RADOME COVER DESIGN FOR BEAMFORMING ANTENNA
20230170608 · 2023-06-01
Inventors
- Cheolbok Kim (Painted Post, NY, US)
- Stanley Abille Mercado (Santa Clara, CA, US)
- Anthony Ng'oma (Horseheads, NY, US)
- Po-Tsung Shih (Painted Post, NY, US)
Cpc classification
H01Q1/02
ELECTRICITY
H01Q1/42
ELECTRICITY
International classification
Abstract
A radome cover design for a beamforming antenna is disclosed. In one aspect, a radome of a polymeric material having two thicknesses with a central thickness optimized for signal transmission at a frequency of interest is provided. Further, the radome is designed to be positioned at a fixed distance from an antenna array so as to provide protection for the antenna array yet still allow for optimal transmission of signals being steered at angles. Such radomes reduce significant signal loss and beam distortion while also being able to be manufactured at commercially reasonable costs.
Claims
1. A radome comprising: a first component comprising a first thickness; and a peripheral component comprising a second thickness, the peripheral component extending outwardly from the first component and configured to cover a housing, wherein the first thickness is different than the second thickness.
2. The radome of claim 1, wherein the first thickness comprises approximately 3.5 millimeters (mm).
3. The radome of claim 1, wherein the first component is generally planar.
4. The radome of claim 3, wherein the peripheral component comprises a second component coplanar with the first component and a third component that extends outwardly and down from the second component.
5. The radome of claim 1, wherein the second thickness comprises approximately 2.2 millimeters (mm).
6. The radome of claim 1, wherein the first component comprises a polymeric material.
7. The radome of claim 1, wherein the first component comprises a dielectric constant of 2.68.
8. The radome of claim 1, wherein the first thickness comprises approximately 2.5 millimeters (mm).
9. The radome of claim 1, wherein the first component comprises a circular planar structure.
10. A radio comprising: a housing delimiting an aperture; a phased array antenna positioned in the aperture; and a radome comprising: a first component configured to cover the aperture and define an air gap between the radome and the phased array antenna, the first component comprising a first thickness; and a peripheral component comprising a second thickness, the peripheral component extending outwardly from the first component and configured to couple to the housing, wherein the first thickness is different than the second thickness.
11. The radio of claim 10, wherein the housing comprises one or more cavities configured to hold electronic circuitry.
12. The radio of claim 10, wherein the first thickness comprises approximately 3.5 millimeters (mm).
13. The radio of claim 10, wherein the first component is generally planar.
14. The radio of claim 13, wherein the peripheral component comprises a second component coplanar with the first component and a third component that extends outwardly and down from the second component.
15. The radio of claim 10, wherein the second thickness comprises approximately 2.2 millimeters (mm).
16. The radio of claim 10, wherein the first component comprises a polymeric material.
17. The radio of claim 10, wherein the first component comprises a dielectric constant of 2.68.
18. The radio of claim 10, wherein the first thickness comprises approximately 2.5 millimeters (mm).
19. The radio of claim 10, wherein the first component comprises a circular planar structure.
20. The radio of claim 10, wherein the air gap is approximately 6 millimeters (mm).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0009]
[0010]
[0011]
DETAILED DESCRIPTION
[0012] Aspects disclosed in the detailed description include a radome cover design for a beamforming antenna. Exemplary aspects of the present disclosure provide a radome of a polymeric material having two thicknesses with a central thickness optimized for signal transmission at a frequency of interest. Further, the radome is designed to be positioned at a fixed distance from an antenna array so as to provide protection for the antenna array yet still allow for optimal transmission of signals being steered at angles. Such radomes reduce significant signal loss and beam distortion while also being able to be manufactured at commercially reasonable costs.
