1. Introduction
The growing applications of the Internet of Things (IoT) and 5G/6G have raised the demand for flexible, wearable, low-cost, and mass-manufacturing microwave and millimeter-wave components. These applications involve billions of connected devices performing several operations such as sensing, data acquisition, processing, and transportation [
1,
2,
3,
4]. Modern printed electronic circuits need to be low-cost and mechanically flexible for wearable applications to fulfill the requirements of mass production and ease assembly conditions on different surfaces. Unfortunately, traditional electronic manufacturing techniques such as subtractive fabrication technologies are not technically and economically competitive in mass production [
5,
6]. They are expensive, resulting in material waste, and are not ideal for mass manufacturing [
7]. Recently, various printing techniques have been adapted for electronics manufacturing. For instance, gravure printing, flexography, inkjet printing, and more specifically screen printing [
8,
9,
10,
11]. The latter seems to be a promising and cost-effective technique for printable microwave/millimeter-wave/THz circuits such as RFID tags, RFIC packaging, energy-harvesting rectennas, and wireless communication antennas [
11,
12,
13]. Today, screen printing offers repeatable accurate printing of antenna circuits on inexpensive flexible thin-film materials such as glass, laminates, and plastic, providing a large substrate selection for flexible electronics [
10]. Nevertheless, specific arrangement and parameters such as ink, printing, and screen conditions must be carefully monitored at higher frequencies on highly flexible transparent substrates. Moreover, depending on ink composition and ink/substrate interaction, post-processing through heat treatment at 135° might be required [
11].
Given what has been achieved in the screen-printing research area, high-frequency circuits involving the screen-printing process on transparent thin-film substrates are still missing from the literature. Moreover, the implementation challenges associated with those types of substrate materials have not been previously revealed. For these reasons, we believe that clarifying screen-printing issues on highly transparent substrates at higher frequencies will provide practical performance optimization guidelines to microwave/millimeter-wave circuits and antenna designers. As a proof of concept, a full-screen printed 1 x 4 Quasi-Yagi-Uda antenna array on a high-transparency flexible Zeonor thin-film substrate is presented and analyzed for emerging 26 GHz band 5G applications. Thanks to the suggested screen-printing improvement, the implementation of the 1 x 4 Quasi-Yagi-Uda antenna array prototype has been highly optimized. Moreover, a repeatability test has been performed by manufacturing 24 antenna array samples equally distributed over 4 substrate sheets for performance comparison. The achieved comparison performances show a good concordance over the considered frequency range from 20 GHz to 30 GHz. They exhibit a large bandwidth and high gain as expected from the traditional subtractive printed circuit board (PCB) manufacturing process using standard substrates.
2. Screen-printing technique
Figure 1 shows a screen-printing process description. Ink is spread on a stencil by a squeegee. Thus, when the stencil is transparent, the ink is deposited on the substrate. The process requires a precise management of stencil mesh and squeegee properties, as well as production techniques. It may also require tightly controlled parameters during printing. Furthermore, ink transfer is mainly influenced by the screen mesh, squeegee speed, and pressure on the screen. The thickness and accuracy of the printed layer are affected by the ink’s rheological properties. It should be noted that thicker ink deposition involves lower resolution [
14].
The parameter selection involves some rules consideration for antenna design, including minimum line width, spacing between adjacent lines, and feeding techniques. The screen printing prototyping uses a commercial screen printing machine. However, to improve cost-effectiveness, only textile stencils were utilized to print all the designed antennas. The substrate is the first element to be selected appropriately, especially at the millimeter-wave frequency range, where it plays a key role in antenna performance. In the millimeter wave frequency range, the substrate plays a key role in antenna performance. It must have low-loss characteristics and be compatible with the physicochemical properties of the selected ink. For our screen printing process, a Zeonor [
15] substrate with a thickness of
(
) has been chosen. In order to ensure a proper printing and good adherence of ink with the substrate it must have an oxygen free plasma treatment. Substrate selection is a key factor in ensuring good compatibility with inks, particularly with reagrd to the substrate’s physical and chemical properties. In this section, we expose the essential properties that promote this compatibility. For instance, in the case of inkjet or screen printing with metallic inks, such as silver ink, the substrate must have a microporous receiving layer, either by plasma etching to create nanometric roughness, or by depositing a porous low dielectric such as a fluoropolymer or polystyrene, which enables better adhesion and avoids excessive ink diffusion. The characteristics of silver inkjet printing were intensively investigated with control of surface energy, which is why the choice of substrate can greatly affect the quality of the print and consequently the electrical performance of the deposited silver layer. In this study, the Kapton was treated with an oxygen-free plansma to create the micro-pored layer without degradation of the electrical properties of the zeonor [
16].
