This application is based upon and claims the benefit of priority from Japanese Patent Application No. 2023-008851, filed on Jan. 24, 2023; the entire contents of which are incorporated herein by reference.
Embodiments described herein relate generally to an antenna device and a wireless device.
For example, it is desirable to improve the characteristics of an antenna device and a wireless device.
According to one embodiment, an antenna device includes a waveguide. The waveguide includes a feed point, and a first region around the feed point. The waveguide is configured to guide a high-frequency signal supplied to the feed point. The waveguide includes a plurality of radiating parts located in the first region. The first region includes a first partial region and a second partial region. The feed point is between the first partial region and the second partial region. A first waveguide wavelength in the waveguide in the first partial region is less than a second waveguide wavelength in the waveguide in the second partial region.
Various embodiments are described below with reference to the accompanying drawings.
The drawings are schematic and conceptual; and the relationships between the thickness and width of portions, the proportions of sizes among portions, etc., are not necessarily the same as the actual values. The dimensions and proportions may be illustrated differently among drawings, even for identical portions.
In the specification and drawings, components similar to those described previously or illustrated in an antecedent drawing are marked with like reference numerals, and a detailed description is omitted as appropriate.
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A direction perpendicular to the first region 10r is taken as a Z-axis direction. One direction perpendicular to the Z-axis direction is taken as an X-axis direction. A direction perpendicular to the Z-axis direction and the X-axis direction is taken as a Y-axis direction. The first region 10r spreads along the X-Y plane.
The waveguide 10 is configured to guide a high-frequency signal supplied to the feed point 10c. The waveguide 10 is, for example, a transmission line configured to propagate the high-frequency signal. The waveguide 10 may be, for example, a radial waveguide. The waveguide 10 may be, for example, a dielectric waveguide. The waveguide 10 may be, for example, a waveguide tube. The high-frequency signal that is supplied to the feed point 10c propagates through the waveguide 10. The propagation direction is a radial direction passing through the feed point 10c.
As shown in
The waveguide 10 may include multiple radiating parts 20. The multiple radiating parts 20 are located in the first region 10r.
In one example, one of the multiple radiating parts 20 (e.g., each of the multiple radiating parts 20) may include a slot pair. The slot pair includes, for example, a first slot 21 and a second slot 22. These slots correspond to apertures 45 provided in the first conductive layer 41 (see
As shown in
Thus, according to the embodiment, the waveguide wavelengths (e.g., the guide wavelengths) are different in the plane of the first region 10r. Accordingly, the radiation direction of the electromagnetic wave radiated from the multiple radiating parts 20 can be tilted with respect to the Z-axis direction.
For example, in a first reference example in which the radiation direction of the electromagnetic wave is tilted with respect to the Z-axis direction, the spacing (the density) of the multiple radiating parts 20 is changed in the plane. In the first reference example, the spacing in the radial direction between the multiple radiating elements corresponding to the tilt direction is increased. On the other hand, the spacing in the radial direction between the multiple radiating elements in the direction opposite to the tilt direction are reduced. Increasing the spacing in the tilt direction causes unnecessary grating lobes. Furthermore, the range of sizes of the multiple radiating elements becomes narrow when the spacing in the direction opposite to the tilt direction is reduced. For example, design freedom is reduced.
In the first reference example, a method of increasing the dielectric constant of the dielectric waveguide may be considered to prevent grating lobes. The element spacing in the tilt direction may be reduced thereby. However, as the dielectric constant increases, the loss due to the dielectric increases, and the efficiency decreases. Also, as the dielectric constant increases, the element spacing in the direction opposite to the tilt direction is further reduced, and the design freedom is further reduced.
In contrast, according to the embodiment, the first waveguide wavelength λ1 is less than the second waveguide wavelength λ2. Thus, the waveguide wavelengths (e.g., the guide wavelengths) are different in the plane of the first region 10r. Accordingly, the radiation direction of the electromagnetic wave radiated from the multiple radiating parts 20 can be tilted with respect to the Z-axis direction without changing the spacing of the multiple radiating parts 20. For example, the grating lobes are suppressed thereby. For example, a high efficiency can be maintained. For example, high design freedom can be maintained. The performance of the antenna can be improved by high design freedom. According to the embodiment, an antenna device can be provided in which the characteristics can be improved.
