1. Introduction
Due to the promising applications in 5G and beyond communication systems, there has been a notable surge in research interest in millimeter-wave frequencies, particularly in developing wideband efficient antennas. However, challenges persist in the design of mmWave antennas, primarily stemming from significant signal attenuation, necessitating the utilization of high-gain antennas. Additionally, the potential escalation of ohmic losses in metal antennas and array feed networks poses concerns, leading to compromised radiation efficiency and gain [
1]. Furthermore, microstrip antennas suffer from narrow impedance bandwidths typically ranging from 2% to 5% [
2]. To address these limitations, DRAs have emerged as a viable solution, offering enhanced gain and expanded bandwidth. DRAs possess several advantageous characteristics, including compact size, versatility in shapes, flexible excitation mechanisms, low profile, and lightweight nature [
3,
4].
While single-layer hemispherical DRAs have been extensively studied across various frequency bands, employing techniques such as a probe or conformal strip feeding, challenges arise when operating at mmWave frequencies. Probe feeding, for instance, becomes impractical due to the necessity of drilling holes in physically small ceramic structures, risking damage to the antenna or significant air-gap sizes relative to the shorter wavelengths [
5]. Conversely, slot feeding emerges as a more favorable option at higher frequencies, given its ease of fabrication and the ability to isolate the antenna from the feed network, thereby minimizing spurious radiation. Furthermore, the resonance modes of isolated hemispherical DRAs can be numerically determined by solving the characteristic mode equation, assuming placement on an infinite perfectly conducting ground plane. These resonance modes can be categorized into two primary groups: Transverse Electric (TEₘₙₛ) and Transverse Magnetic (TMₘₙₛ) modes, with TE
111 and TM
101 representing the fundamental modes. The radiation pattern of the TE
111 mode resembles that of a short horizontal magnetic dipole, while the TM
101 mode exhibits characteristics akin to a short electric monopole. Consequently, the diverse array of modes renders the hemispherical DRA (HDRA) appealing for various applications. The subscripts
n,
m, and
s denote variations in fields along the elevation (θ), azimuth (ϕ), and radial (
r) axes of the spherical coordinate system.
It is well known that a substantial increase in the impedance bandwidth can be achieved by appending a dielectric coat to the DRA [
6] since it acts as a transition zone between the antenna and the free space. Recent reports indicate that the DRA coating can increase gain, circular polarization, and impedance bandwidths [
7,
8]. As an example, a wideband slot-fed multi-layer hemispherical DRA has been reported with an impedance bandwidth of 55% by exciting the TE
111 and TE
221 resonance modes in combination with the slot’s resonance mode [
9]. There have also been suggestions that a coaxial probe fed three-layer hemispherical DRA can be adopted in conjunction with materials that have relative permittivities of 9, 4 and 3 for the inner, middle, and outer layers, respectively, wherein a bandwidth of 65.6% has been realized with a lower gain of 3.2 dBi when lower-order modes of TM
101 and TM
102 are excited [
10]. However, as mentioned earlier, probe feeding is impractical at mmWave frequencies. An alternative design of a three-layer hemispherical DRA has been reported using a rectangular waveguide feed whereby the optimization of the outer layer’s permittivity renders the possibility of a broadband coupling to deliver impedance bandwidth and gain of 9.6% and 6.4 dBi, respectively, through the excitation of the TE
113 mode [
11]. Another research study reported a wide impedance bandwidth of ~25% in cases where a conformal strip is employed to excite a three-layer hemispherical DRA operating in the TE
111 fundamental mode [
12]. A hemispherical DRA on a ground plane, fabricated using 3D printing technology with a conductive material, is presented in [
13]. The antenna is optimized for operation in the C-band. Performance analysis reveals a bandwidth of return losses reaching 12.2%, along with an average and peak gain of 4.69 dBi. However, it is noted that utilizing probe feeding may significantly impact the antenna’s bandwidth and efficiency, particularly in mmWave design scenarios. In [
14], another design employing probe feeding is introduced. It explores a multi-layered cylindrical dielectric resonator antenna crafted with 3D-printing technology and tested at X-band frequencies. This design offers an impedance bandwidth of 65.7% (3.56–7.04 GHz) with a gain of 2.3 dB. However, it is difficult to precisely fix a conformal strip on the DRA surface at mmWave frequencies due to the smaller dimensions and potential air gaps between the strip and DRA. Another slot-coupled three-layer hemispherical DRA design offers a broad impedance bandwidth in the region of 29% with a gain of 4.4 dBi proposed by exciting the fundamental TE
111 resonance mode [
15]. When the performance of a two-layer hemispherical DRA is compared to that of a single-layer counterpart, it becomes evident that there is a broader bandwidth of 31.9% and a gain of 2.5 dBi for the layered DRA compared to 14% for the single-layer DRA that operates at the TM
101 lower order mode [
16]. On the other hand, multi-layer DRA configurations are associated with known limitations, such as the increased physical size and the complex assembly procedure with respect to bonding the different dielectric layers together with no potential air gaps in between. This study addresses the above issue by utilizing 3D printing technology to fabricate a DRA and perforated coat configuration using alumina. It should be noted that innovative 3D printing technology is simple, cost-effective, and has a short fabrication cycle. Hence, it has recently been considered in the context of DRA fabrications as it eliminates the potential air gaps more effectively than other fabrication techniques [
17,
18].