To minimize losses in metallic parts of the antenna, ink selection is a key point in our study. The selected ink must be sufficient for screen-printing and have high conductivity with relatively low cost. Thus a trade off between cost and conductivity should be found. As initial value, the thickness of ink is fixed to two penetration depth (
). Taking into account those constraints, the ECI011 nano-particles silver ink from Henkel has been selected with a conductivity of
. According to equation
1, the penetration depth can be computed at
and the needed ink thickness deduced.
Table 1 summarize the properties of this ink.
With such ink thickness, the expected resolution should be around
for ink strips and
for slots formed on ink strips. This resolution should be suitable for printing antennas in the 5G ETSI millimeter-waves frequency range. As the substrate and the ink properties are set, a feeding method is essential. Various feeding solutions on flexible substrates can be employed for this purpose. For a comprehensive characterization of the manufactured antenna prototypes, a 50
microstrip line along with a
Southwest Microwave End launch connector are implemented. The designed micro-strip lines consist of a signal strip printed on the top face of the substrate, and a ground plane printed on the bottom face. To assess the thickness of selected ink layer , the lineic attenuation of a 50
micro-strip line is extracted from full-wave simulations. The results plotted in
Figure 2 shows that increases the thickness of printed layers up to
allows to reduce metallic losses. Indeed, increasing the thickness does not significantly reduce metallic losses and does not improve the resolution of the printed patterns. [
14].
3. Quasi-Yagi-Uda antenna elements
3.1. Design optimization
The single-element Quasi-Yagi-Uda antenna configuration is shown in
Figure 3.
Its geometrical Parameters have been optimized according to the design rules described in [
17,
18,
19,
20]. The initial Quasi-Yagi-Uda antenna configuration is designed using a full ground plane as shown in
Figure 3 (a). Typically, a Quasi-Yagi-Uda antennas antenna consists of two driven elements fed by a
microstrip line and several directors (parasitic elements), as shown in
Figure 3. For design optimization, 3D HFSS electromagnetic (EM) simulation software has been used while considering the southwest end-launch connector effect. It was demonstrated from simulation results that the distance between the ground plane and driven element (d’) impact significantly matching bandwidth, however, the distance between different directors (d) mainly impacts the gain. The length
sets the antenna operating frequency, whereas
and
set the antenna’s lower and higher cut-off frequencies. Several director configurations have been tested. A trade-off between directivity, directors’ losses and the overall antenna size has enabled us to limit the directors number to 4 directors placed on the top layer. It was reported that a double row of four directors placed respectively on the top and bottom layers may increase the antenna gain [
20].
In the context of our study, the expected gain has not been achieved due to high metallic losses and the thickness of the selected substrate. The computed values from [14] have been modified by a scale factor while considering the dielectric constant parameter. Then, the antenna dimensions were optimized to achieve good impedance matching and the flattest realized gain over the 24.5 GHz to 27.5 GHz frequency band. For instance, simulation results show that an optimized 4 directors configuration exhibits a realized gain of 9.8 dB (11.1 dB in an 8 directors configuration). This represents an increase in antenna size from to (about a 75% size increase) and a radiation efficiency variation from 65% (8 directors) to 69.5% (4 directors).
