CN107922235A - It is layered glass structure - Google Patents
It is layered glass structure Download PDFInfo
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- CN107922235A CN107922235A CN201680048713.2A CN201680048713A CN107922235A CN 107922235 A CN107922235 A CN 107922235A CN 201680048713 A CN201680048713 A CN 201680048713A CN 107922235 A CN107922235 A CN 107922235A
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- soot layers
- soot
- layering
- layers
- glass structure
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B19/00—Other methods of shaping glass
- C03B19/14—Other methods of shaping glass by gas- or vapour- phase reaction processes
- C03B19/1484—Means for supporting, rotating or translating the article being formed
- C03B19/1492—Deposition substrates, e.g. targets
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered 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
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B19/00—Other methods of shaping glass
- C03B19/14—Other methods of shaping glass by gas- or vapour- phase reaction processes
- C03B19/1453—Thermal after-treatment of the shaped article, e.g. dehydrating, consolidating, sintering
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B19/00—Other methods of shaping glass
- C03B19/14—Other methods of shaping glass by gas- or vapour- phase reaction processes
- C03B19/1469—Means for changing or stabilising the shape or form of the shaped article or deposit
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B37/00—Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
- C03B37/01—Manufacture of glass fibres or filaments
- C03B37/012—Manufacture of preforms for drawing fibres or filaments
- C03B37/014—Manufacture of preforms for drawing fibres or filaments made entirely or partially by chemical means, e.g. vapour phase deposition of bulk porous glass either by outside vapour deposition [OVD], or by outside vapour phase oxidation [OVPO] or by vapour axial deposition [VAD]
- C03B37/01446—Thermal after-treatment of preforms, e.g. dehydrating, consolidating, sintering
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B37/00—Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
- C03B37/01—Manufacture of glass fibres or filaments
- C03B37/012—Manufacture of preforms for drawing fibres or filaments
- C03B37/014—Manufacture of preforms for drawing fibres or filaments made entirely or partially by chemical means, e.g. vapour phase deposition of bulk porous glass either by outside vapour deposition [OVD], or by outside vapour phase oxidation [OVPO] or by vapour axial deposition [VAD]
- C03B37/01466—Means for changing or stabilising the diameter or form of tubes or rods
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C13/00—Fibre or filament compositions
- C03C13/04—Fibre optics, e.g. core and clad fibre compositions
- C03C13/045—Silica-containing oxide glass compositions
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C17/00—Surface treatment of glass, not in the form of fibres or filaments, by coating
- C03C17/02—Surface treatment of glass, not in the form of fibres or filaments, by coating with glass
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C17/00—Surface treatment of glass, not in the form of fibres or filaments, by coating
- C03C17/34—Surface treatment of glass, not in the form of fibres or filaments, by coating with at least two coatings having different compositions
- C03C17/3411—Surface treatment of glass, not in the form of fibres or filaments, by coating with at least two coatings having different compositions with at least two coatings of inorganic materials
- C03C17/3417—Surface treatment of glass, not in the form of fibres or filaments, by coating with at least two coatings having different compositions with at least two coatings of inorganic materials all coatings being oxide coatings
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C23/00—Other surface treatment of glass not in the form of fibres or filaments
- C03C23/0005—Other surface treatment of glass not in the form of fibres or filaments by irradiation
- C03C23/0025—Other surface treatment of glass not in the form of fibres or filaments by irradiation by a laser beam
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/10—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type
- G02B6/12—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind
- G02B6/13—Integrated optical circuits characterised by the manufacturing method
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/02—Pure silica glass, e.g. pure fused quartz
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/06—Doped silica-based glasses
- C03B2201/08—Doped silica-based glasses doped with boron or fluorine or other refractive index decreasing dopant
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/06—Doped silica-based glasses
- C03B2201/30—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/06—Doped silica-based glasses
- C03B2201/30—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
- C03B2201/31—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with germanium
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/06—Doped silica-based glasses
- C03B2201/30—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
- C03B2201/32—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with aluminium
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/06—Doped silica-based glasses
- C03B2201/30—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
- C03B2201/34—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with rare earth metals, i.e. with Sc, Y or lanthanides, e.g. for laser-amplifiers
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/06—Doped silica-based glasses
- C03B2201/30—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
- C03B2201/34—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with rare earth metals, i.e. with Sc, Y or lanthanides, e.g. for laser-amplifiers
- C03B2201/36—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with rare earth metals, i.e. with Sc, Y or lanthanides, e.g. for laser-amplifiers doped with rare earth metals and aluminium, e.g. Er-Al co-doped
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2201/00—Type of glass produced
- C03B2201/06—Doped silica-based glasses
- C03B2201/30—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
- C03B2201/40—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with transition metals other than rare earth metals, e.g. Zr, Nb, Ta or Zn
- C03B2201/42—Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with transition metals other than rare earth metals, e.g. Zr, Nb, Ta or Zn doped with titanium
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2203/00—Fibre product details, e.g. structure, shape
- C03B2203/10—Internal structure or shape details
- C03B2203/12—Non-circular or non-elliptical cross-section, e.g. planar core
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2207/00—Glass deposition burners
- C03B2207/20—Specific substances in specified ports, e.g. all gas flows specified
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C2201/00—Glass compositions
- C03C2201/02—Pure silica glass, e.g. pure fused quartz
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C2201/00—Glass compositions
- C03C2201/06—Doped silica-based glasses
- C03C2201/08—Doped silica-based glasses containing boron or halide
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C2201/00—Glass compositions
- C03C2201/06—Doped silica-based glasses
- C03C2201/30—Doped silica-based glasses containing metals
- C03C2201/31—Doped silica-based glasses containing metals containing germanium
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C2201/00—Glass compositions
- C03C2201/06—Doped silica-based glasses
- C03C2201/30—Doped silica-based glasses containing metals
- C03C2201/32—Doped silica-based glasses containing metals containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C2201/00—Glass compositions
- C03C2201/06—Doped silica-based glasses
- C03C2201/30—Doped silica-based glasses containing metals
- C03C2201/34—Doped silica-based glasses containing metals containing rare earth metals
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C2201/00—Glass compositions
- C03C2201/06—Doped silica-based glasses
- C03C2201/30—Doped silica-based glasses containing metals
- C03C2201/40—Doped silica-based glasses containing metals containing transition metals other than rare earth metals, e.g. Zr, Nb, Ta or Zn
- C03C2201/42—Doped silica-based glasses containing metals containing transition metals other than rare earth metals, e.g. Zr, Nb, Ta or Zn containing titanium
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL 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
- C03C2203/00—Production processes
- C03C2203/40—Gas-phase processes
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/10—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type
- G02B6/12—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind
- G02B2006/12035—Materials
- G02B2006/12038—Glass (SiO2 based materials)
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/10—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type
- G02B6/12—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind
- G02B2006/12083—Constructional arrangements
- G02B2006/12121—Laser
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Abstract
Disclosed herein is layering glass structure and manufacture method.The described method includes making soot deposit on dense glass base material to form composite construction, and the composite construction is sintered to form layering glass structure.Dense glass base material can be obtained by being modified to the fibre-optical preform comprising plane surface.Composite construction can include one or more soot layers.Layering glass structure can stack to be formed by combining multiple composite constructions, then the stacking is sintered and fused and be formed.Layering glass structure can be further heated to softening, and be drawn to control linear dimension.Layering glass structure or the layering glass structure of drawing can be configured to slab guide.
Description
The priority of the U.S. Patent application for the Serial No. 62/207992 submitted this application claims August 21 in 2015, its
Entire disclosure is totally incorporated herein by reference.
Technical field
This specification is related to the structure with multiple glassy layers.More specifically, this specification is related to by covering glass
The waveguide for the core glass layer that glass layer surrounds.More specifically, this specification is related to slab guide, it has doped with dilute
The core glass layer of earth elements and peripheral undoped cladding glass layer.
Background
Waveguide is widely used as the laser amplifier in optical system.Waveguide is by being encapsulated between low-refraction cladding regions
High index of refraction core area form.Waveguide laser receives input laser beam and is amplified, to provide the defeated of more power
Go out light beam.Amplification occurs in core area, and the core area is can to improve the gain media of input laser beam power.Core
Body region generally comprises matrix, and the matrix combines the optical centre (such as rare earth element ion) for providing gain.Matrix can be with
It is crystalline material or glass material, and is introduced optical centre as dopant.Crystalline material includes monocrystalline and ceramics.With generation
The crystalline gain media of table includes oxide-base material (such as YAG, YVO doped with rare earth element4), it is representative
Glass gain media include oxide glass host material (such as silica or modified titanium dioxide doped with rare earth element
Silicon).
Concern for superlaser recently promotes people to be directed to exploitation, and there is enough gains to provide tens of kilowatt extremely
The waveguide laser of several megawatts of output powers.High-gain can be realized by the highly doped level for the optical centre for providing gain,
And/or the size by scaling up gain media is realized with increasing by the optical path length of waveguide.Compared to glass
Glass gain media, crystalline gain media allow generally for the doped level of higher, but are difficult to scale up size, and usually compare glass
Glass gain media produces the scattering loss of higher.Optical centre as such as rare earth element ion is usually in glass gain media
In there is lower dissolubility and lower doping concentration, but glass gain media is easier to put in proportion than crystalline gain media
Large scale, and show lower scattering loss.