[0013] In this regard,
[0014]
[0015] In an exemplary aspect, the radome 112 has a first component 208 that is generally planar in an x-y plane and has a first thickness 210 that covers the aperture 108. Further, the radome 112 has a second component 212 that is generally coplanar with the first component 208 and a third component 214 that is angled down and away (along a z-axis) from the second component 212. Collectively the second component 212 and the third component 214 form a peripheral component 216. The peripheral component 216 has a second thickness 218, different from the first thickness 210, and in a specifically contemplated aspect, the second thickness 218 is less than the first thickness 210. A shoulder 220 may be formed where the first component 208 and the second component 212 join. The dimension of the shoulder 220 may correspond to the difference between the first thickness 210 and the second thickness 218. Likewise, the shoulder 220 may be configured to abut the housing 102.
[0016] In an exemplary aspect, the radome 112 is made from a polymeric material and may be injection molded either as a single piece in a single injection, a single piece in two injections, or two pieces secured to one another. For the two-injection process, a first injection creates a piece having the second thickness 218 throughout, and a second injection adds thickness to the first component 208 to achieve the first thickness 210. In an exemplary aspect, the polymeric material may be a polycarbonate/Acrylonitrile Butadiene Styrene (PC/ABS) material such as CYCOLOY™ Resin C2950, sold by SABIC having a sales office at 44 Normar Road, Cobourg, Ontario Canada K9A 4L7. As best understood, the dielectric constant of this material is 2.68.
[0017] As noted, the radome 112 and particularly the first component 208 may be sized in the x-y plane to correspond to the aperture 108 (e.g., a circle with a diameter of approximately 120 millimeters (mm)) with the peripheral component 216 sized to cover the housing 102. In an exemplary aspect, if the radome 112 is going to be used with a phased array antenna 110 that operates at 28 gigahertz (GHz), the first thickness 210 may be approximately 3.5 mm and the second thickness 218 may be approximately 2.2 mm. Approximately as used herein is within one percent (1%). In contrast, if the radome 112 is going to be used with a phased array antenna 110 that operates at 39 GHz, the air gap 206 may be approximately 4.3 mm, the first thickness 210 may be approximately 2.5 mm, and the second thickness 218 may be approximately 2.2 mm.
[0018] The dimension of the second thickness 218 is chosen so as to have sufficient structural integrity to protect the housing 102 and the phased array antenna 110 while also being thinner than the first component 208 so as to reduce material costs and allow for easy manufacturing.
[0019] At first inspection, the numbers for the dimensions set forth above may seem counter-intuitive because, based on Fabry-Perot interferometer theory, the minimum signal reflection at the surface of a dielectric cover (e.g., the back face 204) is achieved when the dielectric cover thickness equals an integer number (N) times half the equivalent wavelength of the signal (i.e., t=Nλ/(2√{square root over (εr)}), where t is the dielectric thickness, λ, is the wavelength of the signal, and εr is the dielectric constant of the material). Accordingly, at 28 GHz, the wavelength in air is 10.7 mm and the wavelength in the radome 112 is 6.5 mm. Thus, one would expect an optimized air gap and first thickness 210 to be about 5.3 mm and 3.3 mm, respectively. However, the presence of metallic and non-metallic structures, as well as the fact that the beams are radiated along a variety of axes as a function of the beam steering changes the performance from the ideal Fabry-Perot calculations.
[0020] Through the use of simulation software, particularly ANSYS HFSS, a variety of simulations confirm the values presented above provide the best compromise. The results of the simulations are provided in
[0021] In this regard,
[0022]
[0023]
[0024]
[0025]
[0026] Unless otherwise expressly stated, it is in no way intended that any method set forth herein be construed as requiring that its steps be performed in a specific order. Accordingly, where a method claim does not actually recite an order to be followed by its steps, or it is not otherwise specifically stated in the claims or descriptions that the steps are to be limited to a specific order, it is in no way intended that any particular order be inferred.
[0027] It will be apparent to those skilled in the art that various modifications and variations can be made without departing from the spirit or scope of the invention. Since modification combinations, sub-combinations, and variations of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and their equivalents.