INTEGRATED WAVEGUIDE CAVITY ANTENNA AND REFLECTOR DISH

Abstract

A feed assembly for a parabolic dish reflector is described. The feed assembly includes a waveguide cavity locatable at the focal point, or any other desired off-boresight location corresponding point, of the parabolic dish, at least one first radiating element optimized for operation at a first frequency band and provided on a top surface of the waveguide cavity, and a plurality of second radiating elements each optimized for operation at a second band of frequencies and provided on the top surface of the waveguide cavity.

Description

BACKGROUND

1. Field

The subject invention relates to a waveguide cavity antenna for a reflector dish and the combination of the waveguide cavity antenna and reflector dish.

2. Related Art

Various antennas are known in the art for receiving and transmitting electromagnetic radiation. Physically, an antenna consists of a radiating element made of conductors that generate radiating electromagnetic field in response to an applied electric and the associated magnetic field. The process is bi-directional, i.e., when placed in an electromagnetic field, the field will induce an alternating current in the antenna and a voltage would be generated between the antenna's terminals or structure. The feed network, or transmission network, conveys the signal between the antenna and the transceiver (source or receiver). The feeding network may include antenna coupling networks and/or waveguides. An antenna array refers to two or more antennas coupled to a common source or load so as to produce a directional radiation pattern. The spatial relationship between individual antennas contributes to the directivity of the antenna.

While the antenna disclosed herein is generic and may be applicable to a multitude of applications, one particular application that can immensely benefit from the subject antenna is the reception of satellite television (Direct Broadcast Satellite, or “DBS”). In DBS, reception is accomplished with a directional antenna aimed at a geostationary satellite. In the standard DBS design, a reflector dish is coupled with one or more antenna feeds, known as feedhorns, each of the feedhorns situated so as to receive reflected signals from the reflector dish corresponding to one of the geostationary satellites. The feedhorn utilizes a waveguide structure with a horn-shaped extension. Each feedhorn is dedicated to a specific angular location in the sky—the angular location is controlled by the lateral movement (i.e., vertical or horizontal movement to correspond to each specific angular location in the sky) of the horn-shaped extension with respect to the focal point of the reflector dish.

A reflector antenna may have multiple feeds, each feed corresponding to a specific band of frequency, such as the Ku band or the Ka band or portions thereof, coming from a specific satellite, or multiple satellites. Depending on the position of the satellites in space, the corresponding feeds may have to be ideally located very close to each other. Ideal positions of multiple feeds may even overlap each other if multiple feeds are coupled to a common reflector dish. In order to physically accommodate the multiple feeds with respect to the common reflector dish, each of the feeds may be positioned at a location close to, but not exactly coinciding with the focal point of the reflector dish. Thus, received signal quality may be degraded based on the distance of a feed from the ideal focal point associated with a specific focal length to diameter ratio (f/d ratio) of the dish.

SUMMARY

The following summary is included in order to provide a basic understanding of some aspects and features of the invention. This summary is not an extensive overview of the invention and as such it is not intended to particularly identify key or critical elements of the invention or to delineate the scope of the invention. Its sole purpose is to present some concepts of the invention in a simplified form as a prelude to the more detailed description that is presented below.

The present invention provides a solution that effectively co-locates the phase center points of multiple feeds or feed arrays at the focal point of the reflector dish, each feed corresponding to a band of frequency coming from a satellite. Thus, the present invention enables multiple frequency reception in a single antenna. Looking at the same satellite location i.e., co-location capabilities in cost effective manner fit for mass-production.

According to certain aspects of the invention, an antenna is disclosed, where the antenna comprises a first array of feed elements corresponding to a first frequency band having a first phase center point; a second array of feed elements corresponding to a second frequency band having a second phase center point coinciding with the first phase center point; and a reflector dish, wherein the common phase center point of the first and second arrays is located at a focal point of the reflector dish.

In one embodiment, a feed element of the second array is physically located at the first phase center point of the first array. A separation between two feed elements of the first array is such that the separation can physically accommodate one or more feed elements of the second array.