The waveguide based on crystalline gain media for being directed to exploitation for high power laser light application produces little effect, because crystallization
Material is difficult to scale up size, and needs long processing time to produce large-sized crystallization medium.With large-sized glass
Glass gain media is available, but sufficiently expensive in the case of using existing manufacturing technology.Manufacture is needed to be used for waveguide
Glass cost effective method.
Summary of the invention
The present disclosure describes the manufacture of the glass structure with multiple glassy layers.These glass structures can be used as waveguide, and
The covering of core layer and low-refraction comprising high index of refraction.In one embodiment, the waveguide is a kind of slab guide,
It has the center high index of refraction core layer being positioned between low-refraction top covering and low-refraction under-clad layer.Core layer and bag
Layer is the different glass of composition.Core layer can include the silica based glasses with rare earth dopant.Covering is silica
Base glass.Silica based glasses include pure silicon dioxide or improved silica.Improved silica is using titanium dioxide
Titanium, germanium oxide or alumina modified silica.
Technique for manufacturing glass structure is included in successive sedimentation soot on dense glass base material.Dense glass base material with
Soot maker relatively moves in soot deposition process, and dense glass base material and porous cigarette are included to be formed in continuous processing
The composite construction of soot layer.Porous soot layers can be made to be deposited on one or more surfaces of dense glass base material, to form tool
There is the multi-layer compound structure of two or more layers.Composite construction consolidation can be made to form densification hierarchy.Densification
Hierarchy may make up prefabricated component, from the prefabricated component drawing waveguide.In other embodiments, hierarchy can will be densified
Fused together with existing glass entity, to increase extra layer.In another embodiment, can be to two or more
A multi-layer compound structure is individually consolidated, and then fuses together them, to form densification hierarchy.Alternatively, can
Two or more multi-layer compound structures are combined before consolidation and are used as with reference to fusing together, to form densification
Hierarchy.
This specification extends to:
A kind of method for manufacturing layering glass structure, the described method includes:
Forming composite construction, the composite construction includes the first soot layers on the dense glass base material, and described first
Soot layers have at least 100 μm of thickness;
Layering glass structure is prepared by the composite construction, described prepare includes consolidating first soot layers;And
The layering glass structure is drawn, the first soot layers of the consolidation have in the layering glass structure of the drawing
There is at least 10 μm of thickness.
This specification extends to:
A kind of method for manufacturing layering glass structure, the described method includes:
The first composite construction is formed, first composite construction includes the first soot on the first dense glass base material
Layer, first soot layers have at least 100 μm of thickness;
The second composite construction is formed, second composite construction includes the second soot on the second dense glass base material
Layer, second soot layers have at least 100 μm of thickness;
Stacked structure is formed by stacking first composite construction and second composite construction, the stacking includes
First soot layers are made to be contacted with second soot layers.
This specification extends to:
A kind of method for manufacturing layering glass structure, the described method includes:
The first composite construction is formed, first composite construction includes the first soot on the first dense glass base material
Layer, first soot layers have at least 100 μm of thickness;
Consolidate first composite construction, the consolidation includes consolidating first soot layers;
The second composite construction is formed, second composite construction includes the second soot on the second dense glass base material
Layer, second soot layers have at least 100 μm of thickness;
Stacked structure, the heap are formed by the first composite construction and second composite construction that stack the consolidation
It is folded to include making the first soot layers of the consolidation contact with second soot layers.
This specification extends to:
A kind of method for manufacturing layering glass structure, the described method includes:
The first composite construction is formed, first composite construction includes the first soot on the first dense glass base material
Layer, first soot layers have at least 100 μm of thickness;
Stacked structure is formed by stacking glassy layer in first soot layers.
Other features and advantages of the present invention, Partial Feature and advantage pair therein are given in the following detailed description
It will be appreciated that for those skilled in the art, or by implementing institute in word description and its claims and attached drawing
State embodiment and be realized.
It is to be understood that what general description and following detailed description above was all merely exemplary, for providing understanding
The property of claims and the overview of feature or frame.
Appended attached drawing, which provides, to be further understood, and attached drawing is incorporated in the present specification and a part for constitution instruction.
Attached drawing is the illustration to the selected aspect of this specification, the principle of its method included together with specification to this specification and
Operation, product and composition explain.It is characterized in the diagram for embodiment selected by this specification shown in attached drawing, its
It need not draw in appropriate proportions.
The brief description of accompanying drawing
Although this specification is made knots with claims, specifically note and clearly define described technology contents,
Think to more fully understand this specification by described description in conjunction with the following drawings, wherein:
Fig. 1 is a kind of schematic diagram of slab guide.
Fig. 2 illustrates the continuous laser sintering and consolidation of composite construction.
Fig. 3 shows the size adjusting of the multilayer glass structures carried out using drawing process.
Fig. 4 illustrates a kind of fibre-optical preform.
Fig. 5 illustrates the dense glass base material with the plane surface formed by fibre-optical preform.
Fig. 6 illustrates deposition of the soot layers on the plane surface of dense glass base material.
Fig. 7 shows the laser sintered of the soot layers that are formed on the plane surface of dense glass base material.
Fig. 8 shows deposition of the soot layers on the sinter layer being formed on the plane surface of dense glass base material.
Fig. 9 shows the representative processing for the layering glass structure with the core surrounded by two coverings
Program.
Figure 10 is shown by combining two composite constructions to form layering glass structure.
Figure 11 is shown by making layering glass structure be combined with composite glass structure to form layering glass structure.
Figure 12 is shown by combining two layering glass structures to form layering glass structure.
Figure 13 is shown using outside vapor deposition method to produce glassy layer.
Figure 14 is shown by composite construction or layering glass structure and the existing or glassy layer that is individually formed to be formed
It is layered glass structure.
The embodiment illustrated in attached drawing is exemplary, it is no intended to limits the model of detailed description or the claims
Enclose.As possible, make the same or similar feature is presented with like reference characters in the accompanying drawings.
Detailed description of the invention
In the following, the illustrative embodiments of this specification are described in detail.
This specification provides the hierarchy with core glass layer region and glass-clad region.This specification also provides
For manufacturing the low-cost manufacture method of layering glass structure.These layering glass structures can be used as waveguide, amplifier and/or swash
Light device.
In one embodiment, layering glass structure is configured to slab guide.Fig. 1 is exemplified with one according to this specification
Kind slab guide.Slab guide 10 includes core layer 20, covering 15 and covering 25.The thickness of core layer 20 is at 5 μm to 300 μm
In the range of or in the range of 10 μm to 300 μm or in the range of 25 μm to 250 μm or in 50 μm to 200 μm of scope
It is interior or in the range of 75 μm to 150 μm.Each in covering 15 and covering 25 is all thicker than core layer 20.Covering 15 and bag
Layer 25 thickness be at least 10 μm or at least 25 μm or at least 50 μm or at least 100 μm or at least 250 μm or
At least 500 μm or at least 1mm or at least 2mm or at least 5mm or at least 10mm or at least 15mm or
At least 20mm or in the range of 10 μm to 50mm or in the range of 25 μm to 40mm or in 50 μm to 30mm of scope
It is interior or in the range of 100 μm to 25mm or in the range of 150 μm to 25mm or in the range of 200 μm to 25mm or
In the range of 250 μm to 25mm or in the range of 500 μm to 25mm.Covering 15 and covering 25 can have identical or different
Thickness.
Core layer 20 and covering 15 and covering 25 include glass material.Compared to covering 15 and covering 25, core layer 20
It is the glass material of refractive index higher.Core layer 20 and covering 15 and covering 25 can be through overdoping or undoped
Glass.The glass can be by doped or undoped silica.The glass can be through overdoping or without
The silica based glasses of doping.Silica based glasses include pure silicon dioxide glass, utilize one or more of oxides
(such as Al2O3、GeO2、Ga2O3、B2O3、P2O5), transition metal oxide (such as TiO2), alkali metal oxide and alkaline earth gold
Belong to the silica glass of oxide modifying and be doped with the silica glass of fluorine and/or chlorine.
Core layer 20 and covering 15 and covering 25 are different in composition.Covering 15 and covering 25 can have identical or different
Composition.When planar-light guide 10 is used as laser, core layer 20 includes the glass with dopant, and forms for amplification
Gain media.Glass with dopant can be the silica based glasses with dopant or the pure dioxy with dopant
SiClx glass.Dopant can be luminescent metal ion, such as rare earth element ion or transition metal ions.In a kind of embodiment party
In formula, core layer 20 includes the silica glass doped with rare earth element or the improved silica glass doped with rare earth element
Glass, and covering 15 and covering 25 include undoped silica glass, undoped improved silica glass or doped with
The silica glass of fluorine and/or chlorine.Rare earth dopant includes Yb3+、Er3+、Tm3+And Nd3+.Comprising oxide modifier (such as
Al2O3、GeO2、TiO2Or Ga2O3) dissolubility of the rare earth dopant in silica based glasses can be improved, and higher can be passed through
Rare earth element ion doping concentration obtain more high-gain.Rare earth dopant may also function as increase silica based glasses refractive index
Effect, and help to reach core-cladding index contrast for realizing needed for effective waveguide.
