WO2015000057A1 - Matériaux composites pour applications microondes à base de diélectrique - Google Patents

Matériaux composites pour applications microondes à base de diélectrique Download PDF

Info

Publication number
WO2015000057A1
WO2015000057A1 PCT/CA2014/000535 CA2014000535W WO2015000057A1 WO 2015000057 A1 WO2015000057 A1 WO 2015000057A1 CA 2014000535 W CA2014000535 W CA 2014000535W WO 2015000057 A1 WO2015000057 A1 WO 2015000057A1
Authority
WO
WIPO (PCT)
Prior art keywords
composite material
polymer
filler
dielectric
relative permittivity
Prior art date
Application number
PCT/CA2014/000535
Other languages
English (en)
Inventor
Mohammadreza TAYFEH ALIGODARZ
Atabak RASHIDIAN
David Mathew KLYMYSHYN
Michael Schulz
Martin Boerner
Thomas Hanemann
Original Assignee
University Of Saskatchewan
Karlsruher Institut Fur Technologie
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by University Of Saskatchewan, Karlsruher Institut Fur Technologie filed Critical University Of Saskatchewan
Publication of WO2015000057A1 publication Critical patent/WO2015000057A1/fr

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B3/00—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties
    • H01B3/18—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances
    • H01B3/30—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B32B27/20—Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/30—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • B32B27/308—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising acrylic (co)polymers
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/46—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates
    • C04B35/462—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates based on titanates
    • C04B35/465—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates based on titanates based on alkaline earth metal titanates
    • C04B35/468—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates based on titanates based on alkaline earth metal titanates based on barium titanates
    • C04B35/4682—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates based on titanates based on alkaline earth metal titanates based on barium titanates based on BaTiO3 perovskite phase
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/48—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on zirconium or hafnium oxides, zirconates, zircon or hafnates
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/48—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on zirconium or hafnium oxides, zirconates, zircon or hafnates
    • C04B35/486—Fine ceramics
    • C04B35/488—Composites
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
    • C04B35/63—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
    • C04B35/632—Organic additives
    • C04B35/634—Polymers
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00—Use of inorganic substances as compounding ingredients
    • C08K3/01—Use of inorganic substances as compounding ingredients characterized by their specific function
    • C08K3/013—Fillers, pigments or reinforcing additives
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00—Use of inorganic substances as compounding ingredients
    • C08K3/18—Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/24—Acids; Salts thereof
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B3/00—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties
    • H01B3/02—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of inorganic substances
    • H01B3/10—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of inorganic substances metallic oxides
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/0485—Dielectric resonator antennas
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2264/00—Composition or properties of particles which form a particulate layer or are present as additives
    • B32B2264/10—Inorganic particles
    • B32B2264/107—Ceramic
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/204—Di-electric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2457/00—Electrical equipment
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54—Particle size related information
    • C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5436—Particle size related information expressed by the size of the particles or aggregates thereof micrometer sized, i.e. from 1 to 100 micron
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54—Particle size related information
    • C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5445—Particle size related information expressed by the size of the particles or aggregates thereof submicron sized, i.e. from 0,1 to 1 micron
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54—Particle size related information
    • C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5454—Particle size related information expressed by the size of the particles or aggregates thereof nanometer sized, i.e. below 100 nm
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
    • C04B2235/602—Making the green bodies or pre-forms by moulding
    • C04B2235/6026—Computer aided shaping, e.g. rapid prototyping
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74—Physical characteristics
    • C04B2235/75—Products with a concentration gradient
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00—Use of inorganic substances as compounding ingredients
    • C08K3/18—Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/20—Oxides; Hydroxides
    • C08K3/22—Oxides; Hydroxides of metals
    • C08K2003/2244—Oxides; Hydroxides of metals of zirconium
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00—Specific properties of additives
    • C08K2201/002—Physical properties

