GB2518420A - Hollow-core photonic bandgap fibers and methods of manufacturing the same - Google Patents

Hollow-core photonic bandgap fibers and methods of manufacturing the same Download PDF

Info

Publication number
GB2518420A
GB2518420A GB1316795.2A GB201316795A GB2518420A GB 2518420 A GB2518420 A GB 2518420A GB 201316795 A GB201316795 A GB 201316795A GB 2518420 A GB2518420 A GB 2518420A
Authority
GB
United Kingdom
Prior art keywords
core
capillaries
corner
fiber
stack
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB1316795.2A
Other versions
GB201316795D0 (en
GB2518420B (en
Inventor
Eric Rodrigue Numkam Fokoua
Francesco Poletti
David John Richardson
Yong Chen
Natalie Violet Wheeler
John Richard Hayes
Marco Petrovich
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
University of Southampton
Original Assignee
University of Southampton
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to GB1316795.2A priority Critical patent/GB2518420B/en
Application filed by University of Southampton filed Critical University of Southampton
Priority to GB1813894.1A priority patent/GB2562687B/en
Priority to GB1813895.8A priority patent/GB2562688B/en
Publication of GB201316795D0 publication Critical patent/GB201316795D0/en
Priority to US15/023,541 priority patent/US11034607B2/en
Priority to PCT/EP2014/070048 priority patent/WO2015040189A2/en
Priority to EP14771866.2A priority patent/EP3047319B8/en
Priority to DK14771866.2T priority patent/DK3047319T3/en
Publication of GB2518420A publication Critical patent/GB2518420A/en
Application granted granted Critical
Publication of GB2518420B publication Critical patent/GB2518420B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/02Optical fibres with cladding with or without a coating
    • G02B6/02295Microstructured optical fibre
    • G02B6/02314Plurality of longitudinal structures extending along optical fibre axis, e.g. holes
    • G02B6/02342Plurality of longitudinal structures extending along optical fibre axis, e.g. holes characterised by cladding features, i.e. light confining region
    • G02B6/02347Longitudinal structures arranged to form a regular periodic lattice, e.g. triangular, square, honeycomb unit cell repeated throughout cladding
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B37/00Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
    • C03B37/01Manufacture of glass fibres or filaments
    • C03B37/012Manufacture of preforms for drawing fibres or filaments
    • C03B37/01205Manufacture of preforms for drawing fibres or filaments starting from tubes, rods, fibres or filaments
    • C03B37/01208Manufacture of preforms for drawing fibres or filaments starting from tubes, rods, fibres or filaments for making preforms of microstructured, photonic crystal or holey optical fibres
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B37/00Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
    • C03B37/01Manufacture of glass fibres or filaments
    • C03B37/012Manufacture of preforms for drawing fibres or filaments
    • C03B37/01205Manufacture of preforms for drawing fibres or filaments starting from tubes, rods, fibres or filaments
    • C03B37/01211Manufacture of preforms for drawing fibres or filaments starting from tubes, rods, fibres or filaments by inserting one or more rods or tubes into a tube
    • C03B37/0122Manufacture of preforms for drawing fibres or filaments starting from tubes, rods, fibres or filaments by inserting one or more rods or tubes into a tube for making preforms of photonic crystal, microstructured or holey optical fibres
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B37/00Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
    • C03B37/01Manufacture of glass fibres or filaments
    • C03B37/02Manufacture of glass fibres or filaments by drawing or extruding, e.g. direct drawing of molten glass from nozzles; Cooling fins therefor
    • C03B37/025Manufacture of glass fibres or filaments by drawing or extruding, e.g. direct drawing of molten glass from nozzles; Cooling fins therefor from reheated softened tubes, rods, fibres or filaments, e.g. drawing fibres from preforms
    • C03B37/027Fibres composed of different sorts of glass, e.g. glass optical fibres
    • C03B37/02781Hollow fibres, e.g. holey fibres
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/02Optical fibres with cladding with or without a coating
    • G02B6/02295Microstructured optical fibre
    • G02B6/02314Plurality of longitudinal structures extending along optical fibre axis, e.g. holes
    • G02B6/02319Plurality of longitudinal structures extending along optical fibre axis, e.g. holes characterised by core or core-cladding interface features
    • G02B6/02323Core having lower refractive index than cladding, e.g. photonic band gap guiding
    • G02B6/02328Hollow or gas filled core
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/02Optical fibres with cladding with or without a coating
    • G02B6/02295Microstructured optical fibre
    • G02B6/02314Plurality of longitudinal structures extending along optical fibre axis, e.g. holes
    • G02B6/02342Plurality of longitudinal structures extending along optical fibre axis, e.g. holes characterised by cladding features, i.e. light confining region
    • G02B6/02357Property of longitudinal structures or background material varies radially and/or azimuthally in the cladding, e.g. size, spacing, periodicity, shape, refractive index, graded index, quasiperiodic, quasicrystals
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/02Optical fibres with cladding with or without a coating
    • G02B6/02295Microstructured optical fibre
    • G02B6/02314Plurality of longitudinal structures extending along optical fibre axis, e.g. holes
    • G02B6/02342Plurality of longitudinal structures extending along optical fibre axis, e.g. holes characterised by cladding features, i.e. light confining region
    • G02B6/02371Cross section of longitudinal structures is non-circular
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2201/00Type of glass produced
    • C03B2201/06Doped silica-based glasses
    • C03B2201/08Doped silica-based glasses doped with boron or fluorine or other refractive index decreasing dopant
    • C03B2201/10Doped silica-based glasses doped with boron or fluorine or other refractive index decreasing dopant doped with boron
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2201/00Type of glass produced
    • C03B2201/06Doped silica-based glasses
    • C03B2201/08Doped silica-based glasses doped with boron or fluorine or other refractive index decreasing dopant
    • C03B2201/12Doped silica-based glasses doped with boron or fluorine or other refractive index decreasing dopant doped with fluorine
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2201/00Type of glass produced
    • C03B2201/06Doped silica-based glasses
    • C03B2201/20Doped silica-based glasses doped with non-metals other than boron or fluorine
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2201/00Type of glass produced
    • C03B2201/06Doped silica-based glasses
    • C03B2201/20Doped silica-based glasses doped with non-metals other than boron or fluorine
    • C03B2201/28Doped silica-based glasses doped with non-metals other than boron or fluorine doped with phosphorus
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2201/00Type of glass produced
    • C03B2201/06Doped silica-based glasses
    • C03B2201/30Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
    • C03B2201/40Doped 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
    • C03B2201/42Doped 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
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2201/00Type of glass produced
    • C03B2201/06Doped silica-based glasses
    • C03B2201/30Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi
    • C03B2201/50Doped silica-based glasses doped with metals, e.g. Ga, Sn, Sb, Pb or Bi doped with alkali metals
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2203/00Fibre product details, e.g. structure, shape
    • C03B2203/10Internal structure or shape details
    • C03B2203/14Non-solid, i.e. hollow products, e.g. hollow clad or with core-clad interface
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2203/00Fibre product details, e.g. structure, shape
    • C03B2203/10Internal structure or shape details
    • C03B2203/14Non-solid, i.e. hollow products, e.g. hollow clad or with core-clad interface
    • C03B2203/16Hollow core
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2203/00Fibre product details, e.g. structure, shape
    • C03B2203/10Internal structure or shape details
    • C03B2203/22Radial profile of refractive index, composition or softening point
    • C03B2203/222Mismatching viscosities or softening points of glass layers
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2203/00Fibre product details, e.g. structure, shape
    • C03B2203/42Photonic crystal fibres, e.g. fibres using the photonic bandgap PBG effect, microstructured or holey optical fibres
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B2205/00Fibre drawing or extruding details
    • C03B2205/10Fibre drawing or extruding details pressurised

Landscapes

  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Optical Fibers, Optical Fiber Cores, And Optical Fiber Bundles (AREA)

Abstract

A method of fabricating a hollow-core photonic-bandgap fiber having a stack of capillaries, with a hollow core 205 and the capillaries at a boundary of the core comprise a plurality of corner core capillaries 203 and a plurality of intermediate core capillaries 203, where the corner core capillaries 203 have a non-circular cross section, and optionally an elongate cross section. The stack is reduced to a fiber with a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts (109, fig 2) and interstitial nodes which together define an array of cavities (115, fig 2). Numerous other related inventions are disclosed.