Now, we optimize the ground plane to reduce the ink consumption while increasing the flatness band of the gain and improving the side lobe rejection. The proposed ground plane configuration is shown in
Figure 3 (b).
and
, have been optimized through a rigorous parametric study. Several effects can be observed on the variation of the gain versus frequency as shown in
Figure 4a and
Figure 5a. However, simulation results demonstrate that If the
is too short, the resulting ground does not affect antenna performance. An optimum value of
has been set to
in the proposed antenna configuration, nevertheless, higher
length causes a reduction in antenna bandwidth (see
Figure 4b). Regarding the impact of
variations, the parametric study results are plotted in
Figure 5a. It shows that the optimum value is approximately equal to the length of a reflector given in [
18]. For lower values of
, the edge of the ground plane does not act as a reflector and higher values than optimal decrease the bandwidth and the maximal gain. Careful attention to input impedance matching (
Figure 4b and
Figure 5) shows that those parameters can optimize the antenna’s bandwidth. Setting the proper values of
and
enables the flattest peak gain in the desired bandwidth.
A further effect concerning the out-of-band gain reduction is also observed. As can be seen, the gain at 20 GHz has been reduced by more than 8 dB (from 1.2 dB to -7.5 dB). Under the same design modifications, the in-band gain variation is reduced to less than 0.5 dB (from 1.3 dB to 0.3 dB).
Table 2 summarizes the optimized geometrical parameters of the antenna including, the 4 directors configuration and modified ground plane.
Figure 5 shows the simulation results of the optimized Quasi-Yagi-Uda antenna. Those results show a maximum gain of 9.8 dB at 27 GHz with a variation of only 0.3 dB within the considered frequency band. In conclusion, the proposed technique allows ground plane reduction from
to
, representing a decrease of 61%.
As regards the radiation pattern performance shown in
Figure 7, the newly optimized antenna parameters have only an influence on the H-plane radiation pattern with no major changes on the E-plane. In the proposed antenna configuration side lobes at
can be reduced from -6 dB to -12.5 dB.
3.2. Measurements
This section deals with the experimental characterization of the single Qausi-Yagi-Uda antenna. For that purposes, 24 antenna prototypes, printed on 4 different sheets, have been printed by CEA-Liten "Ares" facilities. Measurements for performances investigation have been performed in the im2np lab. The size of the printed antenna and the end-launch connector compared to a 50-cent coin is given in
Figure 8.
Measurements have been performed using a DRH 67 GHz RF-SPIN antenna and a MS4647B 4 ports 70 kHz-70 GHz Anritzu VNA. The free space test bench used allows to perform radiation pattern measurements in E and H planes, realized gain in a given direction and matching as function of the frequency up to .
The measurement results are plotted in
Figure 9 and in
Figure 10. For each sheet of printed antennas, the mean (see
Figure 9a) and standard deviation have been computed from individual measurement of the realized gain. Standard deviation for each sheet plotted in
Figure 9b gives further information on the repeatability of the screen printing process. The standard deviation is lower than
over the
to
frequency band. It involves a very low dispersion for 24 measured antennas. The maximum measured gain is
in the line of sight direction. A small shift of approximately
, (less than
) can be observed on measurements. Geometrical measurements of the printed antennas and retro-simulations does not allow to affirm that geometrical issues introduced during the printing cause this mismatch. Retro-simulation of the antenna with
instead of
allows to explain this slight frequency shift between simulations and measurements (see
Figure 9a). By adopting the same approach
measurements results are plotted in
Figure 10. The same discrepancy between simulations and measurements can be observed and same reasons can be invoked to explain the observed frequency shift. Higher dispersion on this parameter can also be observed. Still, in this case, a little frequency shit between measurements of different antennas causes higher variations of the
than for gain versus frequency values. The measured
matching bandwidth ranges from
.
