and Image Display Device
KR20140125173A (en) Multi-layer edge grinding system for glass of touch screen
JP2010128477A (en) Method of manufacturing optical component and optical component
JP5363092B2 (en) Method of manufacturing composite substrate for surface acoustic wave filter and composite substrate for surface acoustic wave filter
JP6682442B2 (en) Base material / ceramic laminate
CN113851153A (en) Spacer, laminated body of substrate, method for manufacturing substrate, and method for manufacturing substrate for magnetic disk
CN111318958B (en) Film for holding glass substrate and method for polishing glass substrate
KR101473174B1 (en) Method for manufacturing liquid crystal display protection film
KR101419002B1 (en) The plank block Processing device which uses lamination plank block processing tool chest
KR101526353B1 (en) Touch screen panel protection sheet
US10112278B2 (en) Polishing a ceramic component using a formulated slurry
CN112969582A (en) Thin glass laminate
US20160378143A1 (en) Sapphire cover with increased survivability
JP6541986B2 (en) Optical element and method of manufacturing imaging element
KR102508911B1 (en) Apparatus for processing ultra thin glass and method for processing ultra thin glass
WO2017009893A1 (en) Method for manufacturing substrate

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 13711768

Country of ref document: EP

Kind code of ref document: A2

WWE Wipo information: entry into national phase

Ref document number: 2013711768

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2014560135

Country of ref document: JP

Kind code of ref document: A

Ref document number: 20147024390

Country of ref document: KR

Kind code of ref document: A