Description

FIBERS AND J4ETHODSOF
MANUFACTURING THE SAME
The present invention relates to hoHowcore photonic bandgap fibers (HC-PBGFs), for example, for application in data transmission and high-power laser pulse delivery, and methods of manufacturing the same.
As iflustrated in Figure 1, HC-PBGFs comprise an elongate fiber body having a hoUow core 3 and a cladding S which surrounds the core 3 at a boundary 7 and comprises a silica lattice of relatively-thin struts 9 and relatively-large intersdtial nodes 11, which together define an array of air holes of cavities which are arranged in packed relation around the core 3, with. the core 3 being formed by omitting a number of capiflaries at the center of the structure. Figure 1 iflustrates a phor art HC-PBGF design which is considered to be most optimized or deal, in preserving a perfect cladding periodicity of nodes 11' at the boundary 7 of the core 3 and the cladding 5.
It is the optical resonance properties of these nodes that primarily determine the photonic bandgap or range of optical frequencies over which light can be effectively confined and guided within the core.
It is desirabie in many apphcations to achieve a wide photonic bandgap over which light can be guided with low loss. The termination of the microstructured cladding around the core forms a continuous boundary which consists of nodes interconnected by struts. As loss is predominantly dictated by the overlap of the guided-mode field with this boundary through scattering at the air-glass interfaces, optimizing its configuration is important in loss reduction.
Owing to recent progress in the development of HC-PBGFs, these fibers are now emerging as a credible alternative to the all-solid optical fibers as used in telecom applications [1, 2]. Indeed, the highly-desirable features of low-H latency, ultralow nonlinearity and potentially lower transmission loss make these fibers suitable for next generation data-carrying fibers. However, the attenuation levels which are fundamentally limited by scattering from surface roughness have yet to be reduced to theoretically predicted levels [3-4].
Numerous efforts in loss reduction have aimed at optimizing the fiber design to reduce the overlap of the guided-mode field with the scattering surfaces.
Notably, the introduction of an anti-resonant core surround has led to the lowest reported loss value of 1.7 dB/km [5]. However, the resulting "thick" core supports a multitude of surface modes within the photonic bandgap, which restrict the usable bandwidth.
It has also been demonstrated that, for fibers with a seven cell (7c) core defect, making the core wall half as thin as the struts in the claddIng eliminates surface modes, thereby Increasing the operational bandwidth [8-10].
In an attempt to expand the usable bandwidth and further reduce loss in fibers with larger core defects, a number of recently-reported HC-PBGFs have been produced without a core tube. ThIs fabrication procedure has, however, resulted in more promInent structural dIstortions, notably, more enlarged core defects, Including oversized air holes on the six "corners" around the core and compressed ciaddings with different perlodicity along the main symmetry axes [1, 2, 11].
Significant theoretical efforts have already been devoted to understanding and predicting the attenuation that could be obtained from a given HC-PBGF design. This work has, however, either neglected the scattering loss contribution, and hence considerably underestimated the total loss, or considered only "ideal" structures with perfectly periodic lattices, which are visibly dIfferent from fabricated lattices [12].
Another strand of activity has focused on modeling fiber geometries obtained from scanning electron mlcrographs of fabricated fibers; however, instrument resolution imposes a constraint on the accuracy of such studies (13, 14]. For a full fiber cross-section, the width of a single glass strut is only a few pixels wide, making it difficult for edge-detection routines to determine accurately the boundaries of the cladding air holes, and even more so to estimate thickness and impact of the metallic coating necessary to acquire the images. Good quantitative agreement between measured and simulated modal properties, such as dispersion and mode-field diameter of current commercial KC-PBGFs, has been obtained using this approach, although any reasonable comparison of loss values is foregone by the omission of part of the cladding [15]. *
Contrary to the common understanding In the art, the present Inventors have recognized that an exact periodicity in the cladding is not a strict requirement for air-guidance. From this recognition, the present inventors have devised Improved fiber designs which are less susceptible to surface-mode induced bandwidth degradation, exhibit a considerable reduction in loss and advantageously allow the core wall thickness to be increased.
In one aspect the present invention provides a method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the corner core capillaries have a non-circular section, and optionally an elongated section; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In another aspect the present invention provides a method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the corner core capillaries include an additional mass segment at a surface thereof which is arranged to face the core between adjacent intermediate core capillaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and Interstitial nodes which together define an array of cavities.
In a further aspect the present invention provides a method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the intermediate core capillaries Include a reduced mass segment at a surface thereof which is arranged to face the core; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In a still further aspect the present invention provides a method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillarIes about a core tube, wherein the stack has a hollow core as defined by the core tube and the capillaries at a boundary of the core tube comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the core tube includes additional mass segments at a surface thereof in correspondence to the positIons of the corner core capillaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In a yet further aspect the present invention provides a method of fabhcating a hoHowcore photonic-bandgap fiber, comprising the steps of; providing a stack of capiflaries about a core tube, wherein the stack has a hoflow core as defined by the core tube and the capiUaries at a boundary of the core tube compnse a plurality of first, corner core capiflaries and a plurality of second, intermediate core capillaries, wherein the core tube is hexagonal in section which provides six planar side members, adjacent ones of which meet at corner junctions, which correspond in position to the corner core capillaries; and reducing the stack to a fiber, wherein the fiber has a holiow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In still another aspect the present invention provides a method of fabricating a hollow-core photonic-handgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capHlar!es, wherein the corner core capillaries have a substantially hexagonal outer section, and the intermediate core capillaries have a substantially frusto-hexagonal outer section; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In yet another aspect the present invention provides a method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of; providing a stack of capillaries, wherein the stack has a hollow core and the capfliaries at a boundary of core are located on a circle of predetermined diameter, about which outer, cladding capillaries are packed; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In a yet further aspect the present invention provides a method of fabricating a hollow-core photonlc-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries; applying a pressure differential between the corner core capillaries and the intermediate core capillaries, whereby a size of the corner core capillaries can be controlled In relation to the intermediate core capillaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In still another aspect the present invention provides a method of fabricating a hollow-core photonlc-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the corner core capillaries are formed of a material having a higher viscosity at a fiber drawing temperature than a material of the intermediate core capillarIes, whereby a size of the corner core capillaries can be regulated in relation to the intermediate core caplilaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In yet another aspect the present invention provides a method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein additional mass segments are located at unfilled junctions between the core capillaries, whereby the mass of the additional mass segments supplements the mass of the corner core capillaries in relation to the intermediate core capillaries, and also supplements the mass at the core boundary; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In a still further aspect the present Invention provides a method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a core former; providing a stack of capillaries to the core former, wherein the stack has a hoilow core as defined by the core former, and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the core capillaries, and optionally outer, cladding capillaries, are sealed such that each has an enciosed volume; providing the stack of capiliarles In a mold; heating the stack of capillaries, whereby the core capillaries expand and fill voids at the surface of the core former; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.
In a yet still further aspect the present invention provides a pre-form stack for use in the fabrication of a hollow-core photonic-bandgap fiber in accordance with any of the above-described methods.
By providing that the nodes at the core boundary are substantially equi-spaced, the modal overlap with the scattering surfaces, and hence fiber loss, is minimized.
In addition, providing the core boundary with nearly equidistant nodes Is effective In eliminating surface modes, without causing significant bandwidth or loss penalty, even in fibers with a thickened core wall or which incorporate a core tube, which can present advantages in fabrication.
With the present invention, it is predicted that for a fiber with a nineteen cell (19c) core defect, in an optimum configuration, losses can be reduced to less than 0.5 dB/km at a wavelength of 1.55 pm over a 450 nm bandwidth, with It being possible to reduce loss further, for example, by a factor greater than 2 by operating at a wavelength of 2 pm or by more than 2.7 times using a fiber with a thirty-seven cell (37c) or greater core defect.
Furthermore, for laser delivery applications, dispersion engineering is easily achieved through control of the size of the core nodes.
Preferred embodiments of the present invention will now be described hereinbelow by way of example oniy with reference to the accompanying drawings, in which: Figure 1 illustrates a lateral cross-section through an "Ideal" I-IC-PBGF in
accordance with the prior art;