In this paper, we introduce a novel approach wherein the traditional layered hemispherical dielectric resonator antenna (DRA) geometry is replaced with an alumina structure comprising two distinct sections: an inner solid DRA and an outer perforated coat featuring a considerably lower effective dielectric constant. This structural modification enables an automated 3D printing process, obviating the requirement for labor-intensive assembly and bonding of numerous solid dielectric layers. Moreover, utilizing the same material for both the DRA and the coat optimizes the 3D printing procedure, thereby enhancing overall efficiency.
It is noteworthy that prior research, as documented in [
19], has introduced a 3D-printed cylindrical DRA with a perforated coat, achieving optimal performance through the utilization of a cross-slot topped by a thin alumina layer to enhance coupling. Conversely, in our proposed hemispherical DRA (HDRA), optimal performance is attained through the implementation of a spiral slot. This discrepancy in performance stems from variations in the electromagnetic field distribution within the two DRAs. Additionally, the perforated coat layers exhibit differing numbers and sizes of air gaps in the respective DRAs. Consequently, maximum coupling to the HDRA is achieved without necessitating the addition of a thin alumina layer between the HDRA and the spiral slot.
Previous research on multi-layer hemispherical DRAs has primarily focused on enhancing impedance bandwidth, overlooking opportunities to widen the CP bandwidth, despite the potential afforded by the outer section to introduce an additional degree of freedom. Another contributing factor to the expanded CP bandwidth is the incorporation of an Archimedean spiral slot to feed the antenna, which excites multiple higher-order modes. Operating within the 18.4–33.4 GHz mmWave frequency band, the antenna demonstrates impressive impedance and axial ratio bandwidths of approximately 58% and 17%, respectively, surpassing those reported in earlier studies for circularly polarized hemispherical DRAs.
The paper is organized as follows:
Section 2 introduces the proposed two configurations of the HDRA;
Section 3 presents the measured results obtained from prototypes of the two HDRA configurations; and
Section 4 offers concluding remarks and summaries. Simulations were conducted using CST Microwave Studio version 2020, and the results closely aligned with experimental measurements.
2. Antenna Configuration
Figure 1 illustrates the two-layer hemispherical DRA and feed network configurations proposed in this study, where the inner and outer layers have respective dielectric constants and radii of
,
a1 and
,
a2. For a single-layer HDRA, i.e.,
= 1, the resonant frequency of the fundamental mode TE
111 can be determined by solving the mode characteristics equation [
20,
21].
in which
,
,
, where
and
represent the spherical Bessel and Hankel functions of the 1st kind and the 2nd kind, respectively. To find the resonant frequency, Equation (1) is solved for a given
a, from which
k0 can be determined. Finally, the resonant frequency can be calculated as [
22]
The feeding spiral is illustrated in
Figure 2 with dimensions defined by the well-known Archimedean spiral function of [
23]
where
р ρ represents the radius of the spiral-slot arm,
α is the spiral constant, and φ is the winding angle. The chosen parameters are
α = 0.08 mm/rad, 0.138π ≤ φ ≤ 2.16π and the width of the spiral-slot arm is
ws = 0.38 mm, which results in a spiral-slot arm length of 3.9 mm that is approximately 0.7λ
eff at an operating frequency of 29 GHz. The variations of the above spiral’s parameters and the separation between the spiral slot arm tuns (
g) can change the spiral’s arm length and provide optimum impedance matching.
