1. Field of the Invention
The present invention relates to a waveguide, a slotted antenna, and a horn antenna preferably for use in a millimeter wave-based onboard radar apparatus, in particular, a digital beam forming (DBF) radar that monitors the direction of travel of an automobile.
2. Description of the Related Art
A DBF radar includes a receiving antenna array composed of a plurality of receiving antenna elements arranged at predetermined intervals (typically, regular intervals) in a scan direction. The DBF radar converts received signals from each receiving antenna element into digital data, performs arithmetic processing on the digital data to impart a phase shift to each received signal, and synthesizes the phase-shifted received signal to generate an equivalent scan beam. The DBF radar can scan at high speed with high precision without the need for any drive part or movable mechanism and therefore is widely used as the onboard millimeter wave radar. However, the DBF radar requires a measure to prevent erroneous detection due to the grating lobe phenomenon.
Japanese Patent Laid-Open No. 2012-147105 discloses a patch antenna unit including transmitting antennas successively displaced and longitudinally symmetrically arranged in a V shape. Side lobes are reduced by using null characteristics of the V-shaped arrangement. However, if the patch antenna is supplied with electric power via a micro-strip line, the dielectric loss is high in the frequency band of the millimeter wave. If a waveguide were used for electric power supply, the loss would be reduced. However, there has not been known any method of supplying electric power to the V-shaped antenna array through a waveguide.
Preferred embodiments of the present invention provide a waveguide, a slotted antenna, and a horn antenna which supply electric power through a single waveguide to an antenna array at least partially arranged in a V-shape.
A preferred embodiment of the present invention provides a waveguide that transmits an electromagnetic wave having an electric field that oscillates in a first direction, the waveguide transmitting the electromagnetic wave in a second direction perpendicular to the first direction, the waveguide including, at least three rectangular waveguide portions, and a protruding wall and a retracted wall that connect a rectangular waveguide portion to another rectangular waveguide portion, wherein each of the rectangular waveguide portions has a tubular shape extending in the second direction, an inner wall of each rectangular waveguide portion has a rectangular cross section, the rectangular waveguide portions are arranged in the second direction, inner spaces of the at least three rectangular waveguide portions are connected to each other, the protruding wall extends from one of a pair of side surfaces of the rectangular waveguide portion opposed in a third direction toward the other of the pair of side surfaces, and the retracted wall extends from the other of the pair of side surfaces toward the one of the pair of side surfaces, the third direction being perpendicular to both the first direction and the second direction, at least one rectangular waveguide portion of the at least three rectangular waveguide portions includes an inner space having a length within a predetermined range in the second direction, the at least one rectangular waveguide portion being disposed between other two rectangular waveguide portions in the second direction; and the predetermined range is between (λg−λg/8)/(2n+M) and (λg+λg/8)/(2n+M), where n denotes a natural number equal to or greater than 2, and M denotes a natural number excluding 0.
Preferred embodiments of the present invention enables electric power supply to an antenna array that is at least partially arranged in a V shape through a single waveguide.
The above and other elements, features, steps, characteristics and advantages of the present invention will become more apparent from the following detailed description of the preferred embodiments with reference to the attached drawings.
Inner spaces of the rectangular waveguide portions 10 and 11 each have a tubular shape extending in the second direction, and each of inner walls of the rectangular waveguide portions has a rectangular cross section. The rectangular waveguide portions 10 and 11 have the same width in the X direction. The positions of the rectangular waveguide portions 10 and 11 in the X direction differ by S, which is smaller than the width of the rectangular waveguide portions 10 and 11.