Figure 2 Illustrates a lateral cross-section through a HC-PBGF in accordance with a first embodiment of the present invention; Figure 3 illustrates a lateral cross-section through a HC-PBGF In accordance with a second embodiment of the present invention; Figure 4 Illustrates plots of the simulated losses for the "ideal" fiber of Figure 1, the fiber of Figure 2 and the fiber of Figure 3; Figure 5 illustrates a plot of the simulated loss as a function of core diameter for the fiber of Figure 3; FIgure 6 illustrates a plot of the simulated loss of the fiber of Figure 3 as a function of a ratio of the thickness (ta) of the struts to the average spacing of the nodes; Figure 7 illustrates plots of the simulated loss of the fiber of Figure 3 as a function of a ratio of the area of the struts to the area of the nodes; Figure 8 illustrates plots of the simulated loss as a function of cladding thickness for the fiber of Figure 3; FIgure 9 Illustrates plots of the simulated loss as a function of the size of the "corner" cavities for the fiber of Figure 3 and the "Ideal" fiber of Figure 1; Figures 10(a) and (b) illustrate contour plots of the average power flow in the z-direction from Fibers Bi and B6, respectively, of the fiber of Figure 3; Figure 11 illustrates plots of the simulated loss as a function or core wall thickness for fibers In accordance with the embodiment of Figure 3, where each having equi-spaced core nodes and having no core tube and core tubes of the same thickness as the capillaries in the starting stack and 1.25 times the thickness of the capillaries in the staffing stack; Figure 12 illustrates plots of loss as a function or core wall thickness for fibers in accordance with the embodiment of Figure 3, where each having oversized "corner" cavities and having no core tube and core tubes of the same thickness as the capillaries in the starting stack and 1.25 times the thickness of the capillaries in the starting stack; Figure 13(a) illustrates plots of the simulated dispersion for fibers In accordance with the embodiment of Figure 3, having increasing node sizes at the core boundary; -10 -Figure 13(b) illustrates plots of the simulated loss as a function of node size, corresponding to Figure 13(a); Figures 14(a) to (g) illustrate a conventional fabrication method for the fabrication of HC-PBGFs; Figures 15(a) and (b) illustrate a fabrication method for fabricating HC-PBGFs in accordance with a first embodiment of the present Invention; Figure 16 illustrates a modified stack for use In the method of Figures 15(a) and (b); Figure 17 illustrates another modified stack for use in the method of Figures 15(a) and (b); Figure 18 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a second embodiment of the present invention; Figure 19 illustrates a modified stack for use in the method of Figure 18; Figure 20 illustrates another modified stack for use In the method of Figure 18; Figure 21 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a third embodiment of the present invention; Figure 22 illustrates a fabricatIon method for fabricating HC-PBGFs in accordance with a fourth embodiment of the present invention; Figure 23 illustrates a modified core tube for use in the method of Figure 22; -11 -Figure 24 illustrates another modified core tube for use in the method of FIgure 22; FIgure 25 Illustrates a method of fabricating the core tube of Figure 24; Figures 26(a) to (c) Illustrate modified stacks for use In the method of Figure 22; Figure 27 illustrates a fabrication method for fabricatIng HC-PBGFs in accordance with a fifth embodiment of the present Invention; Figure 28 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a sixth embodiment of the present invention; Figure 29 illustrates a modified stack for use in the method of Figure 28; Figures 30(a) and (b) illustrate a fabrication method for fabricating HC-PBGFs in accordance with a seventh embodiment of the present invention; Figure 31 Illustrates a modified stack for use in the method of Figures 30(a) and (b); Figure 32 illustrates a fabrication method for fabricating HC-PBGFs in accordance with an eighth embodiment of the present Invention; Figure 33 illustrates a fabrication method for fabricating HC-PBGFs In accordance with a ninth embodiment of the present Invention; Figure 34 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a tenth embodiment of the present InventIon; and Figure 35 illustrates a fabrication method for fabricating HC-PBGFs In accordance with an eleventh embodiment of the present invention.
-12 -In the present embodiments the fiber loss accounts for contributions from both leakage (or confinement) loss and scattering from surface roughness.
The latter Is known to impose a fundamental limit on the achievable attenuation in HC-PBGFs, and as recently shown, is the major loss contribution in fibers with.dB/km loss levels with six or more rings of air holes outside the core defect [3, 4]. For computation purposes, but without loss of generality, the scattering loss is computed here not by the rigorous treatment formulated in (4], but through the simplified method of calculating the normalized interface field intensity of the fiber on the air-glass interfaces (3]: tfr J ff1.?;' 1144 where E and H are the electric and magnetic field vectors of the fundamental mode. In addition, the scattering loss is calibrated by comparing multiple measurements and simulations so that a loss value of 3.5 dB/km around a wavelength of 1.5 pm corresponds to an interface field intensity (F) of 0.Oll6pm'.
Figure 2 illustrates a HC-PBGF in accordance with a first embodiment of the present invention.
The HC-PBGF comprises an elongate fiber body having a hollow core 103 and a cladding 105 which surrounds the core 103 at a boundary 107.
In this embodiment the core 103 is gas filled, here air filled. In other embodiments the core 103 could be filled with any of argon, xeon, helium or hydrogen.
In an alternative embodiment the core 103 could be a vacuum.
-13 -In another alternative embodiment the core 103 could contain a liquid.
In this embodiment the core 103 is substantIally circular in section.
The cladding 105 comprIses a lattice or network 108 of struts 109, 109' and Interstitial nodes 111, 111', whIch together define a plurality of cavities 115, in this embodiment extending along the length of the fiber body, which are arranged in packed relation around the core 103.
In this embodiment the network 108 is formed of glass, such as silicate glasses, fluoride glasses, telluride glasses or chaicogenicide glasses.
In an alternative embodiment the network 108 could be formed of a polymer.
In one embodiment different materials, glasses or polymers, may be used in the cladding 105 for an inner region at the core boundary 107 and for an outer region.
In one embodiment different materials, glasses or polymers, can be used in regions across the cross-section of the cladding 105.
In this embodiment the cavities 115 comprIse gas-filled holes, here air-filed holes. In other embodiments the cavities 115 could be filled with any of argon, xeon, helium or hydrogen.
In an alternatIve embodiment the cavities 115 could be a vacuum.
In another alternative embodiment the cavities 115 could contain a liquid.
In this embodiment the cavities 115 are arranged in triangular-packed relation. -14
In alternative embodIments the cavities 115 could be packed in other relation, such as square-packed or hexagonal-packed.
In this embodiment the struts 109' at the core boundary 107 have substantially equal length, and the nodes 111' at the core boundary 107 are substantially equi-spaced at a pitch p. The present Inventors have established that surprisingly, and contrary to the understanding in the art which requires an exact periodicity of the structure of the cladding 103, as illustrated in the "ideal" fiber of Figure 1, by arranging the core struts 109' to have substantially equal length and the core nodes 111' to be substantially equl-spaced, there is a significant reduction in fiber loss over a much broader operational bandwidth. As Illustrated in Figure 4, the loss value is about 40% lower than the loss seen In the "ideal" fiber of FIgure 1.
The present inventors postulate that the broader operational bandwidth is provided by improved uniformity of the core struts 109' in terms of length and mass, arising from equi-spacing of the core nodes 111', and that the reduction in fiber loss arises as a result of the field being equally prevented from overlapping each of the core struts 109'.
In one embodiment the core nodes 111' have substantially the same size as the nodes 111 withIn the body of the cladding 105 which arrangement yields the lowest fiber loss.
In this embodiment the core struts 109' have an average thickness (t) of about 23 nm, the cladding struts 109 have an average thickness (to) of 47 nm, the average cladding node area Is 0.47 pm2 and the overall effective fiber diameter (DcIdhQ) Is 80 pm, which are the same as for the ideal" fiber of Figure 1.
-15 -In this embodiment the fiber Is a nineteen cell (19c) fiber, having an effective core diameter of 5A, where A Is the average spacing of the cavities 115, which is the same size as the "ideal" fiber of Figure 1.
In an alternative embodiment the fiber could have a different core size, for example, a thirty-seven cell (37c) fiber, having an effective core diameter of 7A, or a sixty-one cell (61c) having an effective core diameter of 9A.
FIgure 3 Illustrates a fiber In accordance with a second embodiment of the present invention.
The fiber of this embodiment is quite similar to the fiber of the first-described embodiment, and thus, in order to avoid unnecessary duplication of description, only the differences will be described in detail, with like parts being designated by like reference signs.
In this embodiment the fiber has an enlarged core 103 as compared both to the "Ideal" fiber of Figure 1 and the fiber of the first-described embodiment.
In this embodiment the core 103 has an effective diameter of 1.26 times greater than that of the "ideal" fiber of Figure 1, where the effective diameter is nit, here 5A, and where A is 4.4 pm In one embodiment the average cavity spacing A is from about 3 pm to about 6 pm In fibers operating at a wavelength of 1.55 pm.
In another embodiment the average cavIty spacing A is from about 4 pm to about 8 pm in fibers operating at the minimum loss wavelength of 2 pm.
As Illustrated in Figure 4, the reduction in fiber loss, as compared to the ideal" fiber of Figure 1, is further reduced in relation to the first-described embodiment, here by a factor as high as 2.4 over the entire transmission bandwidth.
-16 -Figure 5 illustrates a plot of the simulated loss as a function of core diameter for the fiber of Figure 3. As will be seen, the fiber of this embodiment has an optimum core diameter ratio of from about 1.05 to about 1.35 nA, preferably from about 1.05 nA, stiil preferably from about 1.1 to about 1.35 nA, and more preferably from about 1.15 to about 1.30 nA.
In addition, as illustrated in Figure 6, which illustrates the simulated loss for the fiber of Figure 3 as a function of a ratio of the average thickness (ta) of the struts 109 to the average spacing of the nodes 111, the present invention allows for reduction of loss by optimizing the thickness (ta) of the struts 109 in relation to the spacing of the nodes 111. In the present invention, loss is minimized by providing that the ratio of the average thickness (tj of the struts 109 to the average spacing of the nodes 111 is less than about 5%, and optionally less than about 2%.
Furthermore, as illustrated in Figure 7, which illustrates plots of the simulated loss for the fiber of Figure 3 as a function of a ratio of the average area of the struts 109 to the average area of the nodes 111, the present invention allows for reduction of loss by optimizing the area of the struts 109 in relation to the area of the nodes 111; the various plots being for fibers having a ratio of the average thickness (ta) of the struts 109 to the average spacing of the nodes 111 in the range of from 1.7% to 8.6%.
For the purposes of calculation, the area of each strut 109 is the area over which the strut 109 has a substantially uniform thickness, and the area of each node 111 is the area enclosed between three adjoining struts 109 of substantially uniform thickness.
In the present invention, loss is minimized by providing that the ratio of the average area of the nodes 111 to the average area of the struts 109 is from about 1 to about 30, preferably from about 1 to about 20, still more -17 -preferably from about 2 to about 20, yet more preferably from about 4 to about 13, yet still more preferably from about 4 to about 10, and still yet more preferably from about 6 to about 10.
Figure 8 illustrates plots of the simulated loss as a function of wavelength for three exemplary fibers, here in accordance with the fiber of Figure 2, each having the same effective core diameter and the same effectIve diameter for the first two rings of cavities 115, but with a decreasing thickness to the remaining, outer rings of cavIties 115. In this embodiment the decreased thickness of the outer rings of cavities 115 is achieved by radial compression.
In the first fiber (Fiber Al), the core 115 has an effective core radius (R) of 13 pm, the ratio of the effectIve core diameter (Da,) to the effective cladding diameter (Dddu) is 0.31, whereby the thickness of the microstructured cladding in the radial direction is 28.93 pm, the average strut thickness (tc) is 110 nm, the fillet radius (rJW) Is 0.21, where W is the average diameter of the cavities 115, and the photonic bandgap is centered around a wavelength of 1.7 pm.