This specification provides the batch processing for being used for manufacturing layering glass structure.The processing includes soot layers being deposited on
On dense glass base material.Dense glass base material can have be layered glass structure core layer it is corresponding composition or with layering
The corresponding composition of covering of glass structure.In one embodiment, dense glass base material has a plane surface, and soot
Deposition occurs on the plane surface.Dense glass base material can be rectangular flat or the arbitrary shape with plane surface.
The soot for forming soot layers on dense glass base material is supplied using soot maker.In a kind of embodiment party
In formula, soot maker is burner, and soot produces in the following manner:By the way that soot precursor is delivered to burner and is made
Soot precursor is reacted or decomposed to form the soot particles for being deposited on dense glass base material.
The various devices and technique known in the art for being used to generate soot particles can be used.Usually by soot particles with cigarette
The form of soot stream is transferred on deposition surface.Example available for the soot generating means in the various embodiments of the processing
Including flame hydrolysis burner, such as those are commonly used in IVD, OVD and VAD and planar depositions known in the art processing
Device.It is special that suitable burner configuration is disclosed in 6606883,5922100,6837076,6743011 and No. 6736633 U.S.
In profit, disclosures of these documents is incorporated herein by reference in their entirety.
Soot maker can include single burner or multiple burners.It is l that a kind of exemplary burner, which has length,
And the output surface that width is w.The output surface can include N row gases aperture, wherein, N can in the range of 1 to 20 or more
Greatly.In one embodiment, each aperture includes the hole of a diameter of 0.076cm.The length l of output surface can about 2.5 to
In the range of 30.5cm or bigger, and width can be in the range of 0.1 to 7.5cm.Optionally, multiple burners can be configured to combustion
Burner array, to produce substantially continuous soot particles stream in the length and width of array.Can to the quantity of burner and/
Or the size of burner array is adjusted or configures, so that the presumptive area on soot covering dense glass base material deposited surface.
For example, burner array can include multiple single burners (for example, being placed by end to end), these single combustions
Burner configuration is shaped as and deposits temporary transient and spatially uniform soot particles layer.Burner array can include multiple modules
Linear array, these modules are positioned along common direction, to provide soot on the width of extension.Representational burning
Device module and burner array are described in No. 8746013 United States Patent (USP)s, and the disclosure of which includes this by reference of text
Text.Therefore, it can be used to be formed in specific region of the soot maker on dense glass base material and there is substantially evening chemical group
Into the single layer of the soot with substantially uniform thickness.Can be by mobile dense glass base material and/or soot maker in densification
Expand area coverage using soot particles in the additional areas of glass baseplate deposition surface." uniformly composition " and " uniform thickness "
Refer to that the composition in given area and thickness change are less than or equal to the 20% of average composition or thickness.In certain embodiments
In, it is flat in soot that one or both of the composition change of soot and thickness change may be less than or equal to each of which
The 10% of average.
A kind of representative burner can include 9 row gas apertures.In use, according to a kind of embodiment party
Formula, center alignment (such as the 5th row) offer silica gaseous precursors/carrier gas mixture, and adjacent row (such as the 4th
Row and the 6th row) oxygen for being used for that silica gaseous precursors to be carried out with Chemical Measurement control is provided.Positioned at center line both sides
Subsequent two row gas aperture (such as the 2nd row, the 3rd row, the 7th row and the 8th row) provides extra oxygen, and the stream of oxygen can be used
Speed provides oxidant to control Chemical Measurement and soot density for igniting.Outermost row aperture (such as the 1st row and
9th row) such as CH can be provided4/O2Or H2/O2Ignition mixture.The example gases flow rate of this 9 column linear burner
Scope is listed in table 1.
The example gases flow rate of 1.9 column linear burner of table
Gas | Burner column | Exemplary flow rate |
OMCTS | 5 | 15 gram/minutes |
N2 | 5 | 40SLPM |
O2 | 4,6 | 18SLPM |
O2 | 2,3,7,8 | 36SLPM |
CH4 | 1,9 | 36SLPM |
O2 | 1,9 | 30SLPM |
In addition to burner, other soot generating means (such as plasma heating soot sprayer etc.) can be used
Soot particles needed for processing are provided.In plasma heating soot sprayer, provided with certain speed with single one or more
The pre-formed soot particles of kind composition, and plasma is passed to, soot particles are heated to depositing required by plasma
Temperature.In addition, in some embodiments, the combination of burner and plasma heating soot sprayer can be used to provide glass
Glass soot particles.In purpose is facilitated, unless indicated to the contrary, " burner " otherwise used herein represents to be used at this
All soot generating means of reason, unless indicated to the contrary.
Between being typically included in precursor chemical (such as gaseous compound) chemistry occurs for the operation of soot generating means
React to form glass soot particles.Optionally, can also by the supply energy or supplementary heating device of such as plasma come
Auxiliary so chemical reaction.
For example, it is sinterable to form the silica soot of silica glass to be formed that silicon-containing precursor compounds can be used
Particle.A kind of exemplary silicon-containing precursor compounds are octamethylcy-clotetrasiloxane (OMCTS).Can be by OMCTS and H2、O2、CH4
Or other fuel are concomitantly introduced into burner or burner array, OMCTS is aoxidized with life during flame combustion wherein
Into silica soot particles.Other silicon precursors include SiCl4。
For example, a kind of exemplary burner in the production for passing through the silica glass of flame hydrolysis includes hole, pass through
Silicon-containing precursor compounds as such as OMCTS (octamethylcy-clotetrasiloxane) are introduced H by this some holes2、CH4Or other fuel
In flame.OMCTS is generated the fine silica soot for being transported to dense glass base material deposited surface in flame by oxidation
Particle.
The soot particles just provided can be mainly made of single oxide, such as produce undoped silica glass
In the case of.Alternatively, when using soot generating means to produce soot particles, these soot particles can be through overdoping
's.When soot generating means include the burner being used for using flame hydrolysis or flame combustion processing generation soot, can pass through
The precursor comprising dopant is completed to adulterate in flame.Doping precursor can be replenished to the unitary part of soot generating means,
Or it is replenished to soot generating means as the mixture with silica or other substrate glasses precursors.When soot generating means
During comprising plasma heating soot sprayer, from sprayer spraying pre-formed soot particles can be by pre-doping,
Or the soot particles of spraying can be placed in the atmosphere containing dopant, so that soot particles are gradually incorporated in the plasma
It is miscellaneous.In some embodiments, the soot particles provided advantageously have substantially homogeneous compositional.In certain embodiments
In, soot particles can have different compositions.For example, the soot of main glass ingredient can be provided using a kind of soot generating means
Grain, and provide the soot particles of dopant using single soot generating means.In another example, can before sintering or
Dopant is incorporated into existing soot layers in sintering process.
The example of dopant includes IA, IB, IIA, IIB, IIIA, IIIB, IVA, IVB, VA, VB in the periodic table of elements
The element of race, halide and Rare Earth.Doping precursor includes halide, hydride and the organo-metallic compound of dopant.
The compound of the alkoxide cpd of organo-metallic compound including dopant and dopant with various ligands or they
Combination, including:Alkyl compound, alkenyl compound, amine, chelatingligand, ethylenediamine, acac (acetylacetonate), FOD
(the fluoro- 2,2- dimethyl -3,5- octanediones compounds of 6,6,7,7,8,8,8- seven), acetate, 2,4- pentanedionates, 3,5-
Heptane diketonate, 2,2,6,6- tetramethyl -3,5- heptane diketonate, isopropoxide, butylate, methoxide and ethylate.
May in some embodiments, soot particles can be mixed with each other and form the composite material granular with various compositions.May be used also
Can in some embodiments, soot particles substantially avoid depending on each other and mixing are formed before deposition surface is deposited to
Particle.
In some embodiments, dopant is rare earth element ion (such as Yb3+、Er3+、Nd3+、Tm3+、Pr3+、Ho3+)。
There is high index of refraction doped with the silica based glasses of rare earth element, and can be used as being layered the core layer of glass structure.It is known
Rare earth dopant has limited dissolubility in silica based glasses.In order to improve dissolubility, be preferably minimized phase separation
And increase concentration of the rare earth dopant in silica glass, preferably Al is included in glass composition2O3、GeO2、Ga2O3Or its
Oxide (such as the TiO of its high charge density metal ion2).High charge density metal oxide and rare earth in glass composition
The ratio between dopant oxygen compound can be more than 1.0 more than 1.5 or more than 2.0 or more than 3.0 or more than 4.0 or 1.0 to
In the range of 5.0 or in the range of 1.5 to 4.0.