Definitions

  • the embodiments described herein relate to composite materials for use in dielectric-based microwave applications and methods for fabricating microwave devices with the composite materials.
  • some embodiments relate to use of the composite material in dielectric resonator antennas.
  • a microstrip antenna consists of a metallic strip or patch placed above a grounded substrate and generally fed through a coaxial probe or an aperture.
  • DRAs dielectric resonator antennas
  • DRAs are becoming increasingly important in the design of a wide variety of wireless applications from military to medical usages, from low frequency to very high frequency bands, and from on-chip to large array applications. As compared to other low gain or small metallic structure antennas, DRAs offer higher radiation efficiency (due to the lack of surface wave and conductor losses), larger impedance bandwidth, and compact size. DRAs also offer design flexibility and versatility. Different radiation patterns can be achieved using various different geometries or resonance modes, wideband or compact antennas can be provided by different dielectric constants, and excitation of DRAs can be achieved using a wide variety of feeding structures.
  • microstrip antennas are still extensively used for low-gain microwave applications.
  • the widespread use of microstrip antennas may stem primarily from the relatively low fabrication cost of the modern printed-circuit technology used to manufacture these antennas.
  • ceramic-based DRAs can involve a more complex and costly fabrication process due in part to their three-dimensional structure and in part due to the difficulty of working with the ceramic materials.
  • DRAs have been mostly limited to simple structures (such as rectangular and circular shapes).
  • a composite material with dielectric properties for use in microwave applications comprising a filler with a relative permittivity of at least 4, and a polymer constituent, wherein the composite material has a relative permittivity of at least 3 for microwave frequencies.
  • the filler comprises a ceramic constituent.
  • the microwave frequencies have a range of 0.3 GHz to 300 GHz.
  • the microwave applications comprise dielectric resonator applications. In some embodiments, the microwave applications comprise dielectric resonator antenna applications.
  • the filler and the polymer constituent form a mixture.
  • the mixture is homogeneous.
  • the mixture is inhomogeneous.
  • the filler is distributed at a gradient or other varying profile in the inhomogeneous mixture.
  • the composite material comprises a plurality of layers, and at least one of the layers comprises a different mixture than the respective other layers.
  • the filler comprises particles having a mean diameter corresponding to at least 1/10 of a minimum size of a functional pattern of the microwave application.
  • the filler is a powder prior to mixing with the polymer constituent.
  • the filler comprises a material with a high dielectric constant ⁇ . In some embodiments, the filler has a relative permittivity greater than 1000. In some embodiments, the filler has a relative permittivity of at least 4. In some embodiments, the filler has a relative permittivity between 4 and 10000.
  • the filler constitutes at least 5% by weight of the composite material. In some embodiments, the filler constitutes less than 70% by weight of the composite material.
  • the filler constitutes at least 3% by volume of the composite material. In some embodiments, the filler constitutes less than 80% by volume of the composite material. [20] In some embodiments, the polymer constituent has a relative permittivity less than 5 when in substantially pure form.
  • the polymer constituent comprises a resin.
  • the resin comprises a thermosetting material.
  • the polymer constituent comprises a curable polymer.
  • the polymer constituent comprises a positive photoresist polymer, for instance comprising polymethyl methacrylate (PMMA).
  • the polymer constituent comprises a negative photoresist polymer, for instance comprising SU-8.
  • a dielectric resonator antenna for use in microwave applications, the dielectric resonator antenna comprising: a substrate with at least a first planar surface; a resonator body disposed on the first planar surface, the resonator body formed of the composite material described herein; and an excitation structure for exciting the resonator body.
  • the resonator body has a thickness in a range of 1 to 6000 microns.
  • the resonator body is comprised of one or more layers of composite material stacked vertically.
  • the resonator body is comprised of one or more laterally defined segments of composite material.
  • a method of fabricating a composite material for use in microwave dielectric applications comprising mixing a filler with a relative permittivity of at least 4, and a polymer constituent to form the composite material, wherein the composite material has a relative permittivity of at least 3 for microwave frequencies.
  • fabricating a composite material further comprises curing the composite material at a temperature below about 100°C.
  • fabricating a composite material further comprises curing the composite material at a temperature below about 65°C.
  • mixing the filler and the polymer constituent further comprises compounding the filler and the polymer constituent. [32] In some embodiments, mixing the filler and the polymer constituent further comprises stirring the filler and the polymer constituent.
  • a method of fabricating a dielectric resonator antenna comprising providing a substrate with at least a first planar surface; providing a mold on the substrate, the mold defining a cavity therewithin; depositing the composite material described herein within the cavity.
  • the mold comprises a polymer-based material.
  • the deposited composite material has a thickness in a range of 1 to 6000 microns.
  • the deposited composite material is comprised of one or more layers stacked vertically.
  • each of at least one cavity defines one or more laterally defined segments of deposited composite material.
  • liquid crystal polymer or an LCP composite is deposited within the cavity.
  • a further polymer layer may be applied to the top of the cavity.
  • the mold is provided by forming a polymer-based body; exposing the polymer-based body to a lithographic source via a pattern mask, wherein the pattern mask defines the cavity to be formed in the polymer-based body; developing a portion of the polymer-based body; and removing one of an exposed portion and an unexposed portion of the polymer-based body to reveal the cavity.
  • the exposed portion is removed.
  • the inverse cavity structure will result.
  • the method of fabricating a dielectric resonator antenna further comprises removing the mold to leave the composite material.
  • the mold is retained as one of a protective frame and a packaging.
  • the composite material is deposited by injection.
  • FIG. 1A illustrates a third order Koch Island fractal structure polymer-based antenna element fabricated with deep X-ray lithography
  • FIG. 1 B illustrates the antenna element of FIG. 1A at a higher magnification showing sidewall detail
  • FIGS. 2A and 2B illustrate exemplary plots of the relative permittivity and dielectric loss tangent for pure polymethyl methacrylate (PMMA), as a function of frequency;
  • FIGS. 3A and 3B illustrate exemplary plots of the relative permittivity and dielectric loss tangent for SU-8, as a function of frequency
  • FIGS. 4A and 4B illustrate exemplary plots of the relative permittivity and dielectric loss tangent for pure polyester-styrene (PSS) and an example composite material based on PSS with Barium Titanate comprising 50% of the composite by weight, as a function of frequency;
  • PSS polyester-styrene
  • Barium Titanate an example composite material based on PSS with Barium Titanate comprising 50% of the composite by weight, as a function of frequency
  • FIGS. 5A and 5B illustrate an example dielectric resonator antenna formed using composite materials described herein;
  • FIGS. 6A and 6B illustrate examples of resonator bodies formed using composite materials described herein;