In one example, the feed comprises an 1×2 array of elements for a lower frequency band, such as the Ku band, and positioning a single element for a higher frequency band, such as the Ka band in between the two elements of the 1×2 lower frequency band array, and by carefully controlling the phase center location, co-locating the two frequency bands. The phase center of the lower frequency band would be at the mid-point between the two elements of the 1×2 array, while the phase center of the single element for the higher frequency band would be its physical center point. This way the two frequency bands are co-located.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings, which are incorporated in and constitute a part of this specification, exemplify the embodiments of the present invention and, together with the description, serve to explain and illustrate principles of the invention. The drawings are intended to illustrate major features of the exemplary embodiments in a diagrammatic manner. The drawings are not intended to depict every feature of actual embodiments nor relative dimensions of the depicted elements, and are not drawn to scale.

FIGS. 1A and 1B depict an example of an antenna according to an embodiment of the invention.

FIG. 2 illustrates a cross section of an antenna according to the embodiment of FIGS. 1A and 1B.

FIG. 3A depicts an embodiment of an antenna that may be used to transmit/receive two waves of cross polarization.

FIG. 3B depicts a cross section similar to that of FIG. 2, except that the arrangement enables excitation of two orthogonal polarizations from the same face.

FIG. 4 depicts an antenna according to another embodiment of the invention.

FIG. 5 depicts another embodiment of an antenna according to the subject invention.

FIG. 6 illustrates an embodiment optimized for operation at two different frequencies and optionally two different polarizations.

FIG. 7 depicts an embodiment of the invention using a radiating element having flared sidewalls.

FIG. 8A depicts an embodiment of an antenna optimized for circularly polarized radiation.

FIG. 8B is a top view of the embodiment of FIG. 8A.

FIG. 8C depicts another embodiment of an antenna optimized for circularly polarized radiation.

FIG. 8D illustrate a top view of a square circularly polarizing radiating element, while FIG. 8E illustrates a top view of a cross-shaped circularly polarizing radiating element.

FIG. 9 illustrates a linear antenna array according to an embodiment of the invention.

FIG. 10 provides a cross-section of the embodiment of FIG. 9.

FIG. 11 illustrates a linear array fed by a sectorial horn as a source, according to an embodiment of the invention.

FIG. 12A illustrates an example of a two-dimensional array according to an embodiment of the invention

FIG. 12B illustrates a two-dimensional array according to another embodiment of the invention configured for operation with two sources.

FIG. 12C is a top view of the array illustrated in FIG. 12B.

FIG. 13 illustrates and example of a circular array antenna according to an embodiment of the invention.

FIG. 14 is a top view of another embodiment of a circular array antenna of the invention.

FIG. 15 illustrates a process of designing a Cartesian coordinate array according to an embodiment of the invention.

FIGS. 16 and 16A-16E illustrate embodiments of an RF Source reflector feed for planer wave in near field regime of the electromagnetic field, according to the invention.

FIG. 17 illustrate another embodiment of an RF feed that includes several different collection pins, which corresponds to different beam locations (MultiBeam feed arrangement).

FIG. 18 illustrates an embodiment having dual-feed arrangement, for the benefit of generating dual polarization, multiple beam antenna. The Two orthogonal feeds each excites the array from a different face and thus generates dual orthogonal polarizations.

FIG. 19 illustrates the principle of beam tilt/scanning over the diagonal of a symmetrical array, with dual polarization capabilities.

FIGS. 20A-20C illustrate an embodiment wherein the inventive reflector feed is utilized for an array operating in two frequencies of different bands. This is the mixed array concept which employs two set of elements, one for each band, where the high band elements are in frequency cutoff for the lower frequency band, and situated in two square array formation.

The smaller square array formation on the upper right hand corner is being fed at the lower frequency and its elements can support the higher band as well.

FIGS. 20D and 20E illustrate variations for the reflector feeds for the mixed array concept.

FIG. 20F illustrates a flow chart for the design of a mixed array antenna.

FIGS. 21A and 21B illustrate another embodiment of the invention enabling simultaneous dual polarization with wide-angle reception, and easily installable antenna.

FIG. 22 illustrates an example of a reflector feed according to an embodiment of the invention, using a horn as an RF source.