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For example, a third waveguide wavelength 23 in the waveguide in the third partial region 13 is greater than the first waveguide wavelength λ1 and less than the second waveguide wavelength 22. A fourth waveguide wavelength 24 in the waveguide in the fourth partial region 14 is greater than the first waveguide wavelength λ1 and less than the second waveguide wavelength 22.
For example, high design freedom can be maintained in the third and fourth partial regions 13 and 14. The performance of the antenna can be improved.
As shown in
For example, the first waveguide wavelength λ1 corresponds to the guide wavelength in the direction of the angle do in the circumferential direction in the waveguide 10 when viewed from the feed point 10c. The second waveguide wavelength 12 corresponds to the guide wavelength in the direction of the angle (ϕ0+180°) in the waveguide 10 when viewed from the feed point 10c.
For example, the third waveguide wavelength 13 corresponds to the guide wavelength in the direction of the angle (ϕ0+90°) in the circumferential direction in the waveguide 10 when viewed from the feed point 10c. The fourth waveguide wavelength λ4 corresponds to the guide wavelength in the direction of the angle (ϕ0−90°) in the circumferential direction in the waveguide 10 when viewed from the feed point 10c.
For example, the first waveguide wavelength λ1 is the wavelength (the guide wavelength) of the high-frequency signal propagating along the direction from the feed point 10c toward the first partial region 11. The second waveguide wavelength λ2 is the wavelength (the guide wavelength) of the high-frequency signal propagating along the direction from the feed point 10c toward the second partial region 12.
As shown in
For example, in the antenna device 110, the first electromagnetic wave 81 is radiated with beam tilt. For example, an extremely narrow spacing of the multiple radiating parts 20 in the direction (the second partial region 12) opposite to the tilt direction can be suppressed. Design freedom of the size, position, etc., of the multiple radiating parts 20 is increased. The performance of the antenna can be improved.
Examples of the waveguide 10 will now be described.
For example, the high-frequency signal may be input to the feed point 10c of the waveguide 10 via a coaxial line. For example, the high-frequency signal may be input to the feed point 10c via a waveguide tube.
These drawings show several examples of the feed point 10c. In these drawings, the high-frequency signal is input to the waveguide 10 (e.g., a radial waveguide) via a coaxial line 25.
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In the example of
In the example of
The multiple radiating parts 20 radiate the high-frequency signal propagating through the waveguide 10 to the space outside the waveguide 10. The multiple radiating parts 20 are radiating elements (antennas). The multiple radiating parts 20 are provided in the first region 10r around the feed point 10c. The multiple radiating parts 20 function as an array antenna.
One of the multiple radiating parts 20 may be a slot pair. One of the multiple radiating parts 20 may be a single slot antenna. One of the multiple radiating parts 20 may be a helical antenna. One of the multiple radiating parts 20 may be a patch antenna. One of the multiple radiating parts 20 may be a dipole antenna. One of the multiple radiating parts 20 may be a dielectric resonator antenna. One of the multiple radiating parts 20 may be a leaky-wave antenna. Various configurations are applicable to the multiple radiating parts 20.
The multiple radiating parts 20 may be arranged in a substantially spiral configuration in the first region 10r. The center of the spiral is the feed point 10c. The multiple radiating parts 20 may be arranged in a substantially concentric circular configuration in the first region 10r. The center of the concentric circles is the feed point 10c.
As described above, the waveguide 10 may include the first member 30. For example, the first member 30 corresponds to a slow-wave structure. The waveguide wavelength (e.g., the guide wavelength) can be changed in the plane of the first region 10r by the first member 30. The first member 30 has the function of adjusting the guide wavelength of the high-frequency signal propagating through the waveguide 10.