  • FIG. 7 illustrates a plan view of another example dielectric resonator antenna
  • FIG. 8 illustrates a plot of frequency responses of exemplary dielectric resonator antennas formed using composite materials described herein;
  • FIG. 9 illustrates an exploded isometric view of an example dielectric resonator antenna
  • FIGS. 10A and 10B illustrate an example mold for fabricating dielectric applications using composite materials described herein.
  • the dielectric applications may include dielectric resonator applications and dielectric resonator antennas (DRAs).
  • the composite materials include a filler with high relative permittivity (e.g., a ceramic constituent) and a polymer constituent. When the filler and the polymer constituent are mixed, the resulting composite materials can offer desirable performance characteristics and can facilitate greater use of dielectric applications in commercial operations.
  • the compact RF antennas enable improved performance and increased functionality for various emerging wireless communication and sensor devices (e.g., miniature radios/transmitters, personal/wearable/embedded wireless devices, etc., automotive radar systems, small satellites, RFID, sensors and sensor array networks, and bio-compatible wireless devices and biosensors).
  • An example direct fabrication of the composite material is described by Muller et al. in "Fabrication of ceramic microcomponents using deep X-ray lithography" (Microsystem Technologies, vol.1 1 , pp. 271 -277; Published: April 1 , 2005).
  • the composite materials described herein facilitate easier fabrication of devices such as antennas, while retaining many of the benefits of ceramic-based materials.
  • the natural softness of polymers can dramatically simplify fabrication of dielectric elements, for example by enabling the use of lithographic batch fabrication (e.g., X-ray lithography, UV lithography, stereo lithography, e-beam lithography, laser lithography, etc.) or other fabrication, printing or micromachining processes used to form elements of the present devices.
  • Examples of other processes include known microwave and antenna manufacturing techniques in addition to known semiconductor manufacturing techniques, additive techniques (3D printing, masking, casting, screen printing, electroplating, extrusion, vacuum deposition, etc.), subtractive techniques (etching, ablation, laser cutting, milling, cutting, erosion, etc.), and other technologies.
  • additive techniques 3D printing, masking, casting, screen printing, electroplating, extrusion, vacuum deposition, etc.
  • subtractive techniques etching, ablation, laser cutting, milling, cutting, erosion, etc.
  • the composite materials require that the resulting dielectric materials be effectively excited to guide, resonate and/or radiate at microwave frequencies.
  • the use of a polymer-based component in the composite material can dramatically simplify fabrication of devices due to the natural softness of the polymer-based materials.
  • the use of polymer-based materials can provide wide impedance bandwidth, given very low relative permittivity of the polymer materials used.
  • various diverse polymer types with selected parameters can be used to fulfill the requirements of particular applications or to achieve desired performance characteristics.
  • elastic polymers e.g. polydimethylsiloxane (PDMS)
  • PDMS polydimethylsiloxane
  • known photolithographic techniques have evolved to enable fabrication of passive devices with small features.
  • Use of photoresist polymers (e.g., polymethyl methacrylate or PMMA) and/or photosensitive polymers may therefore facilitate lithographic fabrication of precise features on DRAs.
  • X-ray lithography has been found to be a suitable fabrication technique to enable the patterning of tall structures in thick materials with suitable precision and batch fabrication ability.
  • X-ray lithography is a technique that can utilize synchrotron radiation to fabricate three-dimensional structures. Structures can be fabricated with a height up to a few millimetres (e.g., typically a maximum of 3 to 4 mm with current techniques) and with minimum lateral structural features (i.e., layout patterns) in the micrometer or sub- micrometer range. As compared to other fabrication techniques such as UV lithography, X-ray lithography can produce much taller structures (up to several millimetres) with better sidewall verticality and finer features.
  • FIGS. 1A and 1 B there are shown exemplary scanning electron microscope (SEM) images of a polymer-based antenna element 100, demonstrating the ability of X-ray lithography in fabrication of high quality miniature structures.
  • the polymer-based antenna element 100 may be formed using a composite material described herein, such as, for example, a composite incorporating a high- ⁇ ceramic material (e.g., barium titanate).
  • FIG. 1A illustrates a third order Koch Island fractal structure polymer-based antenna element 100 fabricated with deep X-ray lithography.
  • Antenna element 100 shown in FIGS. 1A and 1 B has a thickness of 1.8 mm, excellent sidewall verticality, typically better than 89.7°, and smooth sidewalls.
  • FIG. 1 B illustrates the same antenna element 100 at a higher magnification showing sidewall detail.
  • X-ray lithography may also be used to fabricate tall metallic structures (e.g., capacitors, filters, transmission lines, cavity resonators, and couplers, etc.) and therefore can allow for the fabrication of integrated metal and dielectric structures, including polymer-based resonator antenna circuits (e.g., array structures, feeding networks, and other microwave components), on a common substrate.
  • tall metallic structures e.g., capacitors, filters, transmission lines, cavity resonators, and couplers, etc.
  • polymer-based resonator antenna circuits e.g., array structures, feeding networks, and other microwave components
  • X-ray lithography can use more energetic and higher frequency radiation than more traditional optical lithography, to produce very tall structures with minimum dimension sizes smaller than one micron.
  • X-ray lithography fabrication comprises a step of depositing or gluing a photoresist material on a substrate, exposing the synchrotron radiation through a mask, and developing the material using a suitable solvent or developer.
  • X-ray lithography can also be an initial phase of the so-called LIGA process, where LIGA is the German acronym for Lithographie, Galvanoformung, Abformung (lithography, electrodeposition, and moulding).
  • LIGA is the German acronym for Lithographie, Galvanoformung, Abformung (lithography, electrodeposition, and moulding).
  • a LIGA process may further comprise electroforming of metals and moulding of plastics, which is not strictly required to produce dielectric structures.
  • Suitable polymer-based materials for X-ray lithography microfabrication can be selected so that the deposition process is simplified, and to exhibit sensitivity to X-rays in order to facilitate patterning.
  • pure photoresist polymer materials may best facilitate X-ray lithography fabrication.
  • photoresist materials suitable for X- ray lithography include PMMA and Epon SU-8.
  • PMMA is a positive one-component resist commonly used in electron beam and X-ray lithography. It may exhibit relatively poor sensitivity, thus requiring high exposure doses to be patterned. However, the selectivity (i.e., contrast) achievable with specific developers can be very high, resulting in excellent structure quality. Very thick PMMA layers are sometimes coated on a substrate by gluing. However, patterning thick layers may require hard X-rays and special adjustments for beamline mirrors and filters.
  • PMMA exhibits relatively little absorption in the ultraviolet spectrum, which can make it less desirable as a candidate for optical lithography. However, PMMA exhibits excellent optical transparency in the visible light range, which makes it useful in micro- optics applications.
  • FIGS. 2A and 2B there shown a plot 200 of the relative permittivity for pure PMMA and a plot 250 of the dielectric loss tangent for pure PMMA, as a function of frequency, respectively.