The rectangular waveguide portions 10 and 11 are preferably connected to each other at the shifting plane 2 with a lateral shift S. The portions of the inner spaces of the rectangular waveguide portions 10 and 11 other than the portions shared by the rectangular waveguide portions 10 and 11 are closed with conductive walls. Conductive walls that close the portions of the inner spaces of the rectangular waveguide portions 10 and 11 other than the portions shared by the rectangular waveguide portions 10 and 11 include a protruding wall 90 and a retracted wall 91, which preferably define a step surface. The protruding wall 90 and the retracted wall 91 connect the rectangular waveguide portion 10 and the rectangular waveguide portion 11 to each other. The protruding wall 90 extends in the +X direction from a −Y-directional end of a −X-directional side surface of a pair of side surfaces of the rectangular waveguide portion 11 opposed in the X direction, and is connected to a +Y-directional end of a −X-directional side surface of the rectangular waveguide portion 10. On the other hand, the retracted wall 91 extends in the +X direction from a −Y-directional end of a +X-directional side surface of the pair of side surfaces of the rectangular waveguide portion 11 opposed in the X direction, and is connected to a +Y-directional end of a +−X-directional side surface of the rectangular waveguide portion 10. In this detailed description, a waveguide of such a structure is referred to as a laterally shifting waveguide. The laterally shifting waveguide is able to supply electric power to an antenna displaced in the width direction (X direction) of the waveguide. However, reflection of the radio wave occurs at the shifting plane. In order to cancel the reflection and achieve a reflection matching condition, an additional structural modification is needed.
For small antennas that use radio waves in the millimeter wave frequency band, a hollow waveguide is preferably manufactured by, for example, carving a rectangular groove in a flat metal plate and covering the flat metal plate with a metal plate.
The shifts between the rectangular waveguide portion 10 and the rectangular waveguide portion 11 and between the rectangular waveguide portion 11 and the rectangular waveguide portion 12 are denoted as S1 and S2, respectively. The axial length of the rectangular waveguide portion 11, which is the length of the inner space thereof in the second direction, is denoted as L. In this example, the lateral widths Wa in the X direction of the rectangular waveguide portions 10, 11 and 12 are preferably the same. Depending on the design, however, the width Wa may differ between the rectangular waveguide portions. The two-step laterally shifting waveguide 101 is able to achieve reflection matching by itself.
In the following, expressions concerning reflection matching will be shown.
Γ=γ·exp(jφ+jρ) Expression 1
where Γ denotes a complex reflection coefficient, γ denotes a reflection amplitude ratio, ϕ denotes a phase shift of the reflected wave, and ρ denotes a phase difference due to the propagation path length. As required, subscripts indicating portions or the like will be used for identification of the symbols.
To be precise, the influence of multiple reflection and the phase shift of the transmitted wave, which is not reflected but is transmitted by the shifting plane, need to be considered. For approximation, however, these factors are omitted. In addition, it is assumed that the phase shift of the reflected wave is equal or substantially equal to 90° (π/2). With reference to the phase at a midpoint C in the rectangular waveguide portion 11, the reflected waves Γ1 and Γ2 at the shifting planes 21 and 22 are expressed by the following expressions.
In these expressions, λg denotes the guide wavelength in the waveguide, and kg=2π/λg. The italicized letter j denotes an imaginary unit. Provided that the reflected wave of the entire system, that is, the reflection coefficient to the rectangular waveguide portion 10 is denoted as Γ0, Γ0 is expressed by the following expression.
From Expression 4, Γ0=0 when γ1=γ2, and cos(kg*L)=0.
γ1 and γ2 are proportional to the widths of the retracted walls 911 and 912. Thus, in order for the condition that γ1=γ2 to be satisfied, it is required that S1=S2. The condition that cos(kg*L)=0 is satisfied, when L=λg/4 or an odd multiple of λg/4. Thus, these two requirements are conditions required to achieve reflection matching.
Reflection matching is able to be achieved in a laterally shifting waveguide with more steps. A laterally shifting waveguide with n laterally shifted connections is referred to as an n-step laterally shifting waveguide. Provided that all the rectangular waveguide portions 11 to 1(n−1) have the same axial length (=L), and the shifts between the rectangular waveguide portions at laterally shifted connections 21 to 2n are the same (=S), the reflection coefficient of the entire system is expressed by the following expression.
where γs denotes a reflection amplitude ratio at each retracted wall.