For example, a first slow-wave ratio of the first member 30 in the first partial region 11 is different from the second slow-wave ratio of the first member 30 in the second partial region 12. In one example, the first member 30 includes a dielectric. In one example, the slow-wave ratio can be controlled by changing the dielectric constant (e.g., the effective dielectric constant) of the first member 30.
For example, it is easier to control the guide wavelength by changing the slow-wave ratio of the first member 30. For example, the control range of the guide wavelength is increased. For example, the change of the guide wavelength due to a frequency change can be reduced. For example, a narrow operating band of the antenna can be suppressed.
As shown in
When the waveguide 10 is a waveguide tube, the guide wavelength also changes according to the tube width of the waveguide tube. The guide wavelength may be adjusted by changing the tube width in addition to the relative dielectric constant. The first member 30 is considered to be a slow-wave structure even when the relative dielectric constant of the dielectric 38 is substantially 1.
In
In
In
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The effective relative dielectric constant may be changed by changing the density of the dielectric 38. For example, one type of dielectric 38 can be included to control the distribution of the relative dielectric constant by changing the density of the dielectric 38.
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For example, the first member 30 includes a first member region 31 and a second member region 32 (see
For example, the first member region 31 and the second member region 32 may satisfy at least one of a first condition, a second condition, a third condition, or a fourth condition. In the first condition, the relative dielectric constant of the first member region 31 is different from the relative dielectric constant of the second member region 32. In the second condition, the density of the multiple holes 38h included in the first member region 31 is different from the density of the multiple holes 38h included in the second member region 32. In the third condition, the average size of the multiple holes 38h included in the first member region 31 is different from the average size of the multiple holes 38h included in the second member region 32. In the fourth condition, the configuration of the structure body 37 provided in the first member region 31 is different from the configuration of the structure body 37 provided in the second member region 32.
For example, by providing the first member 30 including the dielectric 38, the control of the guide wavelength is easier, and the control range of the guide wavelength is increased.
As shown in
The major radiation direction 81D of the first electromagnetic wave 81 radiated from the multiple radiating parts 20 is taken as (θ, ϕ)=(θ0, ϕ0). When the spacing Sϕ is small enough that grating lobes substantially do not occur, the spacing Sϕ can be set relatively freely to values regardless of the major radiation direction 81D.
On the other hand, the spacing Sρ is set to an appropriate value. A phase distribution in the aperture plane necessary for the beam tilt is formed thereby. According to the embodiment, the spacing Sρ may be determined by the following first formula.
In the first formula, “λ0” is the free-space wavelength. “ξ” is the slow-wave ratio. The slow-wave ratio is the ratio of the guide wavelength λg in the radial waveguide to the free-space wavelength λ0. That is, ξ=λ0/λg.
For example, the slow-wave structure of the first member 30 is formed using the dielectric 38 having the relative dielectric constant εr. In such a case, ξ=(εr)1/2.
When the slow-wave ratio ξ in the radial waveguide is uniform in the waveguide 10, Sρ changes according to the angle ϕ. The spacing Sρ of the multiple radiating parts 20 is a minimum when ϕ=ϕ0+180º. The minimum value min(Sr) of the spacing Sρ is represented by the following second formula.
On the other hand, the spacing Sp of the multiple radiating parts 20 is a maximum when ϕ=ϕ0. The maximum value max(Sρ) of the spacing Sp is represented by the following third formula.
As shown in
On the other hand, the minimum value min(Sρ) is less than 0.4Δ0 when the slow-wave ratio ξ is greater than 2. For example, when the multiple radiating parts 20 include slot pairs, the slots have a maximum length of about 0.5λ0. Also, the slot pair spacing is set to about λg/4 to suppress reflections. It is therefore difficult to arrange the slot pairs in regions of narrow element spacing. Short slots that have weak radiation amounts are used to arrange the slot pairs. For example, the design freedom degrades when the slot pair spacing is reduced by sacrificing reflection. Also, the performance of the antenna degrades.
When the slow-wave ratio ξ in the radial waveguide is constant, the spacing Sρ fluctuates according to the angle ϕ as described above. When the slow-wave ratio ξ is increased to set the maximum value max(Sρ) to be less than λ0/(1+|sin θ0|) so that grating lobes no longer occur, the spacing Sρ becomes narrow, and regions occur where it is difficult to arrange the slot pairs.