2.1. A Single-Layer HDRA
As a reference, a single-layer hemispherical DRA was initially examined, employing dielectric constants of and , with a radius of =3.8 mm.
The proposed antenna was placed on a 45 × 45 mm2 ground plane printed on a thin Rogers RO4350 dielectric substrate, featuring a thickness and dielectric constant of 0.42 mm and 3.48, respectively.
A feeding microstrip line was positioned on the lower side of the dielectric substrate, measuring 22.5 mm in length and 0.88 mm in width, tailored for optimal impedance matching.
Resonance modes of the single-layer DRA were determined by solving Equations (1) and (2) utilizing MATLAB (2021) code. For the specified dielectric constants, radius, feeding slot, and frequency range, the single-layer HDRA supported dual resonance modes, namely TE
112 and TE
511, at 25 GHz and 30.8 GHz, respectively.
Figure 3 illustrates the performance, showcasing the achievement of a dual-band with impedance bandwidths of 19.29% and 9.37%, spanning frequencies from 24.3 to 29.6 GHz and 30.5 to 33.5 GHz, respectively. The simulated axial ratio bandwidth was obtained over a frequency range of 28.3–29.5 GHz, corresponding to 4.2%. These bandwidths were attained with a broadside gain of 5.7 dBic.
2.2. HDRA of Two Solid Dielectric Layers
To enhance the impedance and AR bandwidths, the single-layer hemispherical DRA has been coated by a lower permittivity dielectric layer as illustrated in
Figure 1. The coating layer’s dielectric constant needs to be less than that of the DRA so that the coat acts as a transition layer between the DRA and free space. With optimized coat thickness, the wave reflections at the DRA surface can be minimized, which results in an enhanced bandwidth. However, the choice of the outer layer’s dielectric constant is limited by the availability of commercial materials. Therefore, a polyimide layer has been utilized with a dielectric constant of
= 3.5. On the other hand, the outer layer thickness of δ
a = a2 −
a1 was increased from 0.9 to 2.4 mm. A comparison of the effects of different outer layer thicknesses on the reflection coefficient is presented in
Figure 4. From these results, it can be noted that the widest impedance bandwidth was observed when the outer layer thickness is 1.9 mm and the narrowest bandwidth appeared when it was 1.4 mm.
Figure 5 illustrates that the widest AR bandwidth is also achieved when an outer layer thickness is 1.9 mm. On the other hand, an outer layer thickness of 1.4 mm yielded the narrowest AR bandwidth. Based on
Figure 4,
Figure 5 and
Figure 6, it was found that using a dielectric coat thickness of 1.9 mm results in significant improvements in impedance and axial ratio bandwidths. This is because with such a coat, the DRA excites the following resonance modes: TE
311, TE
112, TE
511, and TE
312 at 19 GHz, 24.6 GHz, 28.6 GHz, and 33.4 GHz, respectively, with an overall bandwidth of 57% spanning from 18.6 to 33.5 GHz. Therefore, a thickness of 1.9 mm, which corresponds to
a2 = 5.7 mm, has been used for the outer layer. Furthermore,
Figure 7 illustrates the variation in S
11 bandwidth as a function of the coating thickness with the maximum bandwidth achieved using the same outer layer thickness of 1.9 mm.
2.3. Layered HDRA Using Alumina with a Perforated Coat
An equivalent configuration to the presented layered HDRA has been created, which consists of a physically single alumina layer with a top perforated section extending to a depth equal to the thickness of the polyimide coat presented in the previous section. This approach makes it easier to fabricate the proposed mmWave hemispherical DRA in accordance with the FDM 3D-printing technology. Therefore, no physical assembly of the two layers is needed, and there are no potential air gaps since alumina was used for the DRA and coat. Moreover, it is possible to realize the different dielectric constants of the dielectric coat by using different hole sizes, as per the filling-ratio theory [
24]. The proposed 3D-printable HDRA is illustrated in
Figure 8, which reveals that the DRA comprises two concentric alumina sections. Specifically, the outer section is characterized by different air-filling ratios designed to deliver diverse effective dielectric constants of the coating layer [
25]. It should be noted that the DRA and coat dimensions, as well as the feed network of the previous section, have been utilized in the proposed configuration.