Formed and deposit soot particle during, soot maker can remains stationary, or can be relative to deposition table
Face movement (such as vibration or translation) soot maker.Dense glass base material can move each other with soot maker, to permit
Perhaps continuous soot deposit is carried out on the surface of dense glass base material.Relative motion can be by dense glass base material movement, cigarette
The movement of soot maker or the movement of dense glass base material and soot maker are realized.In one embodiment, fine and close glass
The movement of glass base material and/or soot maker can be unidirectional.The one-way movement can be translational motion.Implement in another kind
In mode, the movement of dense glass base material and/or soot maker can be two-way.The bidirectional-movement can be moved back and forth
(such as rearwardly and a forwardly moving).Can be in the scope of about 20mm to 100mm to the distance of deposition surface from burner output surface
Interior (such as 20,25,30,35,40,45,50,55,60,65,70,75,80,85,90,95 or 100mm).Generated and filled by soot
Put the relative motion with dense glass base material, the covering of the soot particles of the Soot Formation device that width is fixed to deposition surface
Linear velocity can be in the range of 0.1 mm/second to 10 meter per seconds.For with multiple burners (such as burner array)
Soot generating means, region overlay are given by the covering linear velocity of soot generating means and the product of cover width.
The average soot density of the silica based glasses of 90% silica is comprised more than usually 0.30 to 1.50g/
cm3In the range of or 0.80 to 1.25g/cm3In the range of or 0.40 to 0.70g/cm3In the range of.
By reciprocal relative motion, the thickness of the soot layers of deposition can be increased.The required thickness of soot layers can be by consolidating
The final use of the layering glass structure formed afterwards determines.Following article is more complete described, and the layering glass structure of consolidation can use
Make the prefabricated component in drawing processing, with the effectively different layer of thinning in a controlled manner, so as to fulfill with target size
Waveguide.Therefore, method described herein is capable of providing advantage relative to other technologies (such as LOC), because can be in rear deposition
Thick soot layers are deposited and adjusted in processing, to meet thickness requirement.When multiple soot layers of the deposition with different compositions are to form
During multi-layer compound structure, the relative thickness of different layers can be determined by the final use of the layering glass structure formed after consolidating.Can
The thickness of soot layers is controlled using the sedimentation rate and sedimentation time of the soot from soot generating means.Soot generating means
Operation each time on dense glass base material passes through the thickness that can all increase soot layers.Soot generating means are in dense glass base
Run on material the number passed through be smaller than 200 less than 100 or less than 50 or less than 25 or less than 10 or 1 to 200 it
Between or between 1 to 100 or between 1 to 50 or between 1 to 25.
The thickness of soot layers is at least 10 μm or at least 25 μm or at least 50 μm or at least 100 μm or at least
For 250 μm or at least 500 μm or at least 1mm or at least 2mm or at least 5mm or at least 10mm or at least
For 15mm or at least 20mm or in the range of 10 μm to 50mm or in the range of 25 μm to 40mm or at 50 μm extremely
In the range of 30mm or in the range of 100 μm to 25mm or in the range of 150 μm to 25mm or at 200 μm to 25mm
In the range of or in the range of 250 μm to 25mm or in the range of 500 μm to 25mm.
In some embodiments, it is desirable to which the soot layers of deposition change with low local soot density.In some embodiment party
In formula, for obtaining forming substantially uniform final sintered glass layer, low local soot density change is important.Remove
Beyond other factors, following factor can influence the local soot density change of soot layers:(i) burner or the life of other soots
Design and position into device;(ii) burner relative to deposition surface movement;(iii) burner or other soots generation dress
The temperature change of provided particle is provided;And the temperature change on (iv) dense glass base material deposited surface.It is advantageously used
With the soot generating means of the burner array comprising multiple burners come obtain chemical composition substantially uniformly and thickness base
Uniform soot deposited layer in sheet." thickness is uniform " refers to that the thickness change of soot layers is less than or equal to soot layers average thickness
20%.In some embodiments, it is desirable to which the thickness change of soot layers is less than or equal to the 10% of soot layers average thickness.At certain
In a little embodiments, burner can be adjusted relative to the movement of deposition surface, it is substantially uniform with auxiliary generation thickness
Soot layers.In some embodiments, burner is made to be vibrated from the side of deposition surface to opposite side, it is basic with deposit thickness
Upper uniform soot layers.In some embodiments, for uniform local soot density is obtained in soot layers, firing
It is important to have substantially uniform temperature before burner direct flame contact deposition surface across the deposition surface.
In the state of firm deposition, soot layers are porous layers.In subsequent processing, soot layers are made to sinter and consolidate, with shape
Into dense glass layer.In sintering processes, soot layers are heated to sintering temperature, so that the soot particles in porous soot layers cause
Densification, so as to form the glassy layer of consolidation.Consolidation can occur in continuous or batch processing.In order to make soot consolidation, by soot
Layer is heated to sufficiently high temperature and for a sufficiently long time, so that soot changes into the glass of densification.Except it
Beyond its factor, those skilled in the art can according to the forming of glass, the required quality and process yields of final glass come
Determine suitable sintering temperature and sintering time.For example, in order to be sintered to the soot of high-purity silicon dioxide, it is usually uncommon
It is 1000 DEG C to 2000 DEG C to hope sintering temperature, is in some embodiments 1400 DEG C to 1600 DEG C.Those skilled in the art one
As know, during sintering stage, it is allowed to which the soot particles for forming soot layers form more chemical bonds in grain boundaries, to obtain
Continuous and densification the glass network of bigger.In some embodiments, it is desirable to which the sintered product in glass material is substantially not
Containing cavity and bubble.
The thickness of the soot layers of consolidation be at least 10 μm or at least 25 μm or at least 50 μm or at least 100 μm,
At least 200 μm or at least 300 μm or at least 500 μm or at least 1mm or at least 2mm or be at least
5mm or at least 10mm or at least 15mm or at least 20mm or in the range of 1 μm to 25mm or at 5 μm extremely
In the range of 20mm or in the range of 10 μm to 15mm or in the range of 10 μm to 10mm or in 10 μm to 5mm of model
In enclosing or in the range of 25 μm to 1mm or in the range of 50 μm to 500 μm or in the range of 50 μm to 250 μm or
In the range of 50 μm to 125 μm.
In some embodiments, it is desirable to by sintering and consolidating soot layers and at least big in the dense glass layer that is formed
Part has high surface quality:Low external waviness;Low surface roughness;And substantially free of cut.Several side can be used
Method obtains high quality surface.For example, preventing that the exposed surface of soot layers is (straight not with dense glass base material or lower section glassy layer
The surface of contact) it is sintered while contacted with solid body.Think avoiding exposed surface from connecing with solid body
Soot layers are sintered in gas or vacuum environment and surface defect can be preferably minimized while touching, and are promoted by having
The soot layers for having high quality surface form dense glass layer.In addition, the surface quality of the glass after sintering can be led to soot
The influence of pollutant (such as surrounding environment particle) on layer exposed surface.Therefore, in clean environment as such as dust free room
In be sintered can help improve sintering after glassy layer surface quality.
Various heat sources can be used to be heated to sintering by soot layers and consolidate required temperature.Can use such as resistance heating,
Sensing heating and laser heating.Fig. 2 is exemplified with the sintering and consolidation using laser heat source.Composite construction 40 includes dense glass base
Material and one or more soot layers.Transport composite construction 40 and make it under sintering laser 45, to be formed by not
Sinter the sintering region 50 that region 55 surrounds.Can be by sintering the movement or positioning or by including in systems of laser 45
Multiple sintering lasers sinter the width in region 50 to control.Illustrated embodiment shows 40 phase of composite construction in Fig. 2
Movement for sintering laser 45.In other embodiments, sintering laser 45 is moved relative to composite construction 40.It is multiple
Close structure 40 and sintering laser 45 can in opposite direction, different directions or moved in same direction with different rates.
It is laser sintered improve between base material and adjacent consolidation soot layers or in sandwich construction it is viscous between continuous soot layers
Conjunction property.Sintering can also by eliminate bubble and/or provide for add soot deposit smooth surface come improve base material with
The interface between interface or adjacent soot layers between adjacent consolidation soot layers.Surface smoothness can be by arithmetic mean roughness Ra
To quantify.Roughness RaIt is count inequality of the roughness component from the fluctuating (peak height and Gu Shen) of surface mean place.It is available
Talysurf known in the art measures roughness Ra, and the average value along surface linear or region part can be denoted as.Profit
With the roughness R on the surface of laser sintered offeraIt is smaller than 1.0nm or less than 0.75nm or less than 0.50nm or is less than
0.35nm or less than 0.25nm or less than 0.15nm or less than 0.10nm or in the range of 0.05nm~1.0nm or
In the range of 0.05nm~0.75nm or in the range of 0.05nm~0.50nm or in the range of 0.05nm~0.25nm.