In the second fiber (Fiber A2), the core 115 has an effective core radius (Rcore) of 13 pm, the thickness of the microstructured cladding in the radial dIrection is 26.84 pm (95% of that of Fiber Al), the avenge strut thickness (ta) Is 110 nm, the fillet radius (rJW) Is 0.21, and the photonic bandgap Is centered around a wavelength of 1.65 pm.
In the third fiber (Fiber A3), the core 115 has an effective core radius (Re) of 13 pm, the thickness of the microstructured cladding in the radial direction Is 24.74 pm (90% of that of Fiber Al), the average strut thickness (tv) is 110 nm, the fillet radius (rJW) is 0.21, and the photonlc bandgap Is centered around a wavelength of 1.625 pm. 18 -
As can be seen from Figure 8, confinement loss, plotted in dotted Unes, increases by more than an order of magnitude for each progressive cladding compression, and contributes to a net reduction in the overall transmission bandwidth.. The narrower bandwidth results from more closely spaced nodes (narrowing the photonic bandgap) and a thinner air cavity region surrounding the core (increasing the confinement loss). However, at wavelengths well within the bandgap, aM fibers have essentially the same value of total loss, which confirms that loss is dominated by scattering from surface roughness, which is mostly unaffected by the structure beyond the second ring of cavities 115. As a result, the HC-PBGF of the present invention advantageously is robust to slight distortions beyond the second ring of air holes 115.
Figure 9 illustrates plots of simulated loss as a function of the size of the oversized "corner" cavities 115' at the core boundary 107 for six fibers (Fibers Bi to B6) iii accordance with the embodiment of Figure 3. Also superposed is the loss plot for [he "ideal" fiber of Figure 1, and the cutback measurement for the fabricated "ideai" fiber [1].
These oversized "corner" cavities arise as a natural consequence of surface tension trying to create a circular core surround from an original hexagonal structure, and in an alternative embodiment cou!d be undersized.
In this embodiment the fiber has an effective core diameter (D,0,) of 26 pm, the ratio of the core diameter (Dre = 2R) to the cladding diameter (DciaddIna) is 0.36 (which compares to 0,31 for the embodiment of Figure 2), the average thickness (t,) of the cladding struts 111 is 110 nfl, the average thickness (ta) of the core struts 111', which define the core boundary 107, is nm and the fillet radius (r/W) is 0.21.
In this embodiment the length: uniformity (Q) of the pitches of the adjacent core nodes 109' for each of the Fibers 31 to 35, which is given by a ratio between the length difference between the longest and shortest pitches (Al) -19 -and the average length of the pitches of the core nodes 109' (mean(l)), is 0.01, 0.15, 0.29, 0.45, 0.57 and 0.74, which compares to a length uniformity (Q) of 0.536 for the "ideal" fiber of Figure 1.
In addition, conservation of the glass volume in the struts 109, 109' was Imposed, resulting In struts 111, 111' longer than average being thinner than and vice-versa for shorter struts 109, 109'.
In Fibers 51 to B6, the size of the corner holes was increased in incremental steps from 2.8RJ(5V3) to 4.8R</(5V3), and the mode profiles and loss computed for all wavelengths across the bandgap.
As before, the scattering loss contrIbution remains dominant for the six ring structures. Although the leakage loss contribution in the fiber with the most enlarged "corner" holes 115' (Fiber B6) is twice as much as for the fiber with the least enlarged "corner" holes 115' (Fiber Si), this still only amounts to 0.035 dB/km, which is a small fraction of the total loss.
As can be seen from Figure 9, fibers with larger corner holes 115' suffer from higher losses. The larger corner holes 115' Impose larger gaps between the nodes 111' on the core boundary 107, and such gaps prompt the electric field to overlap more strongly with the scattering surfaces, generating a significantly higher scattering loss, as illustrated In the contour plots of FIgures 10(a) and (b), which illustrate the contour lines for the time average power flow in the z-directlon over a 30 dB range at 2 dB intervals for Fibers Bi and 56, Fiber Si not only results in reduced overlap of the guided field with the scattering surfaces, but aiso avoids introducing surface modes within the photonic bandgap.
It is strikIng to note that the structure considered to date to be the "ideal" fiber design, as illustrated in Figure 1, Is that which provides the highest loss, despite featuring a core surround that preserves the periodicity of the structure. As discussed above, this is due to a smaller core diameter -20 - (D), but also because the pitch of the nodes 111' on the core boundary 107 is not uniform, which in combination leads to the loss in this ideal" fiber being 2.4 times higher than that of Fiber Bi, in which the nodes 111' on the core boundary are equidistant.
Figure 11 illustrates plots of loss as a function or core wall thickness for fibers (Fibers Cl to C3) in accordance with the embodiment of Figure 3, where each having equi-spaced core nodes 111' and having no core tube and core tubes of the same thickness as the capillaries in the starting stack and 1.25 times the thickness of the capillaries in the starting stack.
As will be seen, when mass conservation Is applied to the wall at the core boundary 107 in the absence of core tube in the preform (Fiber Cl), the fundamental mode bandwidth is wide and loss remains low. Additionally, the effective indices of all the guided modes are clearly separated.
When the core wall thickness Is increased by, for example, introducing a core tube as thick as the cladding capillaries (Fiber C2), there is only a small bandwidth or loss penalty for fundamental mode transmission, with the minimum ioss increasing from 2 to 2.4 dB/km, with a 10 nm reduction in the bandwidth.
In this embodiment the surface modes introduced cross the fundamental mode near the short wavelength edge of the photonic bandgap, ensuring that the bandwidth for the fundamental mode remains largely unaffected.
Higher order modes, however, Interact with these surface modes near the center of the bandgap and therefore suffer a severe reduction in bandwidth.
This also confirms that the design with equal node spacing on the core boundary 107 not only provides the lowest loss but Is also more tolerant to thicker in core wail.
Further increasing the core wall thickness (Fiber C3) has limiting effects on performance. As can be seen, when a core tube which is 1.25 times thicker -21 -than the capillaries is used, surface modes anti-cross with the fundamental mode near the middle of the bandgap, resulting in higher losses and severe reduction In bandwidth.
Figure 12 illustrates plots of loss as a function or core wall thickness for fibers (Fibers Dl to D3) in accordance with the embodiment of Figure 3, where each having oversized "corner" cavities 115' and having no core tube and core tubes of the same thickness as the capillaries in the starting stack and 1.25 times the thickness of the capillaries in the starting stack, following fibers Cl to C3.
As will be seen, the reduction in bandwidth and increase in loss is clearly more noticeable for fibers with oversized "corner holes 115', increasing from a minimum of 2.9 dB/km over a bandwidth of 230 nm (Fiber Dl) to 4.6 dB/km over a bandwidth of 160 nm (Fiber D2).
Similarly to Fiber C3, further Increasing the core waii thickness (Fiber D3) has significant limiting effects on performance.
Figure 13(a) Illustrates plots of dispersion for fibers In accordance with the embodiment of Figure 3, wIth the nodes 111' at the core boundary 107 having a size of approximately 0.6 (Fiber El), 1 (Fiber E2) and 1.4 (Fiber E3) times the average size of the nodes 111 within the body of the cladding 105.
In this embodiment the pitch of the cavities 115 (A) is 3.03 pm, d/A is 0.987 and DJW is 0.6, where W is the average effective internal diameter of the cavities 115.
As can be seen, the fiber of the present invention allows readily for engineered dispersion through adjustment of the size of the core nodes 111' at the core boundary 107.
-22 -Figure 13(b) Illustrates plots of loss as a function of node size, corresponding to Figure 13(a).
As regards application, the HC-PBGF of the present invention has diverse application, including optical fiber communication systems, In particular ultrahigh capacity, ultralong haul systems and low latency short haul systems (such as of interest to financial trading firms/banks), datacomms, in particular low latency fiber links in datacentres and supercomputers, large scale high-energy physics (HEP), in particular use for low latency data transfer In detector arrays and for timing synchronisation, high-power laser delivery, in particular continuous-wave and pulsed radiation formats at diverse wavelengths, and gas sensing, in particular compact gas cells for environmental sensing/laser stabilisatlon.
Figures 14(a) to (g) Illustrate a conventional fabrication method for the fabrication of HC-PBGFs.
In a first step, as illustrated in FIgure 14(a), a pre-form stack 201 Is formed of millimeter-sized hollow capIllaries 203, wIth a predetermined number of capIllaries 203 beIng omitted from a core 205 of the stack 201 in dependence upon the required size of the core of the final, finished fiber.
For ease of illustration, only the innermost rings of capillaries 203 are illustrated, and, in practice, the array of capillaries 203 would be enclosed by a jacket tube, optionally with solid packaging rods to fill voids between the outermost capillaries 203 and the jacket tube. In this embodiment the pre-form stack 201 Is formed around a core tube 207, which is optional and defines a core boundary 209.
The illustrated fiber is for a nineteen cell (19c) fiber, where nineteen capillaries 203 are omitted to define the core 205 of the stack 201.
As noted hereinabove In relation to Figure 1, this conventional fabrication method yields a fiber In which the core struts 9' have unequal length and -23 -mass, as a consequence of the necessity for a periodic arrangement of the cavities 15 which are derived from the capillaries 203.
Figure 14(b) illustrates the arrangement of the capillaries 203 at the core boundary 209 and the contact points 210 therebetween.
In a subsequent step, as illustrated in Figure 14(c), the pre-forrn stack 201 Is heated to soften the glass structure, and the stack 201 is drawn to form canes 211 which have a reduced diameter, typIcally a few millimeters in diameter, and in which the capillarIes 203 are fused together, at least at the contact points 210. An appropriate pressure differential can be used to assist this process and collapse the gaps between the capillarIes 203.
In this process, as illustrated in Figure 14(d), cladding struts 11 of the finished fiber begin to form at the contact points 210 between adjacent capillaries 203, and core struts 11' in the finished fiber form at the surfaces of the capillaries 203 which are presented to the core 205.
Figure 14(e) illustrates the structure of a resulting cane 211.
In a further step, as Illustrated in Figure 14(f), the cane 211 Is clad in a jacket tube 212, here a glass tube, a vacuum is applied to the annular space between the jacket tube 212 and the exterior surface of the cane 211 and a positive pressure is separately applied within the core 205 and the capIllaries 203, and the glass structure is softened by heating and drawn to form a fiber 214 of a required diameter. In the fiber draw process, the cane 211 Is stretched longitudinally, but, due to the applied positive pressure within the core 205 and the capillaries 203, the core and cladding structure are also expanded (in relation to the structure of the cane 211) in the transverse plane of the fiber, as the fiber is progressively stretched, and, as a result the struts 11 of the finished fiber being formed are stretched.
-24 -Before drawing the cane 211, the corner core capillaries 203" present a shorter length between the contact points 210, as highlighted in Figure 14(d), and hence present less mass to the core boundary 209 as compared to the intermediate core capiUaries 203', with the arcuate segments of the corner core capillaries 203" each presenting a volume of 2/ThflRt and the arcuate segments of the intermediate core capillaries 203' each presenting a volume of fiRt, where R is the radius of the capiflaries 203', 203" and t is the thickness of the waRs of the capiRaries 203', 203".