When L=λg/(2n), Γ0 expressed by this expression equal to 0, and reflection matching is achieved. That is, when n (equal to or greater than 2) laterally shifted connections are provided, the condition of L to achieve reflection matching is that L=λg/(2n+M) (M denotes a natural number including 0).
Although, L is no need to be equal to λg/(2n+M) strictly. If L is between (λg−λg/8)/(2n+M) and (λg+λg/8)/(2n+M), efficiency of reflection matching is achieved.
If the long side width of a rectangular waveguide portion is equal to or smaller than λ/2, the rectangular waveguide is cut off and cannot transmit the wave. Thus, the lateral width (Wa−S) of the joint between two waveguides at the shifting plane 2 has to be greater than λ/2. Thus, the following expression concerning the shift S is derived.
S<Wa−λ/2 Expression 6
If a two-step structure cannot achieve reflection matching, an n-step structure (n>3) can be useful. However, the principle of reflection matching is the same as that for the two-step structure. Thus, in the following, reflection matching of an antenna using the two-step laterally shifting waveguide will be described.
The rectangular horn 4 preferably includes a flat surface portion 40 that extends from each short side of the slot 3 to the base portion of the rectangular horn 4 in the direction away from the axis of the rectangular horn 4. That is, the horn antenna preferably includes the flat surface portion 40. In this example, the flat surface portion 40 is perpendicular to the axis of the rectangular horn 4. The flat surface portion 40 produces an electric field of the TE30 mode, which is a higher-order mode. Since the electric field of the TE30 mode and the electric field of the TE10 mode, which is the fundamental mode, are combined with each other, the gain of the antenna is able to be increased in a predetermined azimuth.
In
In the following, an example of a reflection matching design will be derived by reference to expressions.
In this example, approximately, in the range of Wb/λ equal to or smaller than 0.2 or substantially 0.2, the radiation amplitude ratio increases as the dimension of the short side decreases.
The reflected wave from the radiator is expressed by the following expression.
First, an equal amplitude condition for Γw and Γh will be described. The magnitude of Γw varies with L, and L is determined according to the following expression.
2γs·cos(kg·L)=±γh Expression 9
where γh denotes a reflection amplitude ratio of the radiator.
The left side is a positive value when L<λg/4 and is a negative value when λg/4<L<λg/2.
For reflection matching to be achieved in the reflected wave from the radiator, in the case where L<λg/4, the following expression has to be satisfied.
where m denotes an odd number.
A condition required for the laterally shifting waveguide to be housed in a vertical spacing λg of the radiator is expressed by the following expression.
D=λg/8 or 5λg/8
Similarly, in the case where λg/4<L<λg/2, the following expression holds.
In this case, D=3λg/8.
A plurality of rectangular waveguide portions (10, 11, 12, 11′, 12′, . . . ) are arranged in the Y direction to define a laterally shifting waveguide 104 that has the shape of a letter V open in the −X direction as a whole. This structure can be formed by at least three rectangular waveguide portions.
It has been described above that to use the two-step laterally shifting waveguide is effective to achieve reflection matching. However, the above description concerns an approximate analysis under a predetermined condition. As a general design method, a direct analysis using a three-dimensional simulator or the like is suitable. Based on the direct analysis, precise design dimensions are able to be determined considering all factors including the influence of multiple reflection without the need to separately analyze the reflection amplitude ratio, the phase shift or the like of each wave. Furthermore, a structure is also possible in which not only the lateral shift but also the dimension Wb of the short side of the rectangular waveguide portion (depth of the groove) can vary.