Realize the area of surface roughness as described herein and the area phase covered during laser sintered by laser
Symbol is substantially consistent.As described above, multiple lasers can be used to increase laser sintered area coverage.Alternatively, can profit
Single laser or multiple lasers or the surface for making single laser or the inswept sandwich construction of multiple lasers are handled with grating,
To increase sintering area, so as to expand the area of the smooth surface with roughness as described herein.With table as described herein
The area of surface roughness can be at least 0.02mm2Or at least 0.05mm2Or at least 0.10mm2Or at least 0.25mm2、
Or at least 0.50mm2Or at least 1mm2Or at least 5mm2Or at least 10mm2。
Individually and independently the surrounding ambient atmosphere in sintering and consolidation process can be adjusted, to meet various glass
The production of material needs.Thermal history of the soot layers in sintering process can influence the thickness of the dense glass layer formed by the soot layers
Degree, composition, composition homogeneity, the uniformity of physical property (such as refractive index, birefringence etc.) and physical property.Therefore, exist
In the case of needing dense glass layer with uniform composition and/or property, it is desirable to soot layers is undergone base in sintering process
Uniform sintering temperature in sheet.It is substantially uniform to obtain that sensing heating, resistance heating or laser heating is advantageously used
Sintering temperature.
Heat source can be in the range of 0.5mm to 50mm or in 1mm apart from the distance of soot layers exposed surface in sintering process
Model in the range of to 45mm or in the range of 2mm to 40mm or in the range of 3mm to 35mm or in 5mm to 30mm
In enclosing.It can be completed by the way that a branch of or more beam laser beam from one or more lasers to be oriented to the surface of soot layers
Laser heats.Multiple lasers can be used and they are arranged in array or laser storehouse, to realize for example broad soot layers
Region overlay, so as to sinter the multiple regions of soot layers at the same time.Alternatively, one or more laser can be handled by using grating
Device come realize broadness region overlay.One or more lasers can be moved in a controlled manner, with (complete or partial)
The surface of inswept soot layers, so as to effectively be sintered and consolidated in desired zone.The laser of different wave length can be used, its
In, the wavelength of each laser is optimized for specific soot composition.Laser can be focused on or do not focused on.Multiple layers of soot can
Sequentially or simultaneously sinter.The wavelength or depth of focus of laser can be adjusted, be sintered with the sub-surface region to soot layers or
In the stacking that person's intervention is made of two or more soot layers positioned at dense glass base material and apart from dense glass base material most
Soot layers between remote soot layers.
In some embodiments, the heating chamber being sintered is filled with inert gas (such as N2, Ar, Ne, they
Mixture etc.) to improve heat transfer, and prevent apparatus assembly, soot layers, the cause formed by soot layers and/or dense glass base material
The oxidation of close glassy layer.
Composite construction can be formed by the way that one or more soot layers are deposited on dense glass base material.One or more
Multiple soot layers can have identical or different composition.The composition of one or more soot layers can be with the group of dense glass base material
Into identical or different.In one embodiment, the composition of dense glass base material has the composition higher than soot layers
Refractive index.For example, dense glass base material can have the composition of waveguide cores layer, and soot layers can have the composition of waveguide covering.
In another embodiment, the composition of dense glass base material has the refractive index lower than the composition of soot layers.For example,
Dense glass base material can have the composition of waveguide covering, and soot layers can have the composition of waveguide cores layer.
Composite glass structure can include two or more soot layers.Can be on the same side of dense glass base material by two
Or more soot layers be sequentially depositing on top of each other, to be formed with the sandwich construction for forming identical or different soot layers.
For example, dense glass base material can have the composition of waveguide covering, the soot layers with waveguide cores layer composition can be deposited over cause
On close glass baseplate, and the soot layers with waveguide covering composition can be deposited over the soot layers with waveguide cores layer composition
On.In this composite construction, the soot layers with core layer composition are with than dense glass base material or with covering composition
The refractive index of soot layers higher.
In one embodiment, the soot layers with core layer composition are deposited on dense glass base material, and are had
The soot layers of covering composition are deposited in the soot layers with core layer composition.In another embodiment, there is covering
The soot layers of composition are deposited on dense glass base material, and the soot layers with core layer composition are deposited over to be formed with covering
Soot layers on, and with covering composition soot layers be deposited over core layer composition soot layers on.With covering group
Into soot layers can be thicker than with core composition soot layers.Soot layers with covering composition are than the cigarette with core composition
At least 5 times of soot thickness or thick at least 10 times or thick at least 25 times or thick at least 50 times or thick at least 100 times or thickness 5 to 100
It is again or 10 to 100 times or 10 to 90 times or 25 to 75 times thick thick thick.
Alternatively, two or more soot layers can be deposited on the different surfaces of dense glass base material.The difference table
Face can be opposite surface or nonoverlapping surface.For example, dense glass base material there can be the composition of waveguide cores layer, have
First soot layers of waveguide covering composition can be deposited on the first surface of dense glass base material, and with waveguide covering composition
The second soot layers can be deposited on the second surface of dense glass base material, wherein, second surface is located at dense glass base material
On the side opposite with first surface, so that dense glass base material is between the first soot layers and the second soot layers.This
In composite construction, dense glass base material has the refractive index of soot layers higher more peripheral than two.Two or more soot layers can
It is deposited in each in two or more surfaces of dense glass base material.
When deposited two or more soot layers, the deposition of all soot layers can occur before sintering and consolidating, and
All soot layers can be made to undergo sintering and consolidation condition at the same time.Alternatively, the deposition and sintering and consolidation of soot layers can replace
Carry out.For example, soot layers can be formed on dense glass base material, it is sintered and consolidates to form dense glass layer, and can
One or more additional soot layers are deposited on dense glass layer.Then, it is sinterable and consolidate one or more
Additional soot layers, and can redeposited additional one or more soot layers.
(glass can be also referred to as layered herein to the densification hierarchy formed after the sintering of composite construction and consolidation
Glass structure) it is further processed.Additional processing may include dried soot layer (such as using Cl2);Adulterate soot layers;Machinery
Process to form required shape;Polishing;Annealing;Cutting etc..Additional processing may also include drawing.In drawing processing, it will cause
Densification hierarchy is heated to softening, and then makes its thinning by being drawn along selected draw direction.In pulling process,
Densification hierarchy is stretched, and is cured again by cooling.Can be by pulling the densification hierarchy or right softened
It applies active force or thinning is completed to draw under gravity by making the densification hierarchy of softening.
As densification hierarchy is stretched, its is thinning, and dense glass base material and formed by soot one or
One or more linear dimensions (such as thickness, length, height) of more dense glass layers reduce.In a kind of embodiment
In, in the relative thickness (or other corresponding linear dimensions) of dense glass base material and one or more dense glass layers
The relative thickness (or other corresponding linear dimensions) of each is kept constant.That is, dense glass base material relative thickness (or its
Its corresponding linear size) with the relative thickness of each (or other corresponding linear rulers in one or more dense glass layers
It is very little) between proportionate relationship with densification hierarchy after drawing it is thinning keep it is identical.In one embodiment, draw
The proportionate relationship (for example, height and the width, wherein height can be equivalent to thickness) of latter two linear dimension remains unchanged.
Fig. 3 is schematically illustrated by densification hierarchy draw plane waveguide.Densification hierarchy 60 includes core
Body layer 65, covering 70 and covering 75.Densification hierarchy 60 is placed in draw machines, is heated to softening, and in gravity
Effect is lower and/or final size is drawn into tension force aid in treatment, to form the hierarchy 80 drawn.
Drawing processing allows to be controlled the thickness (or other linear dimensions) for being layered glass structure.For example, it can pass through
Draw the thickness (or other linear dimensions) of processing control waveguide core layer and covering.It is layered the thickness of a layer in glass structure
(or other linear dimensions) can be that the thickness (or other linear dimensions) of a layer in the layering glass structure exists after drawing
Before drawing at least 0.1% or at least 1% or at least 2% or at least 5% or at least 10% or at least 20% or at least
40% or at least 50% or at least 60% or at least 75%.It is layered thickness (or other linear rulers of a layer in glass structure
It is very little) after drawing can in the layering glass structure layer thickness (or other linear dimensions) before drawing 0.01% to
In the range of 99% or in the range of 1% to 95% or in the range of 2% to 90% or 5% to 85% scope
It is interior or in the range of 10% to 80% or in the range of 20% to 70% or in the range of 30% to 60%.