Radiation pattern in E and H planes have been measured at
,
,
,. and
. The results of the simulated and measured normalized gain are plotted in
Figure 11. As can be seen, a good agreement between measurements and simulations is achieved. For H-plane at all measured frequencies, side lobes are below
and front to back ratio is lower than
. For E-plane the side lobe level are bellow
except at
. Measurement shows a maximum
beamwidth of
in H-plane and
in E-plane.
Comparison with other published Quasi-Yagi-Uda antennas realized with standard technologies shows that similar performances can be achieved by a careful optimization of screen-printing process and the design (see
Table 3).
4. Quasi-Yagi-Uda antenna array
4.1. Design methode
A corporate feed network using three rounded shapes Wilkinson dividers is adopted for the 1 x 4 Quasi-Yagi-Uda antenna array design. The selected feed network configuration allows more control of feeding each antenna element (amplitude and phase); hence, they are ideal for several antenna array applications such as multi-beam arrays, scanning phased arrays, or shaped-beam arrays [
18]. Typically, two power divider types may be used for the power distribution in the antenna arrays, reactive T-junctions and Wilkinson power dividers. The T-junctions are lossless and simpler to design but do not provide isolation between the output ports. The Wilkinson dividers involve higher design and fabrication complexities, and they are not entirely lossless since reflected power is dissipated in the resistor. However, they provide isolation between output ports, which prevents mismatches and reflected signals from propagating to other parts of the array. To reduce the undesirable coupling and improve isolation between the Wilkinson output ports at higher frequencies, two
microstrip lines have been added between the two output ports [
25]. It should be noted that the
isolation resistor between the output ports (ports 2 and 3) has been implemented using a
per square thin layer carbon past.
The designed Wilkinson power divider and its simulated S-parameters are shown in
Figure 12a and
Figure 12b, respectively. The simulation results show a maximum insertion loss of
and isolation between the output ports (ports 2 and 3) better than
in the frequency range from
to
.
EM simulations have also been performed of the array without the feeding network to evaluate mutual coupling between antenna elements which impact the total array performance. The optimum distance necessary to avoid grating lobes is set to
in the proposed array design. The arrangement adopted could add
to the achieved gain to reach
in the main direction of radiation. The obtained Results show that the added gain is much lower and that the matching is modified (see
Figure 13). The study of the current distribution and transfer parameters between adjacent antennas (
) (see
Figure 13) shows that the proximity of antennas most likely causes this reduction. This generates coupling between the radiating elements and reduces the antenna array gain.
The undesired grating lobes are usually controlled by constraining the distance between antenna elements.
Given our printing resolution limitation, we further spaced the antenna elements to improve the gain, even if doing so results in a possible side lobes generation [
18]. Under those considerations, a maximum of
side lobe rejection level and a gain as close as possible to the theoretical limit of
may be exhibited. Then, spacing between array elements of
is required to satisfy our criteria (see
Figure 13).
The overall dimension of the designed 1 x 4 Quasi-Yagi-Uda antenna array is around
by
, as shown in
Figure 14a.
Figure 14b shows input impedance matching and gain simulation results including End Launch
connector effect, over the frequency range of
to
. As can be seen, a maximum gain of
in the main radiation direction is achieved. The antenna array maintains a good input impedance matching over the
to
frequency range. As expected, the minimum side lobe rejection level is
The simulated radiation efficiency spans from 50 to 55 % in the frequency range of interest.
4.2. Measurements
For comprehensive characterization, 24 antenna arrays have been prototyped over 4 sheets by the CEA-LITEN laboratory.
Figure 15 shows the real size of an antenna array with its connector beside a 50-cent coin. 24 antenna arrays have been printed by the CEA and equally distributed over 4 sheets.
The gain in the main direction of radiation and the matching of each array has been measured with the same test bench as for single Quasi-Yagi-Uda antenna elements. The results plotted in
Figure 16a and
Figure 16b show the mean of measured gain and it’s standard deviation for each of the 4 sheets. The measurements results compared with simulations show a good agreement for the four printed sheets.The maximum deviation between measured and simulated gain does not exceed
between 24 and
. In addition, the standard deviation of each leaf is less than
(see
Figure 16b).