Figure 14(g) illustrates a fiber which resutts from this conventional fabrication method. As wiR be seen, because of the reduced volume of glass available at the corner core capillaries 203", the corner core capiliaries 203" are preferentially stretched in relation to the interm ate core capiflaries 203', and the resufting corner core struts 9' in the finished flber are longer and have a reduced thickness as compared to the intermediate core struts 9' in the finished fiber, which results in the core struts 9' having a significant variation in length.
It is an aim of the present invention to provde improved or alternative fabrication methods for fabricating HC-PBGFs as compared to the conventional fabrication method.
Figures 15(a) and (b) illustrate a fabrication method for fabricating HG-PBGFs in accordance with a first embodiment of the present invention.
In this embodiment the corner core capillaries 203" have a non-circular section, such that the length, and hence mass, presented by the corner core struts 109' in the finished fiber, as derived from the corner core capillaries 203", is equivaient to the length, and hence mass, presented by intermediate core struts 109' in the Finished fiber, as derived from the intermediate core capillaries 203'. a
-25 -With this arrangement, the core struts 109' in the finished fiber have substantially equal length and mass, but the cavities 115 are non-periodic.
As noted hereinabove, the present inventors have recognized that perlodicity of the cavities 115 is not an essential requirement where the core struts 109' in the finished fiber have substantially equal length.
In this embodiment the corner core capillaries 203" are oval in cross-section, but other sections could be employed, especially elongated sections, such as rectangular and teardrop sections, as illustrated in Figures 16 and 17.
Figure 18 illustrates a fabrication method for fabricating HC-PBGF5 in accordance with a second embodiment of the present invention.
In this embodiment the corner core capillaries 203" include an additional mass segment 221 at a surface thereof which is arranged to face the core 205 between adjacent intermediate core capillaries 203', whereby the mass presented by the corner core struts 109' in the finished fiber, as derived from the corner core capillaries 203", is equivalent to that presented by the intermediate core struts 111' in the finished fiber, as derived from the intermediate core capillaries 203'.
In this embodiment the mass segment 221 is at an external surface of the corner core capillary 203".
In this embodiment the mass segment 221 Is Integrally formed with a body of the corner core capillary 203", here comprising a thickened wall section of the corner core capillary 203".
In this embodiment the mass segment 221 is arcuate in section, but could have other shape which provides for equalization of the volumes of the core struts 109' in the finished fiber.
With this arrangement, the core struts 109' in the finished fiber have equal length and mass, but the cavities 115, as derived from the capillaries 203, are non-periodic. As noted hereinabove, the present Inventors have recognized that periodicity of the cavities 115 Is not an essential requirement where the core struts 111' in the finished fiber have substantially equal length.
In an alternative embodiment, as illustrated in Figure 19, the mass segment 221 could be an element separate to a body of the corner core capillary 203". In this embodiment the mass segment 221 is a strip, here a flat strip, but could have other shape which provides for equalization of the volumes of the core struts 109' in the finished fiber.
In another alternative embodiment, as illustrated in Figure 20, the mass segment 221 could be provided at an internal surface of the corner core capillary 203".
Figure 21 illustrates a fabrication method for fabricating l-IC-PBGFs in accordance with a third embodiment of the present invention.
In this embodiment the intermediate core capillaries 203' include a reduced mass segment 231 which is arranged to face the core 205, whereby the mass presented by the intermediate core struts 109', as derived from the intermediate core capillaries 203', Is equivalent to that presented by the corner core struts 109', as derived from the corner core capillaries 203".
In this embodiment the reduced mass segment 231 comprises a thinned wall section of the intermediate core capillaries 203'.
In this embodiment the reduced mass segment 231 is a thinned Internal wall section.
-27 -In an alternative embodiment the reduced mass segment 231 could be a thinned external wall section.
In this embodiment the reduced mass segment 231 is arcuate In section.
With this arrangement, the core struts 109' in the finished fiber have equal length and mass, but the cavities 115 are non-periodic. As noted hereinabove, the present Inventors have recognized that periodicity of the cavities 115 is not an essential requirement where the core struts 109' have substantially equal length.
Figure 22 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a fourth embodiment of the present invention.
In this embodiment a core tube 241 Is utliized, which includes additional mass segments 243 at a surface thereof in correspondence to the positions of the corner core capillaries 203", whereby the mass of the additional mass segments 243 supplements the mass of the corner core capillaries 203", such that the mass provided by each additional mass segment 243 and respective corner core capillary 203" in combination is equivalent to the mass presented by the intermediate core capillarIes 203'.
In this embodiment the additional mass segments 243 are at an external surface of the core tube 241.
With this arrangement, the core struts 109' in the finished fiber have equal length and mass, but the cavities 115 are non-periodic. As noted hereinabove, the present inventors have recognized that periodicity of the cavities 115 Is not an essential requirement where the core struts 109' in the finished fiber have substantially equal length and mass.
In an alternative embodiment, as illustrated in Figure 23, the mass segments 243 could be at an internal surface of the core tube 241.
-28 -In another alternative embodiment, as Illustrated In FIgure 24, the mass segments 243 project both from internal and external surfaces of the core tube 241.
In this embodiment, as illustrated in Figure 25, the core tube 241 Is fabricated by collapsing an arrangement of higher-mass elements 251 and lower-mass elements 253 between two concentric tubes 255, 257, here by application of vacuum in a heated environment which causes melting of the glass structure.
In this embodiment the higher-mass elements 251 are located at positions corresponding to the corner core capillaries 203".
In this embodiment the higher-mass elements 251 comprise solid rods and the lower-mass elements 253 comprise capillaries.
In one embodiment, as illustrated in Figures 26(a) to (c), additional mass elements 259 can be utilized in combination with the core tube 241, in order to control the size of the intermediate core nodes 111' in the finished fiber, as derived from junctions intermediate the corner core capillaries 203".
In this embodiment the additional mass elements 259 comprise solid rods of smaller diameter than the core capIllaries 203', 203", but alternatively could comprise capillaries which collapse to rods during fabrication.
In an alternative embodiment the core tube 241 could include the additional mass elements 259 as an Integral part thereof.
Figure 27 illustrates a fabrication method for fabricating i-IC-PBGFs in accordance with a fifth embodiment of the present invention.
-29 -In this embodiment a hexagonal core tube 261 Is utilized, which provides six planar side members 263, adjacent ones of which meet at corner junctions 265, which correspond in position to the corner core capillaries 203".
In one embodiment the corner junctions 265 can be arcuate.
In one embodiment the core tube 261 includes additional mass segments 267 at the corner junctions 265, whereby the mass of the additional mass segments 267 supplements the mass of the corner core capillaries 203", such that the mass provided by each additional mass segment 267 and respective corner core capillary 203" in combination is equivalent to the mass presented by the intermediate core capillaries 203'.
In this embodiment the additional mass segments 267 can be integrally formed with a body of the core tube 261, for example, as a fillet.
With this arrangement, the resulting core struts 109' In the finished fiber have equal length and mass, but the cavities 115 are non-periodic. As noted hereinabove, the present inventors have recognized that petiodicity of the cavities 115 is not an essential requirement where the core struts 109' in the finished fiber have substantially equal length and mass.
Figure 28 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a sixth embodiment of the present Invention.
In this embodiment the corner core capillaries 203" and the outer, cladding capillaries 203" have a hexagonal outer section, and the intermediate core capillaries 203' have a frusto-hexagonal outer section, here a pentagonal outer profile.
With this arrangement, the core capillaries 203', 203" present a substantially continuous surface at the core 205, in this embodiment substantially hexagonal in sectional shape at the core boundary 209. In an alternative embodiment the continuous surface at the core 205 could have another polygonal sectional shape, such as octagonal. In this embodiment the core 205 will become substantially circular following drawing, as a consequence of surface tension.
In this embodiment the thicknesses (tv, t,) of the wall sections of the corner core capillaries 203" and the Intermediate core capillarIes 203' are sized such that, following drawing of the fiber, the core struts 109' in the finished fiber have substantially equal length and mass.
In this embodiment the core capIllaries 203', 203" have a circular or part-circular Internal section.
In an alternative embodiment, as illustrated in Figure 29, the capillaries 203', 203", 203" could have a hexagonal or frusto-hexagonal Internal section, here pentagonal. In other embodiments the capillaries 203', 203", 203" could have other internal sectional shapes, including other polygonal shapes or shapes intermediate circular and hexagonal.
With this arrangement, the resulting core struts 109' in the finished fiber have equal length and mass, but the cavities 115 are non-periodic. As noted hereinabove, the present inventors have recognized that periodicity of the cavities 115 is not an essential requirement where the core struts 109' in the finished fiber have substantially equal length.
Figures 30(a) and (b) illustrate a fabrication method for fabricating HC-PBGF5 in accordance with a seventh embodiment of the present invention.
In this embodiment the core capillaries 303 are iocated on a circle of predetermined diameter, about which further, outer capillaries 303' are packed, here in hexagonal relation.
-31 -In this embodiment the core capIllaries 303 are provided as a core assembly 304, in which the core capillaries 303 are fused together.
In this embodiment the core capillaries 303 are located about a core tube 307.
In this embodiment additional mass elements 311 are located at the junctions of each of the core capillaries 303, in order to provide for increased mass at the nodes 111' In the finished fiber which result from these junctions.
In an alternative embodiment, instead of fusing the core capIllaries 303 or additionally thereto, the core capillaries 303 could be provided between the core tube 307 and an outer tube, with the outer tube being a thin tube In one embodiment, thInner than the core tube 307, for purposes of retaining the core capIllaries 303 in position.
With this arrangement, the core struts 109' in the finished fiber have equal length and mass, but the cavities 115 are non-periodic. As noted hereinabove, the present inventors have recognized that periodlcity of the cavities 115 is not an essential requirement where the core struts 109' have substantially equal length.
In an alternative embodiment, and similarly to the first-described embodiment of Figures 15(a) and (b), the corner cladding capillaries 303" in a second or subsequent capillary ring, which is outwardly of the core assembly 304, has a non-circular section, such that the outer rings have a tight packing and undesired cladding distortions are prevented.