Figure 9 demonstrates the overall 3D-printing compatible antenna.
A cubic unit cell with a dielectric constant of
εr1, i.e., the same as that of the DRA, was introduced to create the perforated coat. The unit cell is intended to secure an effective dielectric constant of ε
r2eff for the perforated coat that can be calculated using [
17].
The unit cell has a side length of 2.73 mm, or 0.254λ0, where λ0 denotes the free space wavelength at 28 GHz and a wall thickness of tc. The unit cells possess the intrinsic capacity to provide mutual structural support, eliminating the necessity for supplementary support materials during the 3D printing process. As a direct outcome, there is a substantial diminution in both printing duration and material expenditure. The control over the effective permittivity of a perforated dielectric coat can be exercised by modulating the wall thickness as stipulated in Equation (4). The influence of the unit cells’ thickness was explored over a tc range of 0.59 to 0.79 mm, progressing in increments of 0.1 mm, in a hemispherical DRA design adorned with a perforated dielectric coat.
As illustrated in
Figure 10, approximately the same S
11 bandwidths were achieved using wall thicknesses of 0.59 and 0.69 mm, which are wider than that achieved using a thickness of 0.79 mm.
Figure 11 corroborates these findings in the context of AR bandwidth (AR BW), revealing the maximum AR BW is achieved using a
tc = 0.69 mm, whilst the most restricted AR BW was associated with
tc = 0.59 mm. The impact of the wall thickness on the gain is distinctly depicted in
Figure 12 with the highest gain achieved using
tc = 0.69 mm. According to Equation (4), this is expected since a wall thickness of 0.69 mm provides the required effective permittivity of 3.5 for the perforated coat. It should be noted that the 3D printable antenna offers a maximum broadside gain of 9.5 dBic compared to 8.5 dBic achieved with an equivalent HDRA configuration of physically two dielectric layers. This demonstrates that the perforated coat has helped focus the main beam.
Figure 13 compares the return losses of the original structure of two solid layers and that of the 3D-printed HDRA version, underlining the close congruity between the two configurations. For example, the configuration with a perforated coat has achieved an impedance bandwidth of ~58% compared to 57% for the two-layer structure.
4. Conclusions
This study presented a theoretical and practical exploration of a layered hemispherical DRA emitting circular polarization, which is stimulated by a spiral slot feed within the millimeter-wave frequency range. Results demonstrate that incorporating a dielectric coat enhances impedance and axial ratio bandwidths while also boosting gain. This improvement stems from exciting multiple resonance modes beyond the initial dual modes of a single-layer HDRA. Specifically, two-layer HDRA configurations exhibit increased impedance and AR bandwidths of 57% and 18.15%, respectively, coupled with an enhanced gain of 7.5 dBic. Moreover, the successful construction and agreement between simulated and measured results of a two-solid layer HDRA prototype were achieved.
Furthermore, it was demonstrated that an alumina HDRA with a perforated coat can be fabricated via MDF 3D printing, consolidating the two layers into a physical single layer. This streamlines automated assembly and bonding of the layered DRA, eliminating potential air gaps between dielectric layers. This engineered alumina structure, featuring a solid DRA core and a coat characterized by varied air-filling ratios, is designed to achieve the necessary effective dielectric constants. The implementation of an HDRA with a perforated dielectric coat revealed a significant correlation between the two configurations. Additionally, the 3D-printed model exhibited close agreement between simulated and measured results, with impedance bandwidths covering 59.5% and 58%, and CP bandwidths spanning 18% and 17.7%, respectively, within the frequency range of 24.74 to 29.66 GHz and 24.7 to 29.5 GHz. At 28 GHz, simulated and measured gains were 9.53 dBic and 8.6 dBic, respectively.
Considering these attributes, the proposed antenna proves suitable for millimeter-wave satellite communication and radar systems. Furthermore, the superiority of the 3D-printed configuration over its two-solid layers counterpart becomes more pronounced at higher frequencies, such as 60 GHz and sub-terahertz, owing to automated bonding and assembly processes.