By adopting the same approach
measurements results are plotted in
Figure 17. The results plotted in
Figure 17a and
Figure 17b show the mean of measured
and its standard deviation for each of the 4 sheets. As for the Quasi-Yagi-Uda antenna element higher dispersion on this parameter can be observed. Still, in this case, a little frequency shit between measurements of different antennas causes higher variations of the
than for gain versus frequency values. The measured matched bandwidth is very close to the simulated one and it ranges from
. This results shows high reproductibility of the screen-printing process. Sheets 1-2 and 4 show almost the same results, however, only sheet 3 shows a slightly higher average gain than others.
The radiation pattern measurements in both E and H planes have also been performed. The results plotted in
Figure 18 show very good agreements with simulations results. The obtained results exhibit an antenna beam-width of 28 ° and side lobes rejection in the E-plane of respectively,
at
, and
at
. The maximum front-to-back ratio is
. A deviation of
. between simulated and measured results may be explained by the employed measurement setup and alignment errors. In addition, for alignment accuracy investigation, geometrical measurements have also been performed. The most important disagreement between simulated model and printed prototypes show a misalignment between top and bottom layers up to
. Comparison of measured performances and simulation results allows to conclude that such mismatch does not impact the proposed antenna and antenna array behavior.
5. Conclusion
In this paper, we successfully demonstrated a screen-printed 1 x 4 Quasi-Yagi-Uda antenna array on a high-transparency flexible and transparent, Zeonor thin-film substrate for innovative band 5G applications. The flexible, low-profile and cost-effective antenna array was designed, prototyped, and tested for this study. The screen-printing process has been properly optimized to overcome the associated fabrication challenges such as the appropriate ink thickness selection and poor ink adhesion with the high-transparency substrate. A screen-printing repeatability study has also been performed through measurement and performance comparison of 24 antenna array samples to verify the reliability of the screen-printing process at higher frequency bands. The obtained performance results are encouraging, despite slight deviation from the simulation results, proving the ability of the screen-printing process to produce low-profile low-cost antenna arrays on transparent thin-film substrates for 5G/6G applications.
Author Contributions
M.E. designed all the single element antenna and the array. A.V. designed the wilkinson divided.
Funding
This research received no external funding
Acknowledgments
This work is supported by the CEA Liten of Grenoble, France. The authors would likes to thanks David Alincant, for printing the prototypes presented in this article.
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Figure 1.
Schematic of the screen printing process
Figure 1.
Schematic of the screen printing process
Figure 2.
Simulated lineic attenuation of a printed micro-strip line
Figure 2.
Simulated lineic attenuation of a printed micro-strip line
Figure 3.
The designed Quasi-Yagi-Uda antenna (a) complete ground plane, (b) patterned ground plane
Figure 3.
The designed Quasi-Yagi-Uda antenna (a) complete ground plane, (b) patterned ground plane
Figure 4.
Effects of on (a) realized gain, (b) matching of the proposed Quasi-Yagi-Uda screen printed antenna
Figure 4.
Effects of on (a) realized gain, (b) matching of the proposed Quasi-Yagi-Uda screen printed antenna
Figure 5.
Effects of on (a) realized gain, (b) matching of the proposed Quasi-Yagi-Uda screen printed antenna
Figure 5.
Effects of on (a) realized gain, (b) matching of the proposed Quasi-Yagi-Uda screen printed antenna
Figure 6.
Quasi-Yagi-Uda antenna simulated performances
Figure 6.
Quasi-Yagi-Uda antenna simulated performances
Figure 7.
Effects of the modified ground plane on the (a) E-plane and (b) H-plane cut of the radiation pattern of the Quasi-Yagi-Uda antenna at 26 GHz
Figure 7.
Effects of the modified ground plane on the (a) E-plane and (b) H-plane cut of the radiation pattern of the Quasi-Yagi-Uda antenna at 26 GHz
Figure 8.