  • These electrical properties of PMMA were measured using the two-layer microstrip ring resonator technique.
  • the relative permittivity and dielectric loss tangent were measured to be 2.65 and 0.005, respectively.
  • the relative permittivity decreases with increased frequency, reaching 2.45 at 40 GHz.
  • the dielectric loss tangent increases with increased frequency, reaching 0.02 at 40 GHz.
  • the low relative permittivity of pure PMMA may make it less suitable for some dielectric applications, such as antennas.
  • Epon SU-8 is a negative three-component resist suitable for ultraviolet and X-ray lithography. SU-8 exhibits maximum sensitivity to wavelengths between 350-400 nm. However, the use of chemical amplification allows for very low exposure doses. Accordingly, SU-8 may also be used with other wavelengths, including X-ray wavelengths between 0.01-10 nm.
  • the dielectric constant of SU-8 has been reported as between 2.8 and 4.
  • the variation in these reported electrical properties may be due to several factors, including use of different commercial types of SU-8 (e.g. SU-8(5), SU-8(10), SU-8(100), etc.), pre-bake and post-bake conditions (e.g. time and temperature), and exposure dose. Accordingly, the use of SU-8 may require careful characterization of the electrical properties for a particular selected type of SU-8 and corresponding adjustment of fabrication steps.
  • FIGS. 3A and 3B there shown a plot 300 of the relative permittivity for SU-8 and a plot 350 of dielectric loss tangent for SU-8, as a function of frequency, respectively.
  • These electrical properties of SU-8 were independently measured using the two-layer microstrip ring resonator technique.
  • the relative permittivity and dielectric loss tangent were measured to be 3.3 and 0.012, respectively.
  • the relative permittivity decreases with increased frequency, reaching 3.1 at 40 GHz.
  • the dielectric loss tangent increases with increased frequency, reaching 0.04 at 40 GHz.
  • pure photoresist materials may be less than optimal for some dielectric applications, such as microwave and antenna applications, since pure polymer materials generally have low relative permittivity.
  • Certain fabrication techniques, such as X-ray lithography fabrication, for example, can be modified and optimized for different materials and structural requirements. Accordingly, materials used in dielectric applications can be selected to satisfy both lithographic properties required for the various fabrication techniques, and the resultant electrical properties of the fabricated device.
  • the electrical characteristics to be selected include relative permittivity and dielectric loss.
  • a dielectric material can perform as a suitable antenna if the material has fairly high relative permittivity and low loss (e.g., relative permittivity that is typically greater than 5 and loss tangent typically less than 0.1).
  • the polymer constituent of a composite material can be a photochemically or thermally hardenable polymer that has a relative permittivity that is typically less than 5 when in substantially pure form.
  • the polymer constituent may include at least one of synthetic resin or curable polymer.
  • the resin may include a polyester-based material (such as polyester styrene).
  • the resin may be thermosetting and include a hardener material, and the curable polymer may be a positive or negative photoresist polymer.
  • a mold is provided by forming a polymer-based body; exposing the polymer-based body to a lithographic source via a pattern mask, such that the pattern mask defines the cavity to be formed in the polymer-based body; and developing a portion of the polymer- based body and removing either an exposed portion of the polymer-based body or an unexposed portion of the polymer-based body to reveal the cavity.
  • the exposed portion of the polymer-based body is removed.
  • the inverse process is used such that the pattern mask defines the material to be retained and therefore, an unexposed portion of the polymer-based body is removed to reveal the cavity.
  • a filler material with a higher relative permittivity can be used in order to enhance the dielectric properties of the composite material.
  • a filler such as a ceramic constituent can have a relative permittivity greater than 9 when the ceramic constituent is in substantially pure solid form.
  • the relative permittivity of the composite material can be selected to be at least 3 for microwave frequencies, which is generally a practical lower limit for microwave applications. For example, in the case of DRAs, a relative permittivity of at least 3 is generally required to excite the resonant elements.
  • a practical upper limit for the relative permittivity may be the ⁇ value for pure Barium Titanate (1250 ⁇ ⁇ ⁇ 10000, depending on frequency and temperature), because an ideal composite would consist of very high filler loads approaching that of a pure ceramic.
  • Another practical upper limit may be the ⁇ value for BaTi0 3 in Polyimide (k > 125 @ 10 Hz), as this describes a real composite, and ⁇ generally decreases with increasing frequency.
  • the ⁇ value for BaTiO 3 in Polyimide was described by Devaraju et al. in "The Synthesis and Dielectric Study of BATi0 3 /polyimide nanocomposite films" (Microelectronic Engineering, vol. 82, pp.
  • the filler may include structural or functional ceramics.
  • the filler may include high-K materials with a relative permittivity between 4 and 1000 (e.g. zirconia, alumina) or above 10 3 (perowskite-type ceramics e.g. barium titanate, potassium sodium tartrate, barium strontium titanate, etc.).
  • the filler can be in a range of 5-70% of the weight of the composite material. In some other embodiments, the filler can be in a range of 3- 80% of the volume of the composite material.
  • the composite material can be fabricated by mixing the filler with the polymer constituent using a mixer device with variable speed settings. The step of mixing the composite material may include at least one act of compounding or stirring the filler and the polymer constituent, and may involve the use of other materials to aid in mixing.
  • a certain amount of dispersant may be added to the polymer constituent, based on the weight of the polymer constituent.
  • the amount and type of dispersant may vary depending on the characteristics of the polymer and filler constituents.
  • the polymer constituent and the dispersant may be mixed for a desired period of time. The time and the mixing environment (speed, temperature, etc.) will depend on the specific constituents.
  • a hardener material may also be added to the mixture of the polymer constituent and the filler to facilitate the setting of the composite material.
  • the amount of hardener material may correspond to values as recommended by the vendor of the hardener material.
  • the hardener material is mixed with the mixture of the polymer constituent and the filler. To remove air bubbles, the mixture of the polymer constituent and the filler may be placed in a vacuum prior to or after the hardener material is added. Ultrasonic agitation can also assist in removing air bubbles.
  • the mixture should be baked as the final step of material preparation.
  • the baking of the mixture may occur at a temperature below 100°C.
  • the baking of the mixture may occur at a temperature below 65°C.
  • the size of filler particles suitable for use in a composite material is generally related to a functional pattern size for the dielectric application.
  • the size of the filler particles may correspond to a minimum size of the functional pattern for the dielectric application.
  • filler particles may be selected to have a size of 1/10 of the resonator body of a DRA, in one or both dimensions perpendicular to a feeding structure, in order to produce useful anisotropies that can improve antenna performance.
  • the filler material may be provided in the shape of a disc.
  • the filler material may also include one or more layers.
  • the filler material may be oriented with an elongate portion substantially perpendicular to the feeding structure of the dielectric resonator antenna.
