# US 12,113,281 B2 · Broadband antenna assembly > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,113,281 B2 - Document ID: US12113281B2 - Status: Granted - Kind: B2 - Application number: 18/681,417 - Filed: 2022-08-08 - Published: 2024-08-15 - Granted: 2024-10-08 - Earliest claimed: 2021-08-06 - Assignees: Nantenna LLC - Applicants: Nantenna LLC - Inventors: Gary L. Bastin - Web page: https://patentgrep.com/patent/US12113281B2 ## CPC - H01Q 19/108: {Combination of a dipole with a plane reflecting surface (H01Q19/106 takes precedence; strip line H01Q9/065)} - H01Q 9/285: {Planar dipole (H01Q9/065 takes precedence; patch antenna H01Q9/0407)} - H01Q 15/006: {Selective devices having photonic band gap materials or materials of which the material properties are frequency dependent, e.g. perforated substrates, high-impedance surfaces} - H01Q 19/185: wherein the surfaces are plane - H01Q: ANTENNAS, i.e. RADIO AERIALS (radiators or antennas for microwave heating H05B6/72) ## Abstract The teachings of the present application generally for an ultra-high frequency (UHF) antenna assembly which provides for a smaller package size with the same or better efficiency as a much larger antenna, particularly between 100 MHz to 500 MHZ. Particularly, through the combination of components and structures for implementing frequency selective surfaces (FSS) and high impedance structures (HIS) in combination with an anisotropic magneto-dielectric material, the present teachings provide for the use of both lower and higher frequency techniques through the operational frequency band and miniaturization, accurately improving the performance of UHF satellite communication antennas. Specifically improving performance in narrowband, with increases in efficiency, bandwidth, and lowered elevation angle radiation characteristics. ## Claims ### Claim 1 An antenna assembly comprising: a substrate layer having a first dielectric material that is an anisotropic magneto-dielectric material; and a composite layer spaced apart from the substrate layer, the composite layer including: a first radiating element and a second radiating element on a top surface of the composite layer, the first radiating element and the second radiating element each include a transmission line folded into a stepped meander line, the stepped meander line extending between a first location and a second location along the top surface; a ground plane forming a bottom surface of the composite layer; a second dielectric material between the first and the second radiating element and the ground plane; wherein the stepped meander line includes a plurality of steps, each of the plurality of steps including a first elongated section and a second elongated section connected by a transition segment, each of the transition segments are arranged on alternating outer edges of the stepped meander line with each of the transition segments being parallel to one another. ### Claim 2 (depends on 1) The antenna assembly of claim 1, wherein the first radiating element and the second radiating element have an exponential parametric shape having a taper between the first location and the second location on the composite layer. ### Claim 3 (depends on 2) The antenna assembly of claim 2, wherein the outer edges of the stepped meander line have the exponential parametric shape. ### Claim 4 (depends on 3) The antenna assembly of claim 3, wherein each transition segment includes a notch between each of the elongated sections, wherein each of the first elongated section and each of the second elongated section have a first end and a second end, the first end and the second end have an angled profile corresponding to the exponential parametric shape, the notch of the transition segments proximally extending in from first elongated section toward the second elongated section while the angled profile of first elongated section and the second elongated section remain parallel. ### Claim 5 (depends on 4) The antenna assembly of claim 4, wherein the elongated sections each have a self-resonance frequency which cancels a radiated transmission of each corresponding elongated section, and wherein each of the transition segments radiate energy parallel along the parametric shape. ### Claim 6 (depends on 5) The antenna assembly of claim 5, wherein the transmission line of the first radiating element has an equal length to the transmission line of the second radiating element, and wherein the first radiating element is congruent with the second radiating element. ### Claim 7 (depends on 2) The antenna assembly of claim 2, wherein the bottom surface of the composite layer defines a plurality of bandgaps, the plurality of bandgaps defined by the ground plane, the ground plane including at least one first bandgap and at least one second bandgap, wherein the at least one first bandgap inhibits circulating ground currents at a first frequency range, and the at least one second bandgap inhibits circulating ground currents at a second frequency range. ### Claim 8 (depends on 7) The antenna assembly of claim 7, wherein the at least one first bandgap and the at least one second bandgap form a high impedance structure in the ground plane throughout an operational frequency band, causing the ground plane to be a frequency selective surface, reducing loss of radiation by decreasing circulating ground currents at the first