In one embodiment, be densified hierarchy has linear dimension along draw direction, and drawing processing makes this
Linear dimension adds at least 5% or adds at least 10% or add at least 25% or add at least 50% or increase
Added at least 100% or add at least 250% or add at least 500% or increasing degree 10%~500% it
Between or increasing degree between 50%~250%, with formed draw densification hierarchy.The densification layering knot of drawing
The linear dimension of structure in the drawing direction can be equivalent to the length of the densification hierarchy of drawing.The densification layering knot of drawing
The length of structure can be more than 0.1m or more than 0.3m or more than 0.5m or more than 1.0m or more than 2.0m or in 0.1m~5.0m
In the range of or the scope in the range of 0.2m~4.0m or in the range of 0.5m~3.5m or in 1.0m~3.0m
It is interior.The densification hierarchy of drawing also has the linear dimension transverse to draw direction.Draw direction can be equivalent to drawing
The length of hierarchy is densified, and can be equivalent to the width of the densification hierarchy of drawing transverse to the direction of draw direction
Degree.Drawing processing can make the linear dimension of densification hierarchy in the drawing direction relative to the densification hierarchy in horizontal stroke
To in the linear dimension increase on the direction of draw direction.The linear dimension of the densification hierarchy of drawing in the drawing direction
With the ratio between the linear dimension of the densification hierarchy of the drawing on the direction transverse to draw direction can be at least 2.0 or
At least 3.0 or at least 5.0 or at least 10 or at least 15 or at least 20 or at least 25.
The densification hierarchy of drawing can be configured to waveguide.Waveguide includes point that can include one or more plane layers
Rotating fields.Waveguiding structure can include two or more plane layers or three or more plane layers.Waveguiding structure can include one
Series layer, these layers limit the stacking being made of two or more waveguides, wherein, each waveguide is stacked comprising an insertion
Core layer between two coverings.Adjacent waveguide stacks the covering that can be shared between each of which core layer, or can be every
One waveguide uses single covering in stacking.Exemplary sequence of layer is included (by putting in order):Covering-core layer-covering-
Core layer-covering ... or covering-core layer-covering-covering-core layer-covering ... or covering-core layer-covering-core
Body layer-covering-core layer-covering-covering-core layer-covering etc..
Waveguide as described herein is characterized in that low attenuation loss, especially relative to the plane wave formed by ceramic material
For leading.Attenuation loss of the waveguide as described herein in 1000nm~1300nm wave-length coverages is less than 0.5dB/m or is less than
0.3dB/m or less than 0.1dB/m or less than 0.05dB/m or less than 0.01dB/m.
In some embodiments, dense glass base material includes plane surface, and the deposition of soot layers occurs in the flat table
On face.Glass can be configured to tablet (such as rectangular or square tablet).Can be by being processed into arbitrary shape comprising flat table
Face forms dense glass base material.In one embodiment, by fibre-optical preform by being cut to the fibre-optical preform
Or mechanical processing is so that it includes plane surface to form dense glass base material.It is known in the art, fibre-optical preform be by with
Made under type:On rod (bait rod) is lured and consolidate soot one or more layers titanium dioxide silicon substrate soot deposit
Tie to form fibre-optical preform.In deposition processes, titanium dioxide silicon substrate soot deposit is lured on rod rotating, is had to be formed
The porous soot body of layering of general cylindrical shape.For formed porous soot body technology include OVD (Outside Vapor deposition),
IVD (inside vapour deposition) and CVD (chemical vapor deposition).The sintering and consolidation for being layered porous soot body can generate densification
Vitreum-fibre-optical preform (by fibre-optical preform come drawing optical fiber).Fibre-optical preform can be by silica or titanium dioxide silicon substrate
Glass is made, and can include the upper different multiple layers of composition, to provide the refractive index curve guided in a fiber needed for light.
The fibre-optical preform of general cylinder can be cut, to form plane surface.In one embodiment, edge
The axially in parallel direction cutting optical fibre prefabricated component with fibre-optical preform to provide plane surface.As described above one or
The subsequent deposition of more soot layers can occur on a planar surface.It can carry out being cut to two or more to fibre-optical preform
Multiple plane surfaces, and soot deposit can occur on one or more in two or more plane surfaces.Two or
Two in more plane surfaces can be parallel.Fibre-optical preform can be carried out being cut to rectangular flat or pros
Shape tablet.
The dense glass base material formed by fibre-optical preform can have single plane surface or multiple plane surfaces.By optical fiber
The dense glass base material that prefabricated component is formed can have one or more plane surfaces and one or more circular surfaces, its
In, soot deposit occurs on one in plane surface.In one embodiment, dense glass base material has two planes
Surface and the circular surface extended between described two plane surfaces.Two plane surfaces can be parallel.
Fig. 4~8 form layering glass structure exemplified with by fibre-optical preform base material.Fig. 4 is shown on handle 105
Fibre-optical preform 100.Handle 105 is removed, and it is carried out to be cut to flat table along the axial direction of fibre-optical preform 100
Face.In the embodiment shown in Fig. 5, fibre-optical preform 100 is cut in half, to provide dense glass base material 110 and cause
Close glass baseplate 120.Dense glass base material 110 and dense glass base material 120 have deposition surface 115 and 125 respectively, and are equipped with
There is handle 130 to be further processed.
In Fig. 6, soot layers are formed on dense glass base material 110.Soot particles 140 are produced by soot generating means 135
And be deposited on deposition surface 115, to form soot layers 145.In the embodiment shown in fig. 6, soot generating means 135 are matched somebody with somebody
It is set to the linear array of multiple burners.In the embodiment shown in fig. 6, dense glass base material is in movement, and soot
Generating means 135 are static.Dense glass base material can be made to cross soot generating means 135 more than 110 times, with formed have it is required
The soot layers of thickness.Soot layers 145 can be further processed.Processing may include dry or adulterate.
Fig. 7 is exemplified with laser sintered.The dense glass base material 110 with soot layers 145 is burnt using laser 155
Knot.Soot layers 145 are changed into sinter layer 150 by laser 155 along the inswept soot layers 145 of arrow direction.Can be by swashing
The power of light device 155 controls sintering temperature, by laser 155 passes through cigarette by the speed or laser 155 of soot layers 145
The number of soot layer 145 controls sintering time.Sinter layer 150 is dense glass layer.
Fig. 8 on sinter layer 150 exemplified with depositing additional soot layers.Dense glass base material 110 is set to cross soot generation
Device 160, it, which is generated, is used to be deposited on sinter layer 150 to form the soot particles 165 of soot layers 170.Soot layers 170 can have
By with sinter layer 150 is identical or different forms.Soot layers 170 can have the group identical or different with dense glass base material 110
Into.In one embodiment, dense glass base material 110 has the composition of waveguide covering, and sinter layer 150 has waveguide cores layer
Composition, and soot layers 170 have waveguide covering composition.After deposition, soot layers 170 can be further processed, such as
Dry, doping or sintering.After soot layers 170 sinter, product is the layering glass for having dense glass base material and two glassy layers
Structure.
Additional treatment steps of the Fig. 9 exemplified with layering glass structure.Layering glass structure is prepared by dense glass base material, institute
Dense glass base material is stated by being formed with the fibre-optical preform that covering forms.Core layer through overdoping is positioned at dense glass base
On material, and covering is positioned on the core layer through overdoping.Show two processing approach.In an approach, glass will be layered
Glass construction machine is processed into the rectangular shape of plane, is then drawn and provides plane wave to adjust the thickness of core and covering
Lead.In Article 2 processing approach, dense glass base material is drawn with linear adjustment size, subsequently optionally carry out machinery
Processing, to form the waveguide of the rectangular shape with plane.
The waveguide formed by layering glass structure can include one or more plane surfaces or two or more planes
Surface or a plane surface and a circular surface.In one embodiment, waveguide includes rectangle core layer and rectangle bag
Layer.In another embodiment, waveguide includes rectangle core layer and the covering with circular surface.In another embodiment
In, waveguide includes rectangle core layer, rectangle covering and the covering with circular surface.
Other processing can be used to form layering glass structure.In one embodiment, divide as already mentioned above
Two or more composite constructions with dense glass base material and one or more soot layers are not prepared, and they are tied
It is combined to form layering glass structure.Layering glass structure can be formed in the following manner:In a predefined order to single
Composite construction is stacked to form stacked structure, and then the stacked structure is sintered and heated, so that these layers fuse
Into an integrated structure.
In Figure 10, make with dense glass base material 210 and the composite construction of soot layers 215 200 and with dense glass base
Material 220 and the composite construction of soot layers 225 205 are combined to form stacked structure.Dense glass base material 210, dense glass base material
220th, the composition of any of soot layers 215 and soot layers 225 may be the same or different.With reference to rear, can to stacked structure into
Row sinters so that soot layers 215 and soot layers 225 consolidate, and fuse to be formed with dense glass base material 210, dense glass
The layer of base material 220 and the layering glass structure 240 of sinter layer 235.Dense glass base material 210 and/or dense glass base material 220 wrap
Embodiment containing two or more soot layers is within the scope of this specification.
Heat fused is carried out to be combined together layer to manufacture integrated structure using heating.Heating can occur in stove or
In flame.Alternatively, laser can be used to be heated.In one embodiment, heating occurs in a vacuum furnace.Vacuum (or
Low pressure) gas of depositing between condition can help to remove gas and will be present in layer is reduced at least.