  • the ceramic particles may include ceramic powder, micro-powder and/or nano-powder.
  • the ceramic constituent may include ceramic particles having a size determined by the functional pattern size for the dielectric application and elements of the antenna.
  • the ceramic constituent may have a mean diameter in a range of 50 nm to 5 m prior to being mixed with the polymer constituent.
  • the ceramic constituent may have a mean diameter in a range of 300nm to 900nm.
  • the composite material may also include other fillers, such as fiber materials, carbon nanotubes and CdS nanowires and active ferroelectric materials, which can be selected to form materials with desired properties, such as enhanced tunability or power-harvesting ability.
  • the resulting composite materials can provide a broader group of viable materials suitable for dielectric applications. In some cases, the use of such composites may alter photoresist properties, requiring adjustment of lithographic processing, or additional steps in the fabrication process.
  • An example of a composite material is a PSS composite incorporating Barium Titanate (BaTiO 3 ).
  • the BaTiO 3 may comprise 30-60% of the composite material by weight.
  • FIGS. 4A and 4B there is shown a plot 400 of the relative permittivity and a plot 450 of the dielectric loss tangent as a function of frequency for a composite based on PSS and BaTi03 comprising 50% of the composite material by weight.
  • These electrical properties of the PSS and BaTiO 3 composite were measured up to 1.5 GHz using an AgilentTM 4291 B RF Impedance/Material Analyzer.
  • the electrical properties of the PSS and BaTi0 3 composite at 8.5 GHz were also measured using Agilent's 85070E dielectric probe kit and are provided in the table below:
  • Table 1 Electrical Properties of PSS/ BaTiO 3 Composite at 8.5GHz [85] As illustrated in FIG. 4A and Table 1 , compared to the relative permittivity of pure PSS, improvements are observable for the PSS and BaTi0 3 composite. For example, as shown in FIG. 4A, the relative permittivity at 1 GHz is about 8 for the PSS and BaTi0 3 composite, compared to approximately 2 for pure PSS. Similarly, as provided in Table 1 , each of the relative permittivity at 8.5GHz for the various PSS and BaTi0 3 composites is substantially higher than the relative permittivity of pure PSS.
  • a composite material can include PSS and Zirconia (ZrO 2 ). Unlike the PSS and BaTi0 3 composite material, the PSS and Zirconia composite material may not yield a sufficiently high relative permittivity to be used in a monolithic dielectric antenna application. Instead, the PSS and Zirconia composite material may be used in the fabrication of multi-segment structures for which a lower relative permittivity might be needed. Electrical properties of an example PSS and Zirconia composite measured at 8.5 GHz using an AgilentTM 85070E dielectric probe kit are provided in the table below: Ceramic Permittivity
  • the relative permittivity of the PSS/ZrO 2 composite is generally less than the relative permittivity of the PSS/ BaTi0 3 composite.
  • a PSS/ BaTi0 3 composite with 50% BaTi0 3 by weight has a relative permittivity in the range of 7.2-7.6
  • a PSS/Zr0 2 composite with 50% Zr0 2 by weight has a relative permittivity in the range of 5.7-6.0.
  • the filler and the polymer constituent may form a mixture.
  • the mixture may be homogeneous or inhomogeneous.
  • An inhomogeneous mixture may result from delaying a pre-baking process of the composite mixture, since particles tend to move to a lower region of the composite mixture before drying, or through a controlled and gradual change of a density of the filler.
  • the use of the inhomogeneous mixture as the composite material can provide additional advantages to dielectric applications. For example, for antenna applications, each of the impedance bandwidth, the coupling level, and the realized gain of the antenna can be enhanced, and the cross-polarization patterns may be improved. These improvements to the antenna applications may result from constituents in the composite material providing an impedance transformer through one of the segments. As well, improvements in antenna applications may be realized from constituents in the composite material having suitable polarizations and directions such that the electric near-field patterns exhibit desirable characteristics.
  • the filler in the inhomogeneous mixture can be distributed within the composite material based on its weight.
  • the filler can be distributed in one or more layers of the inhomogeneous mixture.
  • one or more different types of composite materials may be stacked one over the other.
  • the filler can be distributed at a gradient or other similar distribution profiles in the inhomogeneous mixture.
  • the distribution profiles may include a linearly increasing or decreasing density, or a logarithmically increasing or decreasing density.
  • photoresist-based polymer materials e.g., pure photoresist materials such as SU-8 and PMMA, and photoresist composite materials such as SU-8 and PMMA mixed with ceramic or other fillers.
  • photoresist-based materials are suitable for lithographic fabrication of antenna structures with precise features in thick layers, particularly if they facilitate the use of deep penetrating lithographies, such as thick resist UV lithography or deep X-ray lithography (DXRL).
  • DRAs generally include a substrate with at least a first planar surface on which a resonator body is disposed and an excitation structure for exciting the resonator body.
  • the resonator body may be formed using the composite material described herein.
  • the resonator body may have a thickness in a range of 1 to 6000 microns.
  • Various fabrication methods may be employed, including direct fabrication, or by injecting the composite materials into lithographically fabricated molds or templates formed of photoresist materials, for fabricating DRAs using the composite material described herein.
  • direct fabrication or by injecting the composite materials into lithographically fabricated molds or templates formed of photoresist materials, for fabricating DRAs using the composite material described herein.
  • the use of such molds enables the use of complicated shapes with a wide range of composite materials that might otherwise be very difficult to produce using other fabrication techniques.
  • LCP liquid crystal polymer
  • LCP is not generally a "curable” polymer, it may also be injected into mold structures, as a low-loss microwave dielectric material for high frequencies.
  • a composite or polymer "lid” layer may be provided to hold the LCP within the mold after fabrication.
  • DRA 500 comprises a ground layer 510, substrate 525, feedline 515, and a resonator body 532.
  • DRA 500 is illustrated with a microstrip feeding structure, however other arrangements, feeding structures and shapes may be used.
  • a DRA formed using the composite materials as described herein may benefit from high relative permittivity, more conventional feeding structures, such as a coplanar transmission line coupling, slot coupling and probe coupling can also be used.
  • Substrate 525 may be a microwave or millimeter-wave substrate material, and ground layer 510 may be attached to this substrate material.
  • substrate 525 may be, for example, a layer of alumina, glass, or silicon that may be doped in accordance with the process requirements.
  • FIGS. 6A and 6B in which there are shown different embodiments of the resonator body 532 formed from the composite material described herein.
  • a resonator body 532a may comprise a single layer 610 of the composite material.
  • a resonator body 532b may comprise multiple layers, such as layers 610a to 610c, shown stacked vertically. It will be understood that a resonator body 532 may be formed using fewer or more layers of the composite material described herein.
  • the composite material in each layer 610 (or 610a to 610c) of the resonator body 532 may comprise a filler that is uniformly distributed, distributed at a gradient or otherwise distributed according to a distribution profile.