In this embodiment the corner cladding capillaries 303" are oval in cross-section, but other sections could be employed, such as rectangular and teardrop, as Illustrated hereinabove In relation to Figures 16 and 17.
-32 -Figure 32 illustrates a fabrication method for fabricating HC-PBGFs in accordance with an eighth embodiment of the present invention.
In this embodiment a pressure Is applied to the corner core capillaries 403" independently of the core 405, the intermediate core capillaries 403' and the outer cladding capillaries 403".
By providing a pressure differential, here a positive pressure differentIal, the size of the corner core capillaries 403" can be controlled in relation to the intermediate core capillaries 403', such that the core struts 109' in the finished fiber have equal length and mass, whilst the cavities 115 are non-periodic. As noted hereinabove, the present Inventors have recognized that periodlcity of the cavities 115 is not an essential requirement where the core struts 109' have substantially equal length.
In this embodiment a first pressure source 406 is applied to the corner core capillaries 403", a second pressure source 407 is applied to the intermediate core capillaries 403' and the outer cladding capillaries 403", and a third pressure source 409 is applied to the core 405.
It will be understood that this aspect of the fabrication method has application to any of the other-described embodiments, in allowing for control of the relative size of the corner core capillaries 403".
Figure 33 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a ninth embodiment of the present invention.
In this embodiment the corner core capillaries 503" are formed of a material having a higher thermal viscosity at the drawing temperature than the material of the intermediate core capillaries 503', and also optionally the outer cladding capillaries 503".
-33 -in this embodiment the capillaries 503', 503", 503" are formed of a glass composition.
In one embodiment the corner core capillaries 503" are formed of substantially pure silica glass and the intermediate core capillaries 503', and also optionally the outer cladding capillaries 503", are formed of a doped silica, where the dopant reduces the glass viscosity. In an alternative embodiment the corner core capillaries 503" could also be a doped silica of different kind to the intermediate core capillaries 503' and optionally the outer cladding capillaries 503".
In this embodiment the silica is halogen doped, here with fluorine, but alternatively the dopant could be chlorine.
In other embodiments the dopants could be any which alter thermal viscosity, such as boron, phosphorus, sodium or titanium.
By virtue of providing a viscosity differential between the corner core capillaries 503" and at least the intermediate core capillaries 503', the size of the corner core capillaries 503" can be regulated in relation to the intermediate core capillarIes 503', thereby ensuring that the corner core capillarIes 503" do not over-expand in relation to the intermediate core capIllaries 503', whereby the core struts 109' in the finished fiber have equal length and mass, whilst the cavities 115 are non-periodic. As noted hereinabove, the present Inventors have recognized that periodicity of the cavitIes 115 Is not an essential requirement where the core struts 109' have substantially equal length.
In one embodiment, and following the method of the eighth-described embodiment above, the pressure in the corner core capillaries 503" could be lower or equal to the pressure in the other capillaries 503', 503".
-34 -It will be understood that this aspect of the fabrication method has application to any of the other-described embodiments, in allowing for control of the relative size of the corner core capillarIes 503".
Figure 34 illustrates a fabrication method for fabricating HC-PBGFs in accordance with a tenth embodiment of the present invention.
In this embodiment additional mass segments 604', 604" are located at the junctions between the core capillaries 603', 603", whereby the mass of the additional mass segments 604', 604" supplements the mass of the corner core capillaries 603", such that the mass provided by each additional mass segment 604" and respective corner core capillary 603" in combination is equivalent to the mass presented by the intermediate core capillaries 603', and also supplements the mass at the core boundary 609.
In this embodiment the additional mass segments 604' at the junctions between intermediate core capillaries 603' can be of a different size, and hence mass, to the additional mass segments 604" at the junctions with corner core capillaries 603".
With this arrangement, the core struts 109' In the finished fiber have equal length and mass, and through control of the mass at the core boundary 107 of the finished fiber, the dispersive properties of the fiber can be controlled.
It will be understood that this aspect of the fabrication method has application to any of the other-described embodiments, in allowing for control of the mass at the core boundary 107 in the finished fiber.
Figure 35 illustrates a fabrication method for fabricating HC-PBGFs in accordance with an eleventh embodiment of the present invention.
In this embodiment the core 705, instead of being empty, includes a core former 711 and the jacket tube 712 is disposed in a mold 715 of -35 -counterpart shape to the jacket tube 712, such that the jacket tube 712 Is a close fit In the mold 715. With this arrangement, radial expansion of the stack 701 beyond the core former 711 and the mold 715 is prevented, thereby maintaining the effective radial dimension of the stack 701.
In this embodiment the core former 711 is circular in section.
In this embodiment the jacket tube 712 and the mold 715 have a counterpart hexagonal sectional shape.
In this embodiment the core former 711 and the mold 715 are formed of graphite, vitreous carbon or another suitable high-temperature, heat-resistant material.
In this embodiment the core capillaries 703', 703" and the cladding capillaries 703" are sealed, such that each has an enclosed volume, and any other capillaries included to add to the mass of the core nodes 111' or core struts 109' are open so as to provide for collapse of any such capillaries.
In this embodiment the pre-form stack 701 is subjected to a blow-molding process prior to drawing the cane 211, In which process the stack 701 Is heated while a vacuum is applied to the volume within the jacket tube 712, which causes the core capIllarIes 703', 703" to expand, as a consequence of being enclosed, and this expansion causes the core capillarIes 703', 703" to fill voids at the surface of the core former 711. In addition, the outer, cladding capillaries 203" will expand to fill voids at the junctions thereof.
In this embodiment the corner core capillarIes 703" each include at least one additional corner mass segment 721, here a plurality of additional corner mass segments 721, which are arranged to face the core 705 between adjacent intermediate core capillaries 703', whereby the mass presented by the core struts 109' in the finished fiber as derived from the -36 -corner core capillaries 703" and the corner mass segments 721 In combination Is equivalent to that presented by the intermediate core struts 109' in the finished fiber as derived from the intermediate core capillaries 703'.
In this embodiment the additional corner mass segments 721 comprise hollow elements which are open and thus collapse under the applied pressure in the blow-molding process.
In this embodiment the additional corner mass segments 721 comprise capillaries of smaller radial dimension than the corner core capillaries 703".
In this embodiment additional interstitial mass segments 723 are provided at each of the interstices of the capillaries 703', 703", 703", whereby the mass of the nodes 111, 111' is controlled.
In this embodiment the interstitial mass segments 723 comprise solid elements, here rods, but in an alternative embodiment could be capillaries which are closed in the blow-molding process.
Finally, it will be understood that the present invention has been described in Its preferred embodiments and can be modified in many different ways without departing from the scope of the invention as defined by the appended claims.
--
References 1. F. Poletti, N. V. Wheeler, M. N. Petrovich, N. Baddela, E. Numkam Fokoua, 3. R. Hayes, D. R. Gray, Z. Li, R. Slavik, and D. 3. Richardson, "Towards high-capacity fibre-optic communications at the speed of light In vacuum," Nature Photonlcs 7, 279-284 (2013).
2. V. Jung, V. A. 3. M. Sleiffer, N. Baddela, M. N. Petrovich, 3. R. Hayes, N. V. Wheeler, D. R. Gray, E. Numkam Fokoua, 3. P. Wooier, H. H.-L. Wong, F. Parmigiani, 5.-U.
Alam, 3. Surof, M. Kuschnerov, V. Veljanovski, H. de Waardt, F. Poletti, and D. 3. RIchardson, "First demonstration of a broadband 37-cell hollow core photonic bandgap fiber and its application to high capacity mode division multiplexing," in Proceedings of the Optical Fiber Communications conference (2013), paper PDP5A.3 (Postdeadilne).
3. P. 3. Roberts, F. Couny, H. Sabert, B. 3. Mangan, D. P. Williams, L. Farr, M. W. Mason, A. Tomlinson, T. A. Birks, 3. C. Knight, and P. S. J.Russeli, "Ultimate low loss of hollow-core photonic crystal fibres," Opt. Express 13, 236-244 (2005).
4. E. Numkam Fokoua, F. Poletti, and D. 3. Richardson, "Analysis of light scattering from surface roughness in hollow-core photonic bandgap fibers," Opt. Express 20, 20980-20991 (2012).
5. B. 3. Mangan, L. Farr, A. Langford, p. j. Roberts, D. P. Williams, F. Couny, M. Lawman, M. Mason, S. Coupland, R. Flea, H. Sabert, T. A. Birks, .3. C. Knight, and P. St. 3. Russell, "Low loss (1.7 dB/km) hollow core photonic bandgap fiber," In Proceedings of Optical Fiber Communication Conference (2004), paper PDP24.
6, P. Roberts, D. Williams, B. Mangan, H. Sabert, F. Couny, W. Wadsworth, T. Birks, 3. Knight, and P. Russell, "Realizing low loss air core photonic crystal fibers by exploiting an antiresonant core surround," Opt.
Express 13, 8277-8285 (2005).
-38 - 7. C. M. Smith, N. Venkataraman, M. 1. Gallagher, D. Muller, ). A.West, N. F. Borrelli, D. C. Allan, and K.W. Koch, "Low-loss hollow-core silica/air photonic bandgap fibre," Nature 424, 657-659, (2003).
8. R. Amezcua-Correa, N. G. Broderick, M. N. Petrovich, F. Poletti, and D.J.
Richardson, "Optimizing the usable bandwidth and loss through core design in realistic hollow-core photonic bandgap fibers," Opt.
Express 14, 7974-7985 (2006).
9. R. Amezcua-Correa, N. G. R. Broderick, M. N. Petrovich, F. Poletti, and D. J. Richardson, "Design of 7 and 19 cells core air-guiding photonic crystal fibers for low-loss, wide bandwidth and dispersion controlled operation/' Opt. Express 15, 17577-17586 (2007).
10.R. Amezcua-Correa, F. Gèrôme, S. G. Leon-Saval, N. G. R. Broderick, 1.
A. Birks, and 3. C. Knight, "Control of surface modes in low loss hollow-core photonic bandgap fibers," Opt. Express 16, 1142-1149 (2008) 11.M. H. Frosz, 3. Noid, T. Weiss, A. Stefani, F. Babic, S. Rammier, and P. St. 3. Russell, "Five-ring holiow-core photonic crystal fiber with 1.8 dB/km loss," Opt. Lett. 38, 2215-2217 (2013).
12.Kunimasa Saitoh and Masanori Koshiba, "Leakage loss and group velocity dispersion in air-core photonic bandgap fibers," Opt. Express 11, 3100-3109 (2003).
13.Ming-Jun U, James A. West, and Karl W. Koch, "Modeling Effects of Structural Distortions on Air-Core Photonic Bandgap Fibers," 3.
Lightwave Technol. 25, 2463-2468 (2007).
14.F. Poletti, M. N. Petrovich, R. Amezcua-Correa, N. G. Broderick, T. M. Monro, and D.3. Richardson, " Advances and Limitations in the Modeling of Fabricated Photonic Bandgap Fibers," in Optical Fiber Communication Con ference and Exposition and The National Fiber Optic Engineers Con ference, Technical Digest (CD) (Optical Society of America, 2006), paper OFC2.
15.Kiarash Zamani Aghaie, Michel 3. F. Digonnet, and Shanhui Fan, "Experimental Assessment of the Accuracy of an Advanced Photonic-Bandgap-Fiber Model," 3. Lightwave Technol. 31, 1015-1022 (2013).
-39 - 16.Francesco Poletti, "Hollow core fiber with an octave spanning bandgap," Opt. Left. 35, 2837-2839 (2010).
17.F. Polettl, and E. Numkam Fokoua Understanding the Physical OrigIn of Surface Modes and Practical Rules for their SuppressIon," accepted for oral presentation at ECOC 2013.
18.Tadashi Murao, Kunimasa Saitoh, and Masanori Koshlba, "Structural Optimization of Air-Guiding Photonic Bandgap Fibers for Realizing Ultimate Low Loss Waveguides," 3. Lightwave Technol. 26, 1602-1612 (2008)