Figure 11 shows a kind of alternative embodiment, wherein, layering glass structure is combined with composite construction with shape
Into stacked structure.Layering glass structure 305 includes dense glass base material 320 and sinter layer 325.Composite construction 300 includes densification
Glass baseplate 310 and soot layers 315.Dense glass base material 310, dense glass base material 320, soot layers 315 and sinter layer 325
Any of composition may be the same or different.With reference to rear, stacked structure can be sintered so that soot layers 315 consolidate, and
And fuse to form the layering glass structure with dense glass base material 310, the layer of dense glass base material 320 and sinter layer 335
340.Dense glass base material 310 includes the embodiment of two or more soot layers within the scope of this specification, and is layered
Glass structure 305 also includes the embodiment of one or more soot layers also in this specification in addition to sinter layer 325
In the range of.
Figure 12 shows another embodiment, wherein, with reference to two layering glass structures to form stacked structure.Layering
Glass structure 405 includes dense glass base material 420 and sinter layer 425.Layering glass structure 400 includes dense glass base material 410
With sinter layer 415.Any of dense glass base material 410, dense glass base material 420, sinter layer 415 and sinter layer 425
Composition may be the same or different.After layering glass structure 405 is combined with layering glass structure 400, so that it may to stacked structure
Fused to form the layering glass knot with dense glass base material 410, the layer of dense glass base material 420 and sinter layer 435
Structure 440.Dense glass base material 410 and/or dense glass base material 410 also include one in addition to sinter layer 415 or sinter layer 425
The embodiment of a or more soot layers is within the scope of this specification.
In Figure 10~12 illustrated processing may extend to reference to three or more composite constructions, layering glass structure or
Combinations thereof.
In other embodiments, layering glass structure is manufactured or provided in the following manner:Make at least one
Composite construction or layering glass structure described in text are combined to provide heap with least one glassy layer formed by another processing
Stack structure, and the stacked structure is heated to sinter and consolidate any soot layers, and the stacking is fused to form layering glass
Glass structure.Independent solution for manufacturing glassy layer includes OVD (Outside Vapor deposition), IVD (inside vapour deposition) and VAD
(vapor axial deposition) or directly handle.Directly processing includes the powder of hybrid glass component, heats to sinter and consolidate, and
Cool down to form glass.
Figure 13 shows the formation of the glassy layer independently of composite construction or the formation for being layered glass structure.These glassy layers
Formed by OVD methods, wherein, soot preform is formed using conventional treatment (such as flame hydrolysis, flame combustion).Soot
The composition of prefabricated component can be identical or different with the composite construction or any layer of layering glass structure being combined with it.Can be to soot
Prefabricated component is dehydrated (such as using Cl2), sintering and consolidate to form blank.It is known in the art, can to OVD (or IVD or
VAD) temperature of method is controlled, so as to sinter and occur when being fixedly arranged at soot deposit.Alternatively, temperature when making generation soot deposit
Degree keeps below sintering temperature, and can use single sintering step.Blank is cut to form the glass with required size
Layer.Figure 14, which is shown, assembles glassy layer and the composite construction according to this specification or layering glass structure, to form tool
There is the layering glass structure of three layers.The triplex glass structure is then heated to sinter (if desired) and fuse these layers, from
And form waveguide.As shown in figure 14, in one embodiment, the glassy layer formed by independent process can be equivalent to layering glass
The covering (illustrated outermost layer in Figure 14) of structure, and composite construction or layering glass structure (illustrated center in Figure 14
Layer) can be equivalent to the core layer of layering glass structure.
Unless otherwise stated, otherwise all it is not intended to and any means as described herein is interpreted as needing to make its step with specific
Order carries out.Therefore, when claim to a method is practically without being set fourth as that its step follows certain order or it does not exist
Specifically represent that step is limited to specific order with any other modes in claims or specification, be all not intended to imply that this
Meaning particular order.
It will be apparent to those skilled in the art can be in the spirit without departing from illustrated embodiment
Various modifications and changes are carried out to the present invention with the case of scope.Because those skilled in the art is contemplated that illustrated
Various improvement, combination, subitem combination and the change of the fusion of embodiment spirit of the invention and essence, it is considered that present invention bag
Include the full content and its equivalents in scope.
Claims (75)
1. a kind of method for manufacturing planar layer glass structure, the described method includes:
Composite construction is formed, the composite construction includes the first soot layers on dense glass base material, first soot
Layer has at least 100 μm of thickness;
Layering glass structure is prepared by the composite construction, described prepare includes consolidating first soot layers;And
The layering glass structure is drawn along draw direction, to form the layering glass structure drawn, the layering of the drawing
Glass structure in the draw direction with first size and on the direction of the draw direction with the second ruler
Very little, the ratio between the first size and second size are at least 3.0, point of the first soot layers of the consolidation in the drawing
There is at least 10 μm of thickness in layer glass structure.
2. the method as described in claim 1, it is characterised in that first soot layers have at least 250 μm of thickness.
3. the method as described in claim 1, it is characterised in that first soot layers have at least thickness of 1mm.
4. the method as described in claim 1, it is characterised in that first soot layers have at least thickness of 10mm.
5. the method as described in claim 1, it is characterised in that model of the thickness of first soot layers at 100 μm to 10mm
In enclosing.
6. the method as described in claim 1, it is characterised in that scope of the thickness of first soot layers at 150 μm to 4mm
It is interior.
7. the method as described in claim 1, it is characterised in that scope of the thickness of first soot layers at 250 μm to 2mm
It is interior.
8. the method as described in claim 1, it is characterised in that the dense glass base material is formed by fibre-optical preform.
9. method as claimed in claim 8, it is characterised in that the fibre-optical preform has cylindrical shape.
10. method as claimed in claim 8, it is characterised in that the dense glass base material is by handling the optical fiber prefabricating
Part makes that it includes plane surface to be formed.
11. method as claimed in claim 10, it is characterised in that first soot layers are arranged on the plane surface.
12. method as claimed in claim 11, it is characterised in that the fibre-optical preform includes circular surface.
13. the method as described in claim 1, it is characterised in that the dense glass base material includes circular surface and flat table
Face, and first soot layers are arranged on the plane surface.
14. the method as described in claim 1, it is characterised in that it is described consolidation include by first soot layers be heated to
Temperature 1000 DEG C few.
15. method as claimed in claim 14, it is characterised in that the heating includes making first soot layers exposed to sharp
Under light.
16. the method as described in claim 1, it is characterised in that layering of the first soot layers of the consolidation in the drawing
There is at least 100 μm of thickness in glass structure.
17. the method as described in claim 1, it is characterised in that layering of the first soot layers of the consolidation in the drawing
There is at least 500 μm of thickness in glass structure.
18. the method as described in claim 1, it is characterised in that layering of the first soot layers of the consolidation in the drawing
There is at least thickness of 5mm in glass structure.
19. the method as described in claim 1, it is characterised in that layering of the first soot layers of the consolidation in the drawing
There is at least thickness of 15mm in glass structure.
20. the method as described in claim 1, it is characterised in that layering of the first soot layers of the consolidation in the drawing
Thickness in glass structure is in the range of 10 μm to 50mm.
21. the method as described in claim 1, it is characterised in that layering of the first soot layers of the consolidation in the drawing
Thickness in glass structure is in the range of 100 μm to 25mm.
22. the method as described in claim 1, it is characterised in that layering of the first soot layers of the consolidation in the drawing
Thickness in glass structure is in the range of 250 μm to 25mm.
23. the method as described in claim 1, it is characterised in that the first soot layers of the consolidation are at least 1mm2Area in
With the average surface roughness R less than 0.50nma。
24. the method as described in claim 1, it is characterised in that the first soot layers of the consolidation are at least 0.50mm2Face
There is the average surface roughness R less than 0.25nm in producta。
25. the method as described in claim 1, it is characterised in that the first soot layers of the consolidation are at least 0.25mm2Face
There is the average surface roughness R less than 0.10nm in producta。
26. the method as described in claim 1, it is characterised in that the drawing makes the linear dimension of the layering glass structure
Add at least 25%.
27. the method as described in claim 1, it is characterised in that the drawing makes the linear dimension of the layering glass structure
Add at least 100%.
28. the method as described in claim 1, it is characterised in that the drawing makes the linear dimension of the layering glass structure
Add 10%~500%.
29. the method as described in claim 1, it is characterised in that the drawing makes the linear dimension of the layering glass structure
Add 50%~250%.
30. the method as described in claim 1, it is characterised in that the layering glass structure of the drawing has at least 0.1m's
Length.
31. the method as described in claim 1, it is characterised in that the layering glass structure of the drawing has at least 0.3m's
Length.
32. the method as described in claim 1, it is characterised in that the layering glass structure of the drawing has at least 1.0m's
Length.
33. the method as described in claim 1, it is characterised in that the drawing layering glass structure length 0.1m~
In the range of 5.0m.
34. the method as described in claim 1, it is characterised in that the drawing layering glass structure length 0.2m~
In the range of 4.0m.
35. the method as described in claim 1, it is characterised in that the drawing layering glass structure length 1.0m~
In the range of 3.0m.