  • the distribution profile may include a gradual variation in one or more dimensions, linear variation or nonlinear variation.
  • Variations in the distribution profile produce anisotropy, which can significantly improve polarization of an antenna and its pattern.
  • anisotropic composites can also be fabricated by exploiting anisotropy of the filler material or its orientation within the composite material.
  • FIG. 7 there is shown a plan view of another example DRA 700. Similar to DRA 500, DRA 700 is illustrated with a microstrip feeding structure. However, unlike DRA 500, feedline 715 of DRA 700 extends into resonator body 732 by a feedline extension portion 770. [103] FIG. 8 is a plot illustrating frequency responses of three different microstrip-fed DRAs formed using the composite material described herein.
  • the dimensions of the components of the three different DRAs are consistent.
  • the resonator body has a length of 2mm, a width of 2mm and a height of 0.9mm.
  • the dimension of the substrate is 8mm x 8mm and a width of the feedline is 1.2mm.
  • the substrate has a thickness of 0.381 mm and a relative permittivity of 2.2.
  • the feedline extension portion is 0.4mm.
  • the resonant frequency is also fixed at approximately 50 GHz.
  • Frequency response 810 is generated by simulating a DRA with a resonator body formed using a composite material with a uniformly distributed filler and a relative permittivity of 5.5.
  • the filler may include BaTi0 3 which comprises 30% by weight of the composite material.
  • the return loss at the resonant frequency is barely -12.9 dB.
  • the DRA associated with the frequency response 810 therefore, is minimally excited by the microstrip feed.
  • Frequency response 820 is generated by a DRA with a resonator body formed using a composite material comprising a filler that is distributed according to a linearly varied gradient.
  • the composite material has a relative permittivity that varies in a direction substantially perpendicular to a planar surface of the substrate, such as the Z- direction, from 7.5 to 3.5.
  • the filler comprises inhomogeneous BaTiO 3 .
  • the return loss at resonance is -20 dB.
  • the DRA associated with the frequency response 820 also has a 10 dB bandwidth of 17% from 46 GHz to 54.5 GHz,
  • the coupling level of a DRA formed using the composite material described herein may increase with the use of a filler that is more inhomogeneous and non-uniformly distributed within the composite material.
  • a further example is illustrated with frequency response 830.
  • Frequency response 830 is generated by a DRA with a resonator body formed using five layers of composite material.
  • each of the five layers comprises a different composite material, namely BaTi0 3 at 60% by weight of the composite material with a relative permittivity of 10, BaTiO 3 at 50% by weight of the composite material with a relative permittivity of 7.5, ZrO 2 at 50% by weight of the composite material with a relative permittivity of 5.7, Zr0 2 at 35% by weight of the composite material with a relative permittivity of 4.6, and pure PSS with a relative permittivity of 2.5.
  • the return loss at resonance for the associated DRA is -32 dB.
  • the DRA associated with the frequency response 830 also has a 10 GHz bandwidth.
  • Some dielectric applications such as those for military uses, require a return loss of at least -20dB.
  • the DRA associated with the frequency response 830 therefore, exhibits dielectric characteristics that are suitable for military applications.
  • FIG. 9 there is shown an exploded isometric view of another example DRA 900 formed using the composite material described herein.
  • DRA 900 comprises a ground layer 910, substrate 925, feedline 915, and a resonator body 932.
  • DRA 900 unlike DRA 500, comprises a tall metal vertical feeding structure 920.
  • Mold 950 may be a first body portion that defines an aperture or cavity 952 therein.
  • the mold 950 may be formed of a photoresist material if fabricated in a lithographic process.
  • Aperture 952 can be filled with a resonator body 932, or second body portion, which may be comprised of a composite dielectric material.
  • resonator body 932 has a higher relative permittivity than mold 950.
  • the cavity may be filled with one or more different composite materials.
  • the cavity may therefore define multiple lateral segments of composite materials.
  • mold 950 may be removed in a later stage of fabrication, although in other embodiments the mold 950 can be retained.
  • Resonator body 932 may have a square or rectangular topology. In other embodiments, different shapes can be used, such as circular, fractal, or other complex shapes. Due to the use of the mold 950 and the filling technique used to form resonator body 932, materials that would not ordinarily be suitable for use in a lithographic fabrication process, such as non-photoresist polymers and composites, can be used to form resonator body 932.
  • Feeding structure 920 can have a substantially flattened rectangular shape and be positioned near to the outer wall of resonator body 932, and either outside or inside the inner wall of mold 950, so that the elongated edge of feeding structure 920 is substantially parallel to the outer wall. In some alternative embodiments, feeding structure 920 can have other lateral shapes and positioning, as described herein.
  • Mold 950 need not necessarily have a "thin” or “narrow” wall structure as depicted in FIG. 9, and in some embodiments the walls of mold 950 may be relatively thick, extending in one or more directions for a large distance. In some cases, mold 950 may comprise larger sheets of photoresist material (e.g., "hole templates"), in which the "hole templates" can be filled with polymer-composite materials (and, where the low permittivity photoresist template sheet may remain following fabrication).
  • photoresist material e.g., "hole templates”
  • Feeding structure 920 is formed of a conductive material (e.g., metal) and extends substantially perpendicularly from the surface of substrate 925. That is, feeding structure 920 can be 10-100% the height of mold 950.
  • a conductive material e.g., metal
  • Feeding structure 920 is electrically coupled to feedline 915, and may have a width generally corresponding to the width of feedline 915.
  • dielectric resonator antennas can be fabricated using non-lithographic techniques, but employing the same mold approach illustrated in FIG. 9.
  • a mold can be formed having one or more recesses for receiving the composite material.
  • the recesses can have a rectangular shape or other shapes, such as circular or partial circular.
  • Mold 1000 has a main body 1010 that may be formed of a plastic material, such as PMMA or any other plastics.
  • Example recesses 1002a to 1002h are formed in mold 1000 in the main body 1010.
  • the recesses 1002 may be formed of various different shapes and sizes. It will be understood that the illustrated recesses 1002 are merely for illustrative purposes and that different configurations of the recesses may be formed in the molds.
  • the mold 1000 may be filled with the composite materials described herein using known techniques, such as injection or tape casting.
  • the fabricated DRA structure may be used with or without the mold 1000.
  • the mold 1000 may be retained after the DRA structure is fabricated as a protective frame or as a packaging.
  • various known methods may be applied.
  • the mold 1000 may be removed using a lift-off process with carbon coated wafers or via X-ray exposure if mold 1000 is formed of a photoresist- type polymer.
  • a sacrificial substrate or release layer (film) holding the mold may also be dissolved to release the mold.
  • the fabricated molds with filled composite materials can be lapped/polished to control the final structure height add/or improve the top surface quality/homogeneity.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Structural Engineering (AREA)
  • Composite Materials (AREA)
  • Health & Medical Sciences (AREA)
  • Polymers & Plastics (AREA)
  • Medicinal Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Physics & Mathematics (AREA)
  • Control Of Motors That Do Not Use Commutators (AREA)

