Broadband wire antenna
US-2021126374-A1 · Apr 29, 2021 · US
US9831559B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9831559-B2 |
| Application number | US-201514818055-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 4, 2015 |
| Priority date | Aug 4, 2015 |
| Publication date | Nov 28, 2017 |
| Grant date | Nov 28, 2017 |
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Official abstract text for this publication.
An antenna array includes a flexible microstrip PCB feed layer and a plurality of radiating elements attached to the flexible PCB feed layer. The radiating elements comprise a Tau scalable log periodic array of low profile radiating elements for producing a monopole, end fire radiation pattern. Radiating elements include printed inverted F antenna elements and multi-arm puck elements for circular polarization. The antenna array is conformable to a curved surface. The radiating elements can be either integrated within a multi-layer flex or rigid flex PCB, or configured as individual elements that are die attached to a common ground plane flex circuit.
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What is claimed is: 1. An antenna comprising: a flexible feed layer configured to conform to a surface; and a plurality of rigid radiating elements connected to the flexible feed layer, each of the plurality of rigid radiating elements comprising: a ground plane; a dielectric substrate disposed on the ground plane; and a radiator connected to the ground plane and the flexible feed layer, wherein: the plurality of rigid radiating elements are organized into a log periodic (LP) array of concentric circles having an active boundary region, rigid radiating elements from an inner radius of the active boundary region to an outer radius of the active boundary region defining a stepped impedance. 2. The antenna of claim 1 , wherein each of the plurality of rigid radiating elements comprises a cavity-backed radiating element. 3. The antenna of claim 2 , wherein the plurality of rigid radiating elements comprises: a first set of radiating elements comprising a first type of cavity of radiating elements; and a second set of radiating elements comprising a second type of cavity of radiating elements. 4. The antenna of claim 1 , wherein a lower frequency boundary of the active region is defined by a size of a first set of radiating elements, and an upper frequency boundary of the active region is defined by a size of a second set of radiating elements, wherein the first set of radiating elements is larger than the second set of radiating elements, and the active region moves across the array in a log periodic fashion. 5. The antenna of claim 4 , wherein each of the plurality of rigid radiating elements comprise a C-disk element. 6. The antenna of claim 4 , wherein each of the plurality of rigid radiating elements comprise a printed inverted F antenna. 7. The antenna of claim 4 , wherein each of the plurality of rigid radiating elements is connected to the feed layer via a serpentine feed line, the length of the serpentine feed line between each of the plurality of rigid radiating elements corresponding to a LP scaling factor. 8. A vehicle comprising: an antenna comprising: a flexible feed layer configured to conform to a surface; and a plurality of rigid radiating elements connected to the flexible feed layer, each of the plurality of rigid radiating elements comprising: a ground plane; a dielectric substrate disposed on the ground plane; and a radiator connected to the ground plane and the flexible feed layer, wherein: the plurality of rigid radiating elements are organized into a log periodic (LP) array of concentric circles having an active region, rigid radiating elements from an inner radius of the active region to an outer radius of the active region defining a stepped impedance. 9. The vehicle of claim 8 , wherein each of the plurality of rigid radiating elements comprises a cavity-backed radiating element. 10. The vehicle of claim 8 , wherein the plurality of rigid radiating elements comprises: a first set of radiating elements comprising a first type of cavity of radiating elements; and a second set of radiating elements comprising a second type of cavity of radiating elements. 11. The vehicle of claim 8 , wherein a lower frequency boundary of the active region is defined by a size of a first set of radiating elements, and an upper frequency boundary of the active region is defined by a size of a second set of radiating element radiating elements, wherein the first set of radiating elements is larger than the second set of radiating elements, and the active region moves across the array in a log periodic fashion. 12. The vehicle of claim 8 , wherein each of the plurality of rigid radiating elements comprise an inverted F antenna. 13. The vehicle of claim 8 , wherein each of the plurality of rigid radiating elements comprise a planar inverted F antenna. 14. An antenna array comprising: a flexible feed layer configured to conform to a surface; and a plurality of rigid radiating elements connected to the flexible feed layer, each of the plurality of rigid radiating elements comprising: a ground plane; a dielectric substrate disposed on the ground plane; and a radiator connected to the ground plane and the flexible feed layer, wherein: the plurality of rigid radiating elements are organized into a log periodic (LP) array of concentric circles having an active region, rigid radiating elements from an inner radius of the active boundary region to an outer radius of the active region defining a stepped impedance; and concentric circles defining sectors, each sector corresponding to a portion of a horizon. 15. The antenna array of claim 14 , wherein a lower frequency boundary of the active region is defined by a size of a first set of radiating elements, and an upper frequency boundary of the active region is defined by a size of a second set of radiating element radiating elements, wherein the first set of radiating elements is larger than the second set of radiating elements, and the active region moves across the array in a log periodic fashion. 16. The antenna array of claim 14 , wherein each of the plurality of rigid radiating elements comprises a multi-arm inverted F puck. 17. The antenna array of claim 14 , wherein each of the plurality of rigid radiating elements comprise an inverted F antenna. 18. The antenna array of claim 14 , wherein each of the plurality of rigid radiating elements comprise a planar inverted F antenna. 19. The antenna array of claim 14 , wherein the plurality of rigid radiating elements comprises: a first set of radiating elements configured to receive signals; and a second set of radiating elements configured to transmit signals. 20. The antenna array of claim 14 , wherein each of the plurality of rigid radiating elements is connected to the feed layer via a feed line, the length of the feed line between each of the plurality of rigid radiating elements corresponding to a LP scaling factor.
providing an omnidirectional coverage (turnstile aerials H01Q21/26) · CPC title
using a dielectric support · CPC title
Substantially flat resonant element parallel to ground plane, e.g. patch antenna (dipole H01Q9/285; monopole H01Q9/40) · CPC title
with folded element, the folded parts being spaced apart a small fraction of the operating wavelength · CPC title
Particular feeding systems · CPC title
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