In contrast, according to the embodiment, the slow-wave ratio ξ in the radial waveguide is appropriately controlled according to the angle ϕ. Thereby, the spacing Sρ can be in the desired range (e.g., constant) regardless of the angle ϕ.
For example, the following fourth formula can be derived from the first formula.
For example, by changing the slow-wave ratio ξ in the radial waveguide according to the fourth formula, the spacing Sρ can be constant regardless of the angle ϕ.
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According to the embodiment as described above, an extremely short spacing Sρ can be suppressed by appropriately changing the slow-wave ratio ξ distribution according to the angle ϕ. For example, the regions in which the multiple radiating parts 20 (e.g., the slot pairs) can be located increase. The design freedom can be improved. The performance of the antenna device 110 can be improved.
For example, according to the embodiment, the first member 30 that includes the dielectric 38 can be used to easily reduce the relative dielectric constant in regions where the slow-wave ratio ξ is low. For example, the dielectric loss can be reduced.
According to the embodiment, it is desirable for the spacing Sρ of the multiple radiating parts 20 in the radial direction passing through the feed point 10c along the first region 10r to be less than λ0/(1+sin θ0). “λ0” is the wavelength of the high-frequency signal in free space. “θ0” is the angle between a direction (the Z-axis direction) perpendicular to the first region 10r and the major radiation direction 81D of the first electromagnetic wave 81 radiated from the multiple radiating parts 20 (see
As described above, one of the multiple radiating parts 20 may include a slot pair. For example, the reflections from the two slots are canceled thereby. The reflections of the multiple radiating parts 20 can be reduced thereby. For example, the performance of the antenna can be improved by adjusting the slot length, slot width, slot position, distance between two slots, etc.
According to the embodiment, the multiple radiating parts 20 may be capable of radiating a circularly polarized wave. By radiating a circularly polarized wave, for example, wireless communication or the like using the first electromagnetic wave 81 radiated from the antenna device 110 is easy regardless of the orientation of the polarized wave to be transmitted.
As described above, the multiple radiating parts 20 may be arranged in a substantially spiral configuration. For example, the structure of the feed point 10c can be simplified. For example, the coaxial cable can be connected to the center of the radial waveguide; and the spirally-arranged multiple radiating parts 20 can be excited by a coaxial mode feeding.
As described above, the multiple radiating parts 20 may be provided in a substantially concentric circular configuration. For example, good radiation characteristics are obtained even for a small-scale antenna device in which the number of the multiple radiating parts 20 is small. For example, power is fed to the waveguide 10 in a rotational mode. The structure of the feed point 10c can be simplified by using the multiple radiating parts 20 in a concentric circular configuration. For example, because the symmetry of the arrangement of the multiple radiating parts 20 is good, good radiation characteristics are easily obtained even for a small-scale antenna device 110.
An electromagnetic wave is radiated (transmitted) from the antenna device 110 in the description above. According to the embodiment, the antenna device 110 may receive an electromagnetic wave. Even when an electromagnetic wave is received by the antenna device 110, for example, a tilted electromagnetic wave can be received with good characteristics.
The waveguide 10 is a rectangular waveguide in the antenna device 111 according to the embodiment illustrated in
In the antenna device 111 as shown in
Thus, according to the embodiment, other than a radial waveguide, the waveguide 10 may be a rectangular waveguide. The waveguide 10 may be, for example, a ridge waveguide. The waveguide 10 may be, for example, a gap waveguide. The waveguide 10 may be, for example, a parallel-plate waveguide. The waveguide 10 may be, for example, a dielectric waveguide. According to the embodiment, in the various waveguides 10, for example, the slow-wave ratio ξ of the beam tilt direction is high (the guide wavelength is short), and the slow-wave ratio ξ in the direction opposite to the beam tilt direction is low (the guide wavelength is long). A beam tilt antenna in which grating lobes are suppressed is obtained thereby, without making the spacing of the multiple radiating parts 20 extremely narrow.