Abstract

L'invention concerne des matériaux composites ayant des propriétés diélectriques pour une utilisation dans des applications microondes, et des procédés de fabrication. Les matériaux composites incluent une charge, par exemple une céramique, à permittivité relative élevée, ainsi qu'un constituant polymère. Le matériau composite résultant a une permittivité relative convenant à une utilisation dans des applications microondes. Des antennes de résonateur diélectrique utilisant le matériau composite sont également décrites.
PCT/CA2014/000535 2013-07-03 2014-07-03 Matériaux composites pour applications microondes à base de diélectrique WO2015000057A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201361842587P 2013-07-03 2013-07-03
US61/842,587 2013-07-03

Publications (1)

Publication Number Publication Date
WO2015000057A1 true WO2015000057A1 (fr) 2015-01-08

Family

ID=52142955

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CA2014/000535 WO2015000057A1 (fr) 2013-07-03 2014-07-03 Matériaux composites pour applications microondes à base de diélectrique

Country Status (1)

Country Link
WO (1) WO2015000057A1 (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9966180B2 (en) 2016-01-22 2018-05-08 Raytheon Company Impedance transformer
US10340599B2 (en) 2013-01-31 2019-07-02 University Of Saskatchewan Meta-material resonator antennas
US10361487B2 (en) 2011-07-29 2019-07-23 University Of Saskatchewan Polymer-based resonator antennas
EP3561957A1 (fr) * 2015-10-28 2019-10-30 Rogers Corporation Antenne de résonateur diélectrique à large bande et à couches multiples et son procédé de fabrication
WO2019222584A1 (fr) * 2018-05-17 2019-11-21 Curators Of The University Of Missouri Matériau composite à constante diélectrique élevée et utilisation dans des dispositifs biocompatibles
US10784583B2 (en) 2013-12-20 2020-09-22 University Of Saskatchewan Dielectric resonator antenna arrays
TWI739771B (zh) * 2015-10-28 2021-09-21 美商羅傑斯公司 寬頻多層介電共振器天線及其製作方法
CN115742523A (zh) * 2022-10-28 2023-03-07 山东森荣新材料股份有限公司 超低介电微波复合基板材料的制造工艺