Claims (17)

1. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the corner core capillaries have a non-circular section, and optionally an elongated section; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding whIch surrounds the core at a core boundary and comprises a lattice or network of struts and interstItial nodes whIch together define an array of cavities.
2. The method of claim 1, wherein the corner core capillaries provide that, in the finished fiber, a ratio between a difference In a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary Is less than about 0.3.
3. The method of claim 1 or 2, wherein the intermediate core capillaries are substantially circular.
4. The method of any of claims 1 to 3, wherein any or each corner core capillary is oval or elliptical in cross-section.
5. The method of any of claims 1 to 4, wherein any or each corner core capillary is rectangular in cross-section.
6. The method of any of claims 1 to 5, wherein any or each corner core capillary has a teardrop section.
-41 -
7. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, Intermediate core capillaries, wherein the corner core capillaries Include an additional mass segment at a surface thereof which is arranged to face the core between adjacent Intermediate core capillaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and Interstitial nodes which together define an array of cavities.
B. The method of claim 7, wherein the additional mass segments provide that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3.
9. The method of claim 7 or 8, wherein any or each additional mass segment is at an external surface of the respective corner core capillary.
10. The method of any of any of claims 7 to 9, wherein any or each additional mass segment is at an internal surface of the respective corner core capillary.
11., The method of any of claims 7 to 10, wherein the additional mass segment is integrally formed with a body of the respective corner core capillary.
-42 -
12. The method of claim 11, wherein any or each additional mass segment is provided by a thickened wall section of the corner core capillary.
13. The method of any of claims 7 to 12, wherein any or each additional mass segment is arcuate In section.
14. The method of any of claIms 7 to 13, whereIn any or each additional mass segment is an element separate to a body of the respective corner core capillary.
15. The method of any of claims 7 to 14, wherein any or each additional mass segment is a solid element, optionally a strip or rod or any suitable cross-section, or two or more solid elements
16. The method of any of claIms 7 to 15, wherein any or each additional mass element is a hollow element, optionally a capillary of any suitable cross-section, and optionally of smaller radial dimension than the respective corner core capillary.
17. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, Intermediate core capillaries, wherein the intermediate core capillaries include a reduced mass segment at a surface thereof which Is arranged to face the core; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities. -4318. The method of claim 17, wherein the reduced mass segments provide that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3.19. The method of claim 17 or 18, wherein any or each reduced mass segment comprises a thinned wall section of the respective intermediate core capillary.20. The method of claim 19, wherein any or each reduced mass segment is a thinned Internal wail section.21. The method of claim 19 or 20, wherein any or each reduced mass segment is a thinned external wail section.22. The method of any of claims 17 to 21, wherein any or each reduced mass segment is arcuate in section.23. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries about a core tube, wherein the stack has a hollow core as defined by the core tube and the capillaries at a boundary of the core tube comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the core tube Includes additional mass segments at a surface thereof in correspondence to the positions of the corner core capillaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.24. The method of claim 23, wherein the additional mass segments provide that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3.25. The method of claim 23 or 24, wherein any or each additional mass segment Is at an external surface of the core tube.26. The method of any of claims 23 to 25, wherein any or each additional mass segment is at an internal surface of the core tube.27. The method of any of claims 23 to 26, wherein any or each additional mass segment projects from internal and external surfaces of the core tube.28. The method of claim 27, wherein the core tube is fabricated by collapsing an arrangement of higher-mass elements and lower-mass elements between two tubes, optionally concentric tubes.29. The method of claim 28, wherein the higher-mass elements are located at positions corresponding to the corner core capillaries.30. The method of claim 28 or 29, wherein the higher-mass elements comprise solid rods of any suitable cross-section, optionally circular.31. The method of any of claims 28 to 30, wherein the lower-mass elements comprise capillaries of any suitable cross-section, optionally circular.32. The method of any of claims 23 to 31, wherein the stack further comprises additionai mass elements at unfilled junctions between adjacent intermediate core capillaries, whereby a size of the core -4 -nodes In the finished fiber, as derived from the intermediate the corner core capillaries, can be controlled.33. The method of claim 32, whereIn the additional mass elements comprise solid rods of any suitable cross-section or capillaries of any suitable cross-section that are of smaller diameter than the core capillaries and collapse to solid rods during fabrication.34. The method of claim 32 or 33, wherein the core tube includes the additional mass elements as an integral part thereof.35. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries about a core tube, wherein the stack has a hollow core as defined by the core tube and the capillarIes at a boundary of the core tube comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the core tube is hexagonal in section which provides six planar side members, adjacent ones of which meet at corner junctions, which correspond in position to the corner core capillaries; and reducing the stack to a fIber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.36. The method of claim 35, wherein the additional mass segments provide that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary Is less than about 0.3.-46 - 37. The method of claim 35 or 36, whereIn the corner junctions are arcuate.38. The method of any of claims 35 to 37, wherein the core tube includes additional mass segments at the corner junctions.39. The method of claim 38, wherein the additional mass segments are integrally formed with a body of the core tube, optionally as a fillet.40. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, Intermediate core capillaries, wherein the corner core capillaries have a substantially hexagonal outer section, and the Intermediate core capillaries have a substantially frusto-hexagonal outer sectIon; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and Interstitial nodes which together define an array of cavities.41. The method of claim 40, wherein the additional mass segments provide that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3.42. The method of claim 40 or 41, wherein outer, cladding capillaries have a substantially hexagonal outer section, 43. The method of any of claims 40 to 42, wherein the intermediate core capillaries have a substantially pentagonal outer section.*, 47 - 44. The method of any of claims 40 to 43, wherein the core capillaries present a substantially continuous surface at the core.45. The method of any of claims 40 to 44, wherein the core has a substantially hexagonal or octagonal sectional shape.46. The method of any of claims 40 to 45, wherein thicknesses (tv, t,) of wall sections of the corner core capillaries and the intermediate core capillaries are sized such that, following reduction of the fiber, the core struts in the finished fiber have substantially equal length and mass.47. The method of any of claims 40 to 46, wherein any or each of the core capillaries have a circular or part-circular internal section.48. The method of any of claims 40 to 47, wherein any or each of the capillaries have a hexagonal or frusto-hexagonal internal section.49. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of core are located on a circle of predetermined diameter, about which outer, cladding capillaries are packed; and reducing the stack to a fiber, whereIn the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and Interstitial nodes which together define an array of cavities.50. The method of claIm 49, wherein the core capillaries provide that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary Is less than about 0.3.51. The method of claim 49 or 50, wherein the outer capillaries are packed In hexagonal or close-packed triangular relation.52. The method of any of claIms 49 to 51, wherein the core capillaries are provided as a core assembly.53. The method of claim 52, wherein the core capillaries are fused together.54. The method of any of claims 49 to 53, whereIn the core capillaries are located about a core tube.55. The method of claim 54, wherein the core capillaries are retained between the core tube and an outer tube, optionally the outer tube is thinner than the core tube.56. The method of any of claims 49 to 55, wherein the stack further comprises additional mass elements located at unfilled junctions of the core capillaries.57. The method of any of claims 49 to 56, wherein corner capillaries in a second or subsequent capillary ring, which Is outwardly of the core assembly, have a non-circular section, optionally an elongated section, whereby the outer rings can have a close packing and undesired cladding distortions can be prevented.58. The method of claim 57, whereIn intermediate capillaries in the second or subsequent ring are substantially circular.59. The method of claim 57 or 58, whereIn any or each corner capillary is oval or elliptical in cross-section.60. The method of any of claims 57 to 59, whereIn any or each corner capillary is rectangular in cross-section.61. The method of any of claims 57 to 60, wherein any or each corner capillary has a teardrop section.62. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries; applying a pressure differential between the corner core capillaries and the Intermediate core capillaries, whereby a size of the corner core capillaries can be controlled in relation to the Intermediate core capillaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.63. The method of claim 62, wherein the pressure differential provides that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pItch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3.64. The method of claim 62 or 63, whereIn a pressure Is applied to the corner core capillaries separately of the intermediate core capillaries, and optionally outer, cladding capillaries.-50 - 65. The method of claim 63 or 64, wherein a pressure is applied to the corner core capillaries separately of the Intermediate core capillaries, outer, cladding capillaries and the core.66. The method of claim 65, whereIn a first pressure source is applied to the corner core capillaries, a second pressure source is applied to the Intermediate core capillaries and the outer, cladding capillaries, and a third pressure source Is applied to the core.67. A method of fabricating a hollow-core photonic-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein the corner core capillaries are formed of a material having a higher viscosity at a fiber drawing temperature than a material of the intermediate core capillaries, whereby a size of the corner core capillaries can be regulated In relation to the intermedIate core capillaries; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and Interstitial nodes which together define an array of cavities.68. The method of claim 67, wherein the viscosity relationship of the materials of the corner and Intermediate core capillaries provides that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3. -5169. The method of claim 67 or 68, wherein the corner core capillaries are formed of a material having a higher viscosity at the fiber drawing temperature than a material of outer, cladding capillaries.70. The method of any of claims 67 to 69, wherein the capillaries are formed of a glass composition.71.. The method of claim 70, wherein the corner core capillaries are formed of substantially pure silica glass and the intermediate core capillaries are formed of a doped silica glass.72. The method of claim 70, wherein the corner core capillaries and the intermedIate core capIllaries are formed of differently-doped silica glasses.73. The method of claim 71 or 72, wherein the outer, cladding capillaries are formed of a doped silica glass.74. The method of any of claims 71 to 73, whereIn the doped silica is a halogen-doped silica, optionally a fluorine-doped silica or a chlorine-doped silica.75. The method of any of claims 71 to 73, wherein the doped silica is doped with one or more elements which alter the glass viscosity, optionally one or more of boron, phosphorus, sodium or titanium.76, The method of any of claims 71 to 73, wherein the doped silica is applying a pressure differential between the corner core capillaries and the intermediate core capillarIes.77. The method of claim 76, wherein a pressure in the corner core capillaries Is lower or equal to the pressure applied at least to the intermediate core capillaries.-52 -: 78. A method of fabricating a hollow-core photonlc-bandgap fiber, comprising the steps of: providing a stack of capillaries, wherein the stack has a hollow core and the capillaries at a boundary of the core comprise a plurality of first, corner core capillaries and a plurality of second, intermediate core capillaries, wherein additional mass segments are located at unfilled junctions between the core capillaries, whereby the mass of the additional mass segments supplements the mass of the corner core capillaries in relation to the intermediate core capillaries, and also supplements the mass at the core boundary; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and interstitial nodes which together define an array of cavities.79. The method of claim 78, wherein the additional mass segments provide that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3.80. The method of claim 78 or 79, wherein the additional mass segments at the unfilled junctions between intermediate core capillaries are of a different size and mass to the additional mass segments at the unfilled junctions with corner core capillaries.81. A method of fabricating a hollow-core photonlc-bandgap fiber, comprising the steps of: providing a core former; providing a stack of capillaries to the core former, wherein the stack has a hollow core as defined by the core former, and the capillaries at a boundary of the core comprise a plurality of first, corner core -53 -capillaries and a plurality of second, Intermediate core capillaries, wherein the core capillaries, and optionally outer, cladding capillaries, are sealed such that each has an enclosed volume; providing the stack of capillaries in a mold; heating the stack of capillaries, whereby the core capillaries expand and fill voids at the surface of the core former; and reducing the stack to a fiber, wherein the fiber has a hollow core and a cladding which surrounds the core at a core boundary and comprises a lattice or network of struts and Interstitial nodes which together define an array of cavities.82. The method of claim 81, wherein the expansion of the enclosed core capillaries provides that, in the finished fiber, a ratio between a difference in a length of a longest and shortest pitch spacing of the nodes at the core boundary to an average pitch spacing of the nodes at the core boundary is less than about 0.3.83. The method of claim 81 or 82, wherein the stack comprises a Jacket tube, and further comprising the step of: applying a vacuum within the jacket tube.84. The method of any of claims 81 to 83, wherein the mold is of counterpart shape to the stack, such that the stack is a close fit in the mold and radial expansion of the stack beyond the core and the mold is prevented, thereby maintaining the effective radial dimension of the stack.85. The method of any of claims 81 to 84, wherein the core former is circular in section.86. The method of claims 81 to 85, wherein the stack and the mold have a counterpart hexagonal sectional shape.-54 - 87. The method of any of claims 81 to 86, wherein the core former and the mold are formed of a high-temperature heat-resistant material, optionally graphite or vitreous carbon.88. The method of any of claims 81 to 87, wherein the corner core capillaries each include at least one additional corner mass segment which is arranged to face the core between adjacent intermediate core capillaries.89. The method of claim 88, wherein the corner core capillaries each Include a plurality of additional corner mass segments.90. The method of claim 88 or 89, wherein the additional corner mass segments comprise hollow elements which are open and collapse in fabrication.91. The method of claim 90, whereIn the hollow elements comprise capillaries, optionally of smaller radial dimension than the corner core capillaries.92. The method of any of claims 81 to 91, where the stack comprises additional interstitial mass segments at each of the Interstices of the capillaries, whereby the mass of the nodes in the resulting can be controlled.93. The method of claim 92, wherein the interstitial mass segments comprise solid elements of any suitable cross-section, optionally rods.94. The method of claim 92, wherein the interstitial mass segments comprise hollow elements of any suitable cross-section, optionally capillaries.-55 - 95. The method of any of claims 81 to 94, wherein the corner core capillaries are formed of a material having a higher viscosity at a fiber drawing temperature than a material of the Intermediate core capillaries 96. The method of claim 95, wherein the capillaries are formed of a glass composition.97. The method of claim 96, whereIn the corner core capillaries are formed of substantially pure silica glass and the Intermediate core capillaries are formed of a doped silica glass.98. The method of claim 96, whereIn the corner core capillarIes and the Intermediate core capillaries are formed of differently-doped silica glasses.99. The method of claim 97 or 98, wherein outer, cladding capillaries are formed of a doped silica glass.100. The method of any of claims 97 to 99, wherein the doped silica is a halogen-doped silica, optionally a fluorine-doped silica or a chlorine-doped silica.101. The method of any of claims 97 to 99, wherein the doped silica Is doped with one or more elements which alter the glass viscosity, optionally one or more of boron, phosphorus, sodium or titanium.102. A pre-form stack for use in the fabrication of a hollow-core photonic-bandgap fiber in accordance with the method of any of claims 1 to 101.
GB1316795.2A 2013-09-20 2013-09-20 Hollow-core photonic bandgap fibers and methods of manufacturing the same Active GB2518420B (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
GB1813894.1A GB2562687B (en) 2013-09-20 2013-09-20 Methods of manufacturing hollow-core photonic bandgap fibers.
GB1813895.8A GB2562688B (en) 2013-09-20 2013-09-20 Methods of manufacturing hollow-core photonic bandgap fibers.
GB1316795.2A GB2518420B (en) 2013-09-20 2013-09-20 Hollow-core photonic bandgap fibers and methods of manufacturing the same
US15/023,541 US11034607B2 (en) 2013-09-20 2014-09-19 Hollow-core photonic bandgap fibers and methods of manufacturing the same
PCT/EP2014/070048 WO2015040189A2 (en) 2013-09-20 2014-09-19 Hollow-core photonic bandgap fibers and methods of manufacturing the same
EP14771866.2A EP3047319B8 (en) 2013-09-20 2014-09-19 Methods of manufacturing hollow-core photonic bandgap fibers
DK14771866.2T DK3047319T3 (en) 2013-09-20 2014-09-19 PHOTONIC BAND GAB FIBERS WITH HOLE CORE AND METHODS OF MANUFACTURE THEREOF