FIG. 23 illustrates an example of a patch radiation source which may be used with the reflector feed of the invention.

FIG. 24 schematically illustrates an embodiment of the invention which utilizes the parallel-plate structure as a feeder for a dish antenna.

FIG. 25 illustrates an integrated reflector dish and waveguide cavity antenna according to one embodiment of the invention.

FIG. 26A illustrate a dual-band feeder to a dish antenna according to an embodiment of the invention, while FIG. 26B is a side view of the feeder. FIG. 26C illustrates the cone of each of the feeders, and the resulting combined cone.

FIG. 27 illustrates another dual-band feeder to a dish antenna according to an embodiment of the invention.

FIG. 28 illustrates another feed assembly for a dish antenna according to an embodiment of the invention.

FIG. 29 illustrates yet another embodiment of a feed for a dish antenna.

FIG. 30A shows top schematic view of the feed elements and associated components of the Δf₃ and Δf₄ bands, as discussed with respect to FIG. 29, while FIG. 30B shows top schematic view of the feed elements and associated components of the Δf₃ band only, as discussed with respect to FIG. 29.

FIG. 31 shows example antenna feed assemblies using micro-slots and micro-strip technology.

FIG. 32 shows an embodiment of the antenna feed assembly that comprises a thin, conductive plate including two micro-slot split-feed arrays.

FIG. 33 shows an embodiment of the antenna feed assembly having a conductive plate, one array is a 1×1 array consisting of a single element whose phase center is at the common point.

FIG. 34 shows an embodiment of the antenna feed assembly having microstrip elements and arrays to form the feed to the dish antenna.

FIG. 35 illustrates an embodiment of a dish reflector feed assembly where another array is positioned on plate within another array.

FIG. 36 illustrates an embodiment wherein different arrays corresponding to different frequency bands do not have to comprise same type of feed elements.

DETAILED DESCRIPTION

Various embodiments of the invention are generally directed to radiating elements and antenna structures and systems incorporating the radiating element. The various embodiments described herein may be used, for example, in connection with stationary and/or mobile platforms. Of course, the various antennas and techniques described herein may have other applications not specifically mentioned herein. Mobile applications may include, for example, mobile DBS or VSAT integrated into land, sea, or airborne vehicles. The various techniques may also be used for two-way communication and/or other receive-only applications.

According to an embodiment of the present invention, a radiating element is disclosed, which is used in single or in an array to form an antenna. The radiating structure may take on various shapes, selected according to the particular purpose and application in which the antenna will be used. The shape of the radiating element or the array of elements can be designed so as to control the phase and amplitude of the signal, and the shape and directionality of the radiating/receiving beam. Further, the shape can be used to change the gain of the antenna. The disclosed radiating elements are easy to manufacture and require relatively loose manufacturing tolerances; however, they provide high gain and wide bandwidth. According to various embodiments disclosed, linear or circular polarization can be designed into the radiating element. Further, by various feeding mechanisms, the directionality of the antenna may be steered, thereby enabling it to track a satellite from a moving platform, or to be used with multiple satellites or targets, depending on the application, by enabling multi-beam operation.

According to one embodiment of the present invention, an antenna structure is provided. The antenna structure may be generally described as a planar-fed, open waveguide antenna. The antenna may use a single radiating element or an array of elements structured as a linear array, a two-dimensional array, a circular array, etc. The antenna uses a unique open wave extension as a radiating element of the array. The extension radiating element is constructed so that it couples the wave energy directly from the wave guide.

The element may be extruded from the top of a multi-mode waveguide, and may be fed using a planar wave excitation into a closed common planar waveguide section. The element(s) may be extruded from one side of the planar waveguide. The radiating elements may have any of a number of geometric shapes including, without limitation, a cross, a rectangle, a cone, a cylinder, or other shapes.