As shown in
The first driver 10D is configured to rotate the waveguide 10 in a plane (the X-Y plane) including the first region 10r. The first electromagnetic wave 81 that is radiated from the multiple radiating parts 20 may be conically scanned by the rotation of the waveguide 10.
The first driver 10D mechanically (physically) rotates the waveguide 10. For example, the beam (the first electromagnetic wave 81) can be conically scanned. Unlike a phased array that electronically performs beam scanning, the beam scanning is possible without using circuit elements such as phase shifters, etc.
According to the second embodiment, the antenna device 120 may be utilized as a receiving device. For example, an electromagnetic wave arriving along the direction of the angle (θ0, ϕ0) can be received.
As shown in
In the antenna device 130, the transmissive member 50 is configured to transmit the first electromagnetic wave 81 radiated from the multiple radiating parts 20. The transmissive member 50 may be configured to change the transmission phase of the first electromagnetic wave 81. For example, the direction of a second electromagnetic wave 82 radiated from the transmissive member 50 changes according to the change of the transmission phase.
For example, the transmissive member 50 tilts the beam by changing the pass phase of the electromagnetic field of the first electromagnetic wave 81. The tilt angle of the beam due to the transmissive member 50 may be the same as or different from the tilt angle of the beam due to the waveguide 10.
In the example of
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The transmissive member 50 may include a transmit-array. The transmit-array is, for example, an array of multiple elements (unit cells) having different pass phases.
In the example of
In the example of
For example, the transmissive members 50 illustrated in
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The transmissive member 50 overlaps the waveguide 10. In this state, the waveguide 10 is rotated the angle ϕ1, and the transmissive member 50 is rotated the angle ϕ2. In such a case, the x-component “kx” and the y-component “ky” of the wave number of the second electromagnetic wave 82 passing through the transmissive member 50 are represented by the following fifth formula.
In the fifth formula, a wave number k0 is 2π/λ0. λ0 is the free-space wavelength.
The tilt direction (θ0, ϕ0) of the beam of the antenna device 120 from the fifth formula is represented by the following sixth formula and seventh formula.
“kx” and “ky” are changed by the angle ϕ1 (the rotation angle) of the waveguide 10 and the angle ϕ2 (the rotation angle) of the transmissive member 50. The tilt direction (θ0, ϕ0) of the beam can be changed by these angles.
For example, the waveguide 10 that has an angle θ1 of not less than 30 degrees and the transmissive member 50 that has the angle θ2 of not less than 30 degrees are combined. The angle ϕ1 of the waveguide 10 and the angle ϕ2 of the transmissive member 50 are changed (rotated) in the range of not less than −180 degrees and not more than 180 degrees. Accordingly, the angle θ0 changes in the range of not less than 0 degrees and not more than 90 degrees, and the angle ϕ0 changes in the range of not less than −180 degrees and not more than 180 degrees. The two-dimensional beam scanning is possible in any direction.
These figures illustrate the tilt direction (θ0, ϕ0) of the beam when the waveguide 10 and the transmissive member 50 are rotated. In the example, the angle θ1 and the angle θ2 are 30 degrees. The angle ϕ1 of the waveguide 10 and the angle ϕ2 of the transmissive member 50 are changed in the range of not less than −180 degrees and not more than 180 degrees.
By changing the angle ϕ1 and the angle ϕ2 as shown in
By changing the angle ϕ1 and the angle ϕ2 as shown in
The transmissive member 50 may be included as described above. The direction of the first electromagnetic wave 81 radiated from the waveguide 10 can be changed by the transmissive member 50. For example, the range of the beam scanning can be increased. The transmissive member 50 may be mechanically rotated. The second driver 50D may perform the rotation. The range of the beam scanning can be further increased.
For example, two-dimensional beam scanning is made possible by the rotation of the waveguide 10 and the rotation of the transmissive member 50. For example, in a reference example in which beam scanning is performed electronically by a phased array, an additional circuit of phase shifters or the like is included. According to the embodiment, such an additional circuit is unnecessary. According to the embodiment, for example, beam scanning can be performed inexpensively.