Photograph of a screen-printed Quasi-Yagi-Uda antenna
Figure 8.
Photograph of a screen-printed Quasi-Yagi-Uda antenna
Figure 9.
(a) Measured gain for 24 screen-printed quasi-Yagi-Uda, (b) standard deviation on gain measurement for each sheet as function of the frequency
Figure 9.
(a) Measured gain for 24 screen-printed quasi-Yagi-Uda, (b) standard deviation on gain measurement for each sheet as function of the frequency
Figure 10.
(a) Measured for 24 screen-printed quasi-Yagi-Uda, (b) standard deviation on measurement for each sheet as function of the frequency
Figure 10.
(a) Measured for 24 screen-printed quasi-Yagi-Uda, (b) standard deviation on measurement for each sheet as function of the frequency
Figure 11.
Radiation pattern of Quasi-Yagi-Uda antenna at (a) 24.5 GHz, (b) 25 GHz, (c) 26 GHz and (d) 27 GHz.
Figure 11.
Radiation pattern of Quasi-Yagi-Uda antenna at (a) 24.5 GHz, (b) 25 GHz, (c) 26 GHz and (d) 27 GHz.
Figure 12.
(a) Top view of the modified wilkinson power divider (b) simulated S-parameters of a single wilkinson modified power divider as function of the frequency
Figure 12.
(a) Top view of the modified wilkinson power divider (b) simulated S-parameters of a single wilkinson modified power divider as function of the frequency
Figure 13.
Effect of array pitch on antenna array performances
Figure 13.
Effect of array pitch on antenna array performances
Figure 14.
(a) Top view of the 4x1 Quasi-Yagi screen-printed antenna array, (b) Simulation results of and gain for the 4x1 Quasi-Yagi Uda antenna array as function of the frequency
Figure 14.
(a) Top view of the 4x1 Quasi-Yagi screen-printed antenna array, (b) Simulation results of and gain for the 4x1 Quasi-Yagi Uda antenna array as function of the frequency
Figure 15.
Photograph of a screen printed Quasi-Yagi-Uda antenna array
Figure 15.
Photograph of a screen printed Quasi-Yagi-Uda antenna array
Figure 16.
(a) average per sheet of measured gain, (b) standard-deviation per sheet of measured gain
Figure 16.
(a) average per sheet of measured gain, (b) standard-deviation per sheet of measured gain
Figure 17.
(a) average per sheet of , (b) standard-deviation per sheet of
Figure 17.
(a) average per sheet of , (b) standard-deviation per sheet of
Figure 18.
Normalized radiation pattern at (a) 24.5 GHz, (b) 25 GHz, (c) 26 GHz and (d) 27 GHz
Figure 18.
Normalized radiation pattern at (a) 24.5 GHz, (b) 25 GHz, (c) 26 GHz and (d) 27 GHz
Table 1.
Properties of the silver ink
Table 1.
Properties of the silver ink
| Ink name |
conductivity |
|
thickness |
| ECI1011 |
|
|
|
Table 2.
Geometrical parameters the elementary Yagi antenna.
Table 2.
Geometrical parameters the elementary Yagi antenna.
| Parameter |
value |
Parameter |
value |
|
|
|
|
| d |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Table 3.
Comparison with other published 5G 26 GHz Quasi-Yagi-Uda antennas.
Table 3.
Comparison with other published 5G 26 GHz Quasi-Yagi-Uda antennas.
| Ref |
|
bandwidth |
Gain |
substrate |
metallization |
radiators |
| This work |
|
|
|
zeonor |
silver ink |
4 |
| [21] |
|
|
|
screen-printable ink |
AgNW ink |
1 |
| [22] |
|
|
|
Megtron6* |
copper |
4 |
| [23] |
|
|
|
Neltec NX9240* |
copper |
5 |
| [17] |
|
|
|
RO4350B* |
- |
3 |
| [20] |
|
|
|
MFLEX* |
- |
3x2 |
| [24] |
|
|
|
liquid crystal |
copper |
3 |
|
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