36. the method as described in claim 1, it is characterised in that the ratio between the first size and second size are at least
5.0。
37. the method as described in claim 1, it is characterised in that the ratio between the first size and second size are at least
10。
38. the method as described in claim 1, it is characterised in that the layering glass structure of the drawing 1000nm~
There is the decay less than 0.5dB/m in the wave-length coverage of 1300nm.
39. the method as described in claim 1, it is characterised in that the layering glass structure of the drawing 1000nm~
There is the decay less than 0.1dB/m in the wave-length coverage of 1300nm.
40. the method as described in claim 1, it is characterised in that the layering glass structure of the drawing 1000nm~
There is the decay less than 0.05dB/m in the wave-length coverage of 1300nm.
41. the method as described in claim 1, it is characterised in that the dense glass base material includes silica based glasses.
42. method as claimed in claim 41, it is characterised in that first soot layers include the titanium dioxide containing dopant
Silicon-based glass.
43. method as claimed in claim 42, it is characterised in that the dopant includes rare earth element.
44. method as claimed in claim 43, it is characterised in that the silica based glasses containing dopant include
Al, Ge or Ti.
45. method as claimed in claim 44, it is characterised in that the dense glass base material includes pure silicon dioxide glass.
46. the method as described in claim 1, it is characterised in that the composite construction also includes straight with first soot layers
Second soot layers of contact, second soot layers have at least 100 μm of thickness.
47. method as claimed in claim 46, it is characterised in that second soot layers have at least thickness of 1mm.
48. method as claimed in claim 46, it is characterised in that first soot layers have than second soot layers more
High refractive index.
49. method as claimed in claim 48, it is characterised in that first soot layers have than the dense glass base material
The refractive index of higher.
50. method as claimed in claim 46, it is characterised in that the preparation, which further includes, consolidates second soot layers.
51. method as claimed in claim 50, it is characterised in that layering of the second soot layers of the consolidation in the drawing
There is at least 25 μm of thickness in glass structure.
52. method as claimed in claim 51, it is characterised in that the second soot layers of the consolidation have and the fine and close glass
The identical composition of glass base material and the composition different from first soot layers.
53. method as claimed in claim 52, it is characterised in that second soot layers include silica based glasses, and
First soot layers include the silica based glasses containing dopant.
54. method as claimed in claim 46, it is characterised in that the composite construction also includes straight with second soot layers
3rd soot layers of contact.
55. method as claimed in claim 54, it is characterised in that second soot layers have than first soot layers and
The refractive index of the 3rd soot layers higher.
56. method as claimed in claim 46, it is characterised in that the composite construction is also included and connect with the 3rd soot layers
Tactile one or more soot layers.
57. the method as described in claim 1, it is characterised in that the composite construction also includes the second soot layers, and described second
Soot layers are arranged on the dense glass base material surface opposite with first soot layers.
58. the method as described in claim 1, it is characterised in that described to prepare the first soot layers for being additionally included in the consolidation
The second soot layers of upper formation.
59. method as claimed in claim 58, it is characterised in that the preparation, which further includes, consolidates second soot layers.
60. method as claimed in claim 59, it is characterised in that also include forming the in the second soot layers of the consolidation
Three soot layers.
61. method as claimed in claim 58, it is characterised in that also include forming the 3rd soot in second soot layers
Layer.
62. the method as described in claim 1, it is characterised in that the layering glass structure of the drawing has plane configuration.
63. a kind of method for manufacturing layering glass structure, the described method includes:
The first composite construction is formed, first composite construction includes the first soot layers on the first dense glass base material,
First soot layers have at least 100 μm of thickness;
The second composite construction is formed, second composite construction includes the second soot layers on the second dense glass base material,
Second soot layers have at least 100 μm of thickness;
Stacked structure is formed by stacking first composite construction and second composite construction, described stack includes making institute
The first soot layers are stated to contact with second soot layers.
64. the method as described in claim 63, it is characterised in that further including consolidates the stacked structure.
65. a kind of method for manufacturing layering glass structure, the described method includes:
The first composite construction is formed, first composite construction includes the first soot layers on the first dense glass base material,
First soot layers have at least 100 μm of thickness;
Consolidate first composite construction, the consolidation includes consolidating first soot layers;
The second composite construction is formed, second composite construction includes the second soot layers on the second dense glass base material,
Second soot layers have at least 100 μm of thickness;
Stacked structure is formed by the first composite construction and second composite construction that stack the consolidation, it is described stack bag
Including makes the first soot layers of the consolidation be contacted with second soot layers.
66. the method as described in claim 65, it is characterised in that further including consolidates the stacked structure.
67. a kind of method for manufacturing layering glass structure, the described method includes:
The first composite construction is formed, first composite construction includes the first soot layers on the first dense glass base material,
First soot layers have at least 100 μm of thickness;
Stacked structure is formed by stacking glassy layer in first soot layers.
68. the method as described in claim 67, it is characterised in that further including consolidates the stacked structure.
69. a kind of waveguide, it includes:
First covering;
Core layer on first covering;And
The second covering on the core layer;
Wherein, at least one of first covering, the core layer and described second covering are configured to plane layer, described flat
Surface layer has at least length of 0.1m;And
Wherein, the waveguide has the decay less than 0.5dB/m in the wave-length coverage of 1000nm~1300nm.
70. the waveguide as described in claim 69, it is characterised in that the plane layer has at least length of 0.5m.
71. the waveguide as described in claim 69, it is characterised in that the plane layer has at least length of 1.0m.
72. the waveguide as described in claim 69, it is characterised in that scope of the length of the plane layer in 0.1m~5.0m
It is interior.
73. the waveguide as described in claim 69, it is characterised in that the waveguide is in the wave-length coverage of 1000nm~1300nm
With the decay less than 0.1dB/m.
74. the waveguide as described in claim 69, it is characterised in that the plane layer is the core layer.
75. the waveguide as described in claim 69, it is characterised in that first covering, the core layer and second bag
At least two in layer are configured to the plane layer that length is at least 0.1m.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201562207992P | 2015-08-21 | 2015-08-21 | |
US62/207,992 | 2015-08-21 | ||
PCT/US2016/047478 WO2017034904A1 (en) | 2015-08-21 | 2016-08-18 | Layered glass structures |
Publications (1)
Publication Number | Publication Date |
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CN107922235A true CN107922235A (en) | 2018-04-17 |
Family
ID=56801846
Family Applications (1)
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CN201680048713.2A Withdrawn CN107922235A (en) | 2015-08-21 | 2016-08-18 | It is layered glass structure |
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EP (1) | EP3337768A1 (en) |
JP (1) | JP2018531863A (en) |
CN (1) | CN107922235A (en) |
WO (1) | WO2017034904A1 (en) |
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US10574021B2 (en) | 2016-05-13 | 2020-02-25 | Corning Incorporated | Optical tube waveguide lasing medium and related method |
JP7369573B2 (en) * | 2019-09-13 | 2023-10-26 | 信越石英株式会社 | Method for manufacturing reflective members and glass laminated members |
WO2021095917A1 (en) * | 2019-11-13 | 2021-05-20 | 엘지전자 주식회사 | Composite glass for communication and method for producing same |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5125946A (en) * | 1990-12-10 | 1992-06-30 | Corning Incorporated | Manufacturing method for planar optical waveguides |
DE4418401C1 (en) * | 1994-05-26 | 1995-06-01 | Heraeus Quarzglas | Continuous quartz glass plate mfr. |
DE69512690T2 (en) * | 1994-09-23 | 2000-06-08 | British Telecommunications P.L.C., London | Method of making a planar waveguide |
CA2352378C (en) * | 2000-08-29 | 2005-05-10 | Lucent Technologies Inc. | Chalcogenide glass based raman optical amplifier |
US6606883B2 (en) * | 2001-04-27 | 2003-08-19 | Corning Incorporated | Method for producing fused silica and doped fused silica glass |
US6792187B2 (en) * | 2002-12-17 | 2004-09-14 | Corning Incorporated | Ca-Al-Si oxide glasses and optical components containing the same |
DE102004054392A1 (en) * | 2004-08-28 | 2006-03-02 | Heraeus Quarzglas Gmbh & Co. Kg | Method for joining components made of high-siliceous material, as well as assembled from such components component composite |
DE102006059779B4 (en) * | 2006-12-15 | 2010-06-24 | Heraeus Quarzglas Gmbh & Co. Kg | A method of producing a synthetic quartz hollow cylinder, a thick-walled hollow cylinder obtained by the method, and a method of producing an optical fiber preform |
WO2011139659A1 (en) * | 2010-04-27 | 2011-11-10 | Soreq Nuclear Research Center | Optical waveguide fabrication |
-
2016
- 2016-08-18 WO PCT/US2016/047478 patent/WO2017034904A1/en active Application Filing
- 2016-08-18 EP EP16757461.5A patent/EP3337768A1/en not_active Withdrawn
- 2016-08-18 CN CN201680048713.2A patent/CN107922235A/en not_active Withdrawn
- 2016-08-18 JP JP2018508761A patent/JP2018531863A/en active Pending
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JP2018531863A (en) | 2018-11-01 |
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