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1767582B1 (fr) * 2004-06-16 2012-03-28 NTN Corporation Composition élastomère fortement diélectrique et antenne diélectrique
US20120245016A1 (en) * 2011-03-23 2012-09-27 The Curators Of The University Of Missouri High dielectric constant composite materials and methods of manufacture

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1767582B1 (fr) * 2004-06-16 2012-03-28 NTN Corporation Composition élastomère fortement diélectrique et antenne diélectrique
US20120245016A1 (en) * 2011-03-23 2012-09-27 The Curators Of The University Of Missouri High dielectric constant composite materials and methods of manufacture

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
CHAUDHARY ET AL.: "Wideband Two-layer Rectangular Dielectric Resonator Antenna with (Zr 0.8Sn0.2)TiO4-Epoxy Composite System", SPECIAL MATERIALS GROUP, 2011 *

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10361487B2 (en) 2011-07-29 2019-07-23 University Of Saskatchewan Polymer-based resonator antennas
US10340599B2 (en) 2013-01-31 2019-07-02 University Of Saskatchewan Meta-material resonator antennas
US10784583B2 (en) 2013-12-20 2020-09-22 University Of Saskatchewan Dielectric resonator antenna arrays
EP3561957A1 (fr) * 2015-10-28 2019-10-30 Rogers Corporation Antenne de résonateur diélectrique à large bande et à couches multiples et son procédé de fabrication
TWI739771B (zh) * 2015-10-28 2021-09-21 美商羅傑斯公司 寬頻多層介電共振器天線及其製作方法
EP3979418A1 (fr) * 2015-10-28 2022-04-06 Rogers Corporation Antenne à résonateur diélectrique large bande à multiples couches et procédé de fabrication d'antenne à résonateur diélectrique large bande à multiples couches
US9966180B2 (en) 2016-01-22 2018-05-08 Raytheon Company Impedance transformer
US10692641B2 (en) 2016-01-22 2020-06-23 Raytheon Company Method of additively manufacturing an impedance transformer
WO2019222584A1 (fr) * 2018-05-17 2019-11-21 Curators Of The University Of Missouri Matériau composite à constante diélectrique élevée et utilisation dans des dispositifs biocompatibles
US11844881B2 (en) 2018-05-17 2023-12-19 The Curators Of The University Of Missouri Composite material with high dielectric constant and use in biocompatible devices
CN115742523A (zh) * 2022-10-28 2023-03-07 山东森荣新材料股份有限公司 超低介电微波复合基板材料的制造工艺
CN115742523B (zh) * 2022-10-28 2023-07-07 山东森荣新材料股份有限公司 超低介电微波复合基板材料的制造工艺

Similar Documents

Publication Publication Date Title
CA2899236C (fr) Antennes a resonateur a base de meta-materiaux
US10361487B2 (en) Polymer-based resonator antennas
WO2015000057A1 (fr) Matériaux composites pour applications microondes à base de diélectrique
Byford et al. Demonstration of RF and microwave passive circuits through 3-D printing and selective metalization
WO2015089643A1 (fr) Réseaux d'antennes à résonateur diélectrique
US9806393B2 (en) Gap waveguide structures for THz applications
TW202124593A (zh) ３ｄ列印天線
Czarny et al. High permittivity, low loss, and printable thermoplastic composite material for RF and microwave applications
CN109075437A (zh) 使用具有图案化空腔的电介质基板的堆叠式贴片天线
Rashidian et al. Deep x-ray lithography processing for batch fabrication of thick polymer-based antenna structures
Rashidian et al. Photoresist-based polymer resonator antennas: lithography fabrication, strip-fed excitation, and multimode operation
O'Brien et al. Miniaturization of microwave components and antennas using 3D manufacturing
Whittow et al. Applications and future prospects for microstrip antennas using heterogeneous and complex 3-D geometry substrates
Rashidian et al. Photoresist-based polymer resonator antennas with permanent frame
Chappell et al. Wide bandgap composite EBG substrates
Adhiyoga et al. Magneto-dielectric properties of PDMS–magnetite composite as a candidate for compact microstrip antennas in the C-band 5G frequency
Rashidian et al. Development of polymer-based dielectric resonator antennas for millimeter-wave applications
Rashidian et al. Microwave performance of photoresist-alumina microcomposites for batch fabrication of thick polymer-based dielectric structures
JP2004048736A (ja) 不連続な伝送線における信号特性の向上を図る基板
Mazhar et al. On the fabrication of thin-film artificial metal grid resonator antenna arrays using deep X-ray lithography
Rahiminejad Microsystem technology for microwave applications at frequencies above 100 GHz
Castro Engineered Nanocomposite Materials for Microwave/Millimeter-Wave Applications of Fused Deposition Modeling
Apaydin et al. Integrated RF circuits design and packaging in high contrast ceramic-polymer composites
He Reconfigurable Microwave Electronics Using Additive Manufacturing and Magnetic Nanomaterials
Mazhar METAL EMBEDDED ARTIFICIAL GRID DIELECTRIC RESONATOR ANTENNA ARRAYS AND SIW FEEDING MECHANISMS FOR MM-WAVE APPLICATIONS

Legal Events

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

Ref document number: 14820679

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 14820679

Country of ref document: EP

Kind code of ref document: A1