frequency range and the second frequency range. ### Claim 9 (depends on 8) The antenna assembly of claim 8, wherein the first frequency range overlaps with the second frequency range. ### Claim 10 (depends on 8) The antenna assembly of claim 8, wherein exponential parametric taper of the first radiating element and the second radiating element reduce transmission speed of energy while widening the operational frequency band working in conjunction with the at least one first bandgap and the at least one second bandgaps to electromagnetically decouple the first radiating element and the second radiating element with respect to each other throughout the operational frequency band, providing the antenna assembly with a physically small size relative to the operational frequency band. ### Claim 11 (depends on 7) The antenna assembly of claim 7, wherein the first bandgap is a defected bandgap that reduces fall off of the first frequency range by 20 percent to 50 percent; and the second bandgaps is a photonic bandgap configured to reduces fall off of the second frequency range by 20 percent to 50 percent. ### Claim 12 (depends on 1) The antenna assembly of claim 1, wherein the plurality of steps of each of the first radiating element and second radiating element progressively extend in expanse between the first location and the second location on the composite layer, such that the first elongated section has a shorter length than the second elongated section, and the second elongated section has a shorter length than a third elongated section. ### Claim 13 (depends on 1) The antenna assembly of claim 1, wherein the antenna assembly has an operational frequency of 100-500 MHZ. ### Claim 14 (depends on 1) The antenna assembly of claim 1, wherein the substrate layer is spaced apart from the ground plane by a distance. ### Claim 15 (depends on 1) The antenna assembly of claim 1, wherein the first radiating element and the second radiating element are arranged on the composite layer such that the second radiating element is orthogonal to the first radiating element forming an electrical phase shift of 90 degrees, increasing circular polarization. ### Claim 16 An antenna assembly with an operational frequency band between 100 MHz and 500 Mhz, the antenna assembly comprising: a base; a substrate layer disposed on the base, the substrate layer having an anisotropic magneto-dielectric material; and a composite layer spaced apart from the substrate layer, the composite layer including: two radiating elements on a top surface of the composite layer, each of the radiating elements each include a stepped meander line with an exponential parametric tapered shape; a ground plane forming a bottom surface of composite layer, the ground plane defining a plurality of bandgaps forming a frequency selective surface; a dielectric material between the two radiating elements and the ground plane; wherein exponential parametric taper of the two radiating elements reduce transmission speed of energy while widening an operational frequency band working in conjunction with the plurality of bandgaps to electromagnetically decouple the two radiating elements with respect to each other throughout the operational frequency band, providing the antenna assembly with a physically small size relative to the operational frequency band. ### Claim 17 (depends on 16) The antenna assembly of claim 16, wherein each of the stepped meander lines include a plurality of steps, each of the plurality of steps including a first elongated section and a second elongated section connected by a transition segment, each of the transition segments are arranged on alternating outer edges of the stepped meander line with each of the transition segments being parallel to one another. ### Claim 18 (depends on 17) The antenna assembly of claim 17, wherein the first radiating element and the second radiating element have an exponential parametric shape having a taper along each of the outer edges of the stepped meander line between the first location and the second location on the composite layer. ### Claim 19 (depends on 18) The antenna assembly of claim 18, wherein each transition segment includes a notch between each of the elongated sections, and wherein each of the first elongated sections and each of the second elongated sections have a first end and a second end, the first end and the second end have an angled profile corresponding to the exponential parametric curve, the notch of the transition segments proximally cutting in from first elongated section toward the second elongated section while the angled profile of first elongated section and the second elongated section remain parallel. ### Claim 20 (depends on 17) The antenna assembly of claim 17, wherein the plurality of bandgaps are at least one defected bandgap and at least one photonic bandgap, the plurality of bandgaps decrease magnitudes of circulating ground currents in the ground plane throughout the operational frequency band, increasing energy radiated by the two radiating elements throughout the operational frequency band, the at least one defected bandgap prevents circulating ground currents at a first frequency range, and the at least one photonic bandgap prevents circulating ground currents at a second frequency range making the ground plane a high impedance structure and a frequency selective surface.