For example, a traveling-wave array antenna is typically designed so that the radiation amplitude ratio gradually increases from the power supply end toward the distal end, since the electric power in the power supply path decreases each time the radio wave passes through a radiating element. This is able to be achieved by changing dimensions of the slot and the horn. However, in that case, the radiation directivity characteristics also change, and therefore the design becomes more complicated. As an alternative, it is useful to change the dimension of the short side of the rectangular waveguide portion. As shown by the alternate long and short dash line 70 in
Furthermore, rectangular waveguide portions 10″, 11″, 12″, 13″, 14″ and 15″ are connected in the −Y direction. A power supply opening 6 is provided between the rectangular waveguide portions 10 and 10″. As shown in
Of the preferably fourteen transmitting horns, twelve transmitting horns 802 excluding transmitting horns 801 located at the opposite ends in the Y direction are arranged at regular intervals in the Y direction. A pitch B1 between the transmitting horn 801 at either end in the Y direction and the adjacent transmitting horn 802 is smaller than a pitch B2 between adjacent two of the inner twelve transmitting horns. A dimension C1 in the Y direction of the transmitting horns 801 at the opposite ends is smaller than a dimension C2 in the Y direction of the inner twelve transmitting horns 802.
The receiving portion 7 is disposed at the open side of the letter V defined by the transmitting antenna array 80. The receiving portion 7 is an antenna array preferably defined by five receiving antenna subarrays 70a, 70b, 70c, 70d and 70e. Each receiving antenna subarray preferably includes a rectangular waveguide portion and fourteen receiving horns 71. The rectangular waveguide portion is not shown because the rectangular waveguide portion is disposed on the side opposite to the receiving horns 71. Each receiving antenna subarray extends in the Y direction, and the receiving horns 71 are arranged at regular intervals in the Y direction. The five receiving antenna subarrays are also arranged at regular intervals in the X direction. In the Y direction, the five receiving antenna subarrays are preferably disposed at at least three different positions. More specifically, the five receiving antenna subarrays are preferably arranged as follows. With reference to the receiving antenna subarray 70c located at the middle, the receiving antenna subarrays 70b and 70d adjacent to the receiving antenna subarray 70c are disposed at positions shifted by about 3.15 mm in the −Y direction, for example. The receiving antenna subarrays 70a and 70e located on the outer side of the receiving antenna subarrays 70b and 70d in the X direction in the receiving portion 7 are disposed at positions shifted by about 1.35 mm, for example, in the −Y direction with reference to the receiving antenna subarray 70c located at the middle.
Of the preferably fourteen receiving horns of each of the five receiving antenna subarrays 70a, 70b, 70c, 70d and 70e, twelve receiving horns 702 excluding receiving horns 701 located at the opposite ends in the Y direction are arranged at regular intervals in the Y direction. A pitch D1 between the receiving horn 701 at either end in the Y direction and the adjacent receiving horn 702 is preferably smaller than a pitch D2 between adjacent two of the inner twelve receiving horns. A dimension E1 in the Y direction of the receiving horns 701 at the opposite ends is preferably smaller than a dimension E2 in the Y direction of the inner twelve receiving horns 702.
While preferred embodiments of the present invention have been described above, it is to be understood that variations and modifications will be apparent to those skilled in the art without departing from the scope and spirit of the present invention. The scope of the present invention, therefore, is to be determined solely by the following claims.
Number | Date | Country | Kind |
---|---|---|---|
2015-168365 | Aug 2015 | JP | national |
2015-173073 | Sep 2015 | JP | national |
2015-191860 | Sep 2015 | JP | national |
2016-146694 | Jul 2016 | JP | national |
Number | Name | Date | Kind |
---|---|---|---|
4786913 | Barendregt et al. | Nov 1988 | A |
20120229362 | Abe | Sep 2012 | A1 |
20130033404 | Abe | Feb 2013 | A1 |
Number | Date | Country |
---|---|---|
2011-193421 | Sep 2011 | JP |
2011-193421 | Sep 2011 | JP |
2012-147105 | Aug 2012 | JP |
Entry |
---|
Abe, A.; “Radar Antenna Unit and Radar Device,”; U.S. Appl. No. 15/248,132, filed Aug. 26, 2016. |
Number | Date | Country | |
---|---|---|---|
20170062931 A1 | Mar 2017 | US |