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1316795.2A GB2518420B (en) 2013-09-20 2013-09-20 Hollow-core photonic bandgap fibers and methods of manufacturing the same

Publications (3)

Publication Number Publication Date
GB201316795D0 GB201316795D0 (en) 2013-11-06
GB2518420A true GB2518420A (en) 2015-03-25
GB2518420B GB2518420B (en) 2019-05-01

Family

ID=49553206

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1316795.2A Active GB2518420B (en) 2013-09-20 2013-09-20 Hollow-core photonic bandgap fibers and methods of manufacturing the same

Country Status (1)

Country Link
GB (1) GB2518420B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017080564A1 (en) * 2015-11-10 2017-05-18 Nkt Photonics A/S An element for a preform, a fiber production method and an optical fiber drawn from the preform
US10527782B2 (en) 2015-12-23 2020-01-07 Nkt Photonics A/S Hollow core optical fiber and a laser system
US10551574B2 (en) 2015-12-23 2020-02-04 Nkt Photonics A/S Photonic crystal fiber assembly
GB2583352A (en) * 2019-04-24 2020-10-28 Univ Southampton Antiresonant hollow core fibre, preform therefor and method of fabrication

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3102864B1 (en) * 2019-10-31 2021-11-12 Univ Limoges Architecture for electromagnetic waveguide
CN116002965B (en) * 2022-12-06 2024-06-11 长飞光纤光缆股份有限公司 Wire arranging die, device and method for preparing quartz image-transmitting optical fiber bundle

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004057393A1 (en) * 2002-12-20 2004-07-08 Crystal Fibre A/S Photonic band-gap optical fiber with large hollow core
US20100247046A1 (en) * 2009-03-31 2010-09-30 Imra America, Inc. Wide bandwidth, low loss photonic bandgap fibers
US20110085769A1 (en) * 2009-03-31 2011-04-14 Imra America, Inc. Wide bandwidth, low loss photonic bandgap fibers

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6968107B2 (en) * 2000-08-18 2005-11-22 University Of Southampton Holey optical fibres
JP5888966B2 (en) * 2011-12-16 2016-03-22 古河電気工業株式会社 Photonic band gap fiber manufacturing method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004057393A1 (en) * 2002-12-20 2004-07-08 Crystal Fibre A/S Photonic band-gap optical fiber with large hollow core
US20100247046A1 (en) * 2009-03-31 2010-09-30 Imra America, Inc. Wide bandwidth, low loss photonic bandgap fibers
US20110085769A1 (en) * 2009-03-31 2011-04-14 Imra America, Inc. Wide bandwidth, low loss photonic bandgap fibers

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11072554B2 (en) 2015-11-10 2021-07-27 Nkt Photonics A/S Element for a preform, a fiber production method and an optical fiber drawn from the preform
WO2017080564A1 (en) * 2015-11-10 2017-05-18 Nkt Photonics A/S An element for a preform, a fiber production method and an optical fiber drawn from the preform
US11662518B2 (en) 2015-12-23 2023-05-30 Nkt Photonics A/S Hollow core optical fiber and a laser system
US10989866B2 (en) 2015-12-23 2021-04-27 Nkt Photonics A/S Hollow core optical fiber and a laser system
US11002919B2 (en) 2015-12-23 2021-05-11 Nkt Photonics A/S Photonic crystal fiber assembly
US10551574B2 (en) 2015-12-23 2020-02-04 Nkt Photonics A/S Photonic crystal fiber assembly
US11360274B2 (en) 2015-12-23 2022-06-14 Nkt Photonics A/S Photonic crystal fiber assembly
US11474293B2 (en) 2015-12-23 2022-10-18 Nkt Photonics A/S Hollow core optical fiber and a laser system
US10527782B2 (en) 2015-12-23 2020-01-07 Nkt Photonics A/S Hollow core optical fiber and a laser system
US11846809B2 (en) 2015-12-23 2023-12-19 Nkt Photonics A/S Photonic crystal fiber assembly
US11977255B2 (en) 2015-12-23 2024-05-07 Nkt Photonics A/S Hollow core optical fiber and a laser system
GB2583352A (en) * 2019-04-24 2020-10-28 Univ Southampton Antiresonant hollow core fibre, preform therefor and method of fabrication
US11668871B2 (en) 2019-04-24 2023-06-06 University Of Southampton Antiresonant hollow core fibre, preform therefor and method of fabrication
GB2583352B (en) * 2019-04-24 2023-09-06 Univ Southampton Antiresonant hollow core fibre, preform therefor and method of fabrication

Also Published As

Publication number Publication date
GB201316795D0 (en) 2013-11-06
GB2518420B (en) 2019-05-01

Similar Documents

Publication Publication Date Title
US11034607B2 (en) Hollow-core photonic bandgap fibers and methods of manufacturing the same
EP3047318B1 (en) Hollow-core photonic bandgap fibers
Ding et al. Recent progress in low-loss hollow-core anti-resonant fibers and their applications
JP7482897B2 (en) Anti-resonant hollow core fiber, preform therefor and method of fabrication - Patents.com
Belardi Design and properties of hollow antiresonant fibers for the visible and near infrared spectral range
US11215751B2 (en) Antiresonant hollow core preforms and optical fibres and methods of fabrication
GB2518420A (en) Hollow-core photonic bandgap fibers and methods of manufacturing the same
US20050238307A1 (en) Nonlinear optical fibre method of its production and use thereof
US20100104869A1 (en) Photonic Crystal Fibers and Methods for Manufacturing the Same
US11428865B2 (en) Hollow core photonic bandgap optical fibres and methods of fabrication
CN1513121A (en) Thin walled core band-gap wave guides
Komanec et al. Hollow-core optical fibers
Wang et al. Design and analysis for large-mode-area photonic crystal fiber with negative-curvature air ring
GB2562687A (en) Hollow-core photonic bandgap fibers and methods of manufacturing the same
US20200319399A1 (en) Hollow Core Optical Fiber And Method Of Making The Same
GB2562688B (en) Methods of manufacturing hollow-core photonic bandgap fibers.
Xu et al. Crossings in photonic crystal fiber with hybrid core and design of broadband dispersion compensating photonic crystal fiber
Murawski et al. A photonic crystal fiber splice with a standard single mode fiber
JP2007041166A (en) Photonic band gap fiber and method of manufacturing the same
GB2563758A (en) Hollow-core photonic bandgap fibers and methods of manufacturing the same
GB2562971A (en) Hollow-core photonic bandgap fibers and methods of manufacturing the same
Jaroszewicz et al. Low-loss fusion splicing of single-mode fiber and a photonic crystal fiber suitable for construction of a patch cord for measurement devices
GB2562689A (en) Hollow-core photonic bandgap fibers and methods of manufacturing the same
CN114675368A (en) Photonic crystal fiber and preparation method thereof
WO2024155448A1 (en) Hollow core optical fibre with yield tolerant microstructure

Legal Events

Date Code Title Description
R108 Alteration of time limits (patents rules 1995)

Free format text: EXTENSION ALLOWED

Effective date: 20181129

Free format text: EXTENSION APPLICATION

Effective date: 20181127

R108 Alteration of time limits (patents rules 1995)

Free format text: EXTENSION APPLICATION

Effective date: 20190123

Free format text: EXTENSION ALLOWED

Effective date: 20190124

732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)

Free format text: REGISTERED BETWEEN 20220513 AND 20220518