Low-cost satellite user terminal antenna
US-2017084994-A1 · Mar 23, 2017 · US
US11394124B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11394124-B2 |
| Application number | US-202117334507-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 28, 2021 |
| Priority date | Aug 5, 2015 |
| Publication date | Jul 19, 2022 |
| Grant date | Jul 19, 2022 |
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A radio frequency antenna array uses lenses and RF elements, to provide ground-based coverage for cellular communication. The antenna array can include two spherical lenses, where each spherical lens has at least two associated RF elements. Each of the RF elements associated with a given lens produces an output beam with an output area. Each lens is positioned with the other lenses in a staggered arrangement. The antenna includes a control mechanism configured to enable a user to move the RF elements along their respective tracks, and automatically phase compensate the output beams produced by the RF elements based on the relative distance between the RF elements.
Opening claim text (preview).
What is claimed is: 1. A communication system, comprising: at least first and second lenses within an array of lenses; the first lens has a first RF element oriented to produce a first output beam; wherein first RF element is configured for a first phase; the second lens has a second RF element oriented to produce a second output beam; wherein second RF element is configured for a second phase; wherein the array of lenses further comprises a third lens; the third lens has a third RF element oriented to produce a third output beam; wherein the third RF element is configured for a third phase; a controller configured to combine at least the first output beam and the second output beam to produce a first overlapped beam as a function of the first phase and the second phase; and wherein the controller is further configured to combine at least the first overlapped beam and the third output beam to produce a second overlapped beam. 2. The communication system of claim 1 , wherein the first phase is different from the second phase. 3. The communication system of claim 1 , wherein at least one of the first lens, the second lens, and the third lens are spherical. 4. The communication system of claim 1 , wherein at least one of the first RF element and the second RF element is configured for dual-polarization. 5. The communication system of claim 1 , wherein the third lens is collinear with first and second lenses. 6. The communication system of claim 1 , wherein the third lens is not collinear with first and second lenses. 7. The communication system of claim 1 , wherein the first output beam is different from the second output beam. 8. The communication system of claim 1 , wherein the first output beam is configured for a first beam width, and the second output beam is configured for a second beam width. 9. The communication system of claim 8 , wherein the first beam width is the same as the second beam width. 10. The communication system of claim 8 , wherein the first beam width is different than the second beam width. 11. The communication system of claim 1 , further comprising: a fourth lens, a fifth lens, a sixth lens, and a seventh lens within the array of lens; the lenses arranged in rows, where each row is parallel to each other. 12. The communication system of claim 11 , wherein the rows are closely packed. 13. The communication system of claim 1 , wherein the controller is further configured to selectively switch between at least the first output beam and the second output beam to effectively locate a target. 14. The communication system of claim 13 , wherein the target is a satellite.
for focusing · CPC title
the units being spaced along or adjacent to a rectilinear path {(waveguide fed H01Q21/0037)} · CPC title
Refracting or diffracting devices, e.g. lens, prism · CPC title
formed of solid dielectric material · CPC title
using refracting or diffracting devices, e.g. lens {(radome H01Q1/42)} · CPC title
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