The equiphase surface 81a illustrated in
When the equiphase surface 81a is nonlinear, the pass phase distribution 82a may be changed to correct the equiphase surface 81a. When the pass phase distribution 82a is nonlinear, the equiphase surface 81a may be changed to correct the pass phase distribution 82a.
As shown in
In the antenna device 132, the rotary joint 10R is configured to hold the waveguide 10 and the transmissive member 50 at any angle. Accordingly, twisting and damage of the transmission line for power feeding is suppressed when the waveguide 10 and the transmissive member 50 are mechanically rotated.
According to the embodiment, the first driver 10D and the second driver 50D described above may include motors, etc.
According to the third embodiment, the antenna device (the antenna devices 130 to 132) may be utilized as a receiving device. For example, an electromagnetic wave that arrives along the direction of the angle (θ0, ϕ0) can be received.
A fourth embodiment relates to a wireless device.
As shown in
For example, by providing the electrical circuit 201, the antenna device 110 can be utilized as a wireless communication device, a radar, a wireless power supply device, etc.
For example, the electrical circuit 201 is configured to supply a high-frequency signal to the antenna device 110. The electrical circuit 201 causes the antenna device 110 to radiate an electromagnetic wave. When the antenna device 110 receives an electromagnetic wave, the electrical circuit 201 is configured to demodulate a high-frequency signal.
According to the embodiment, the antenna device (e.g., the antenna device 110) and the wireless device 210 are applicable to wireless power transmission, radar, a wireless communication device using a phased array, etc.
According to the embodiment, grating lobes can be suppressed in an array antenna having beam tilt. The design freedom can be increased.
Embodiments may include the following configurations (e.g., technological proposals).
An antenna device, comprising:
The antenna device according to Configuration 1, wherein
The antenna device according to Configuration 2, wherein
The antenna device according to Configuration 3, wherein
The antenna device according to Configuration 1 or 2, wherein
The antenna device according to any one of Configurations 1 to 5, wherein
The antenna device according to Configuration 1, wherein
The antenna device according to any one of Configurations 1 to 7, wherein
The antenna device according to any one of Configurations 1 to 8, wherein
The antenna device according to any one of Configurations 1 to 9, wherein
The antenna device according to any one of Configurations 1 to 10, wherein
The antenna device according to any one of Configurations 1 to 10, wherein
The antenna device according to Configuration 1, further comprising:
The antenna device according to Configuration 1, further comprising:
The antenna device according to Configuration 14, further comprising:
An antenna device, comprising:
A wireless device, comprising:
According to embodiments, an antenna device and a wireless device can be provided in which the characteristics can be improved.
Hereinabove, exemplary embodiments of the invention are described with reference to specific examples. However, the embodiments of the invention are not limited to these specific examples. For example, one skilled in the art may similarly practice the invention by appropriately selecting specific configurations of components included in antenna devices such as waveguides, transmissive members, drivers etc., from known art. Such practice is included in the scope of the invention to the extent that similar effects thereto are obtained.
Further, any two or more components of the specific examples may be combined within the extent of technical feasibility and are included in the scope of the invention to the extent that the purport of the invention is included.
Moreover, all antenna devices and wireless devices practicable by an appropriate design modification by one skilled in the art based on the antenna devices and the wireless devices described above as embodiments of the invention also are within the scope of the invention to the extent that the purport of the invention is included.
Various other variations and modifications can be conceived by those skilled in the art within the spirit of the invention, and it is understood that such variations and modifications are also encompassed within the scope of the invention.
While certain embodiments have been described, these embodiments have been presented by way of example only, and are not intended to limit the scope of the inventions. Indeed, the novel embodiments described herein may be embodied in a variety of other forms; furthermore, various omissions, substitutions and changes in the form of the embodiments described herein may be made without departing from the spirit of the inventions. The accompanying claims and their equivalents are intended to cover such forms or modifications as would fall within the scope and spirit of the invention.
Number | Date | Country | Kind |
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2023-008851 | Jan 2023 | JP | national |