FIGS. 1A and 1B depict an example of an antenna 100 according to an embodiment of the invention. FIG. 1A depicts a perspective view, while FIG. 1B depicts a top elevation. The antenna 100 comprises a single radiating element 105 coupled to waveguide 110. The radiating element 105 and waveguide 110 together form an antenna 100 having a beam shape that is generally hemispherical, but the shape may be controlled by the geometry of radiating element 105, as will be explained further below. The waveguide may be any conventional waveguide, and in this example is shown as having a parallel plate cavity using a simple rectangular geometry having a single opening 115 serving as the wave port/excitation port, via which the wave energy 120 is transmitted.

For clearer understanding, the waveguide is shown superimposed over Cartesian coordinates, wherein the wave energy within the waveguide propagates in the Y-direction, while the energy emanating from or received by the radiating element 105 propagates generally in the Z-direction. The height of the waveguide h_w is generally defined by the frequency and may be set between 0.1λ and 0.5λ. For best results the height of the waveguide h_w is generally set in the range 0.33λ to 0.25λ. The width of the waveguide W_w may be chosen independently of the frequency, and is generally selected in consideration of the physical size limitations and gain requirements. Increasing width would lead to increased gain, but for some applications size considerations may dictate reducing the total size of the antenna, which would require limiting the width. The length of the waveguide L_w is also chosen independently of the frequency, and is also selected based on size and gain considerations. However, in embodiments where the backside 125 is close, it serves as a cavity boundary, and the length L_y from the cavity boundary 125 to the center of the element 105 should be chosen in relation to the frequency. That is, where the backside 125 is closed, if some part of the propagating wave 120 continues to propagate passed the element 105, the remainder would be reflected from the backside 125. Therefore, the length Ly should be set so as to ensure that the reflection is in phase with the propagating wave.

Attention is now turned to the design of the radiating element 105. In this particular embodiment the radiating element is in a cone shape, but other shapes may be used, as will be described later with respect to other embodiments. The radiating element is physically coupled directly to the waveguide, over an aperture 140 in the waveguide. The aperture 140 serves as the coupling aperture for coupling the wave energy between the waveguide and the radiating element. The upper opening, 145, of the radiating element is referred to herein as the radiating aperture. The height h_e of the radiating element 105 effects the phase of the energy that hits the upper surface 130 of the waveguide 110. The height is generally set to approximately 0.25λ₀ in order to have the reflected wave in phase. The lower radius r of the radiating element affects the coupling efficiency and the total area πr² defines the gain of the antenna. On the other hand, the angle θ (and correspondingly radius R) defines the beam's shape and may be 90° or less. As angle θ is made to be less than 90°, i.e., R>r, the beam's shape narrows, thereby providing more directionality to the antenna 100.

FIG. 2 illustrates a cross section of an antenna according to the embodiment of FIGS. 1A and 1B. The cross section of FIG. 2 is a schematic illustration that may be used to assist the reader in understanding of the operation of the antenna 200. As is shown, waveguide 210 has a wave port 215 through which a radiating wave is transmitted. The radiating element 205 is provided over the coupling port 240 of the waveguide 210 and has an upper radiating port 245. An explanation of the operation of the antenna will now be provided in the case of a transmission of a signal, but it should be apparent that the exact reverse operation occurs during reception of a signal.

In FIG. 2, the wave front is schematically illustrated as arrows 250, entering via wave port 215 and propagating in the direction Vt. As the wave reaches the coupling port 240, at least part of its energy is coupled into the radiating element 205 by assuming an orthogonal propagation direction, as schematically illustrated by bent arrow 255. The coupled energy then propagates along radiating element 205, as shown by arrows 260, and finally is radiated at a directionality as illustrated by broken line 270. The remaining energy, if any, continues to propagate until it hits the cavity boundary 225. It then reflects and reverses direction as shown by arrow Vr. Therefore, the distance Ly should be made to ensure that the reflecting wave returns in phase with the propagating wave.

Using the inventive principles, transmission of wave energy is implemented by the following steps: generating from a transmission port a planar electromagnetic wave at a face of a waveguide cavity; propagating the wave inside the cavity in a propagation direction; coupling energy from the propagating wave onto a radiating element by redirecting at least part of the wave to propagate along the radiating element in a direction orthogonal (or other angle) to the propagation direction; and radiating the wave energy from the radiating element to free space. The method of receiving the radiation energy is completely symmetrical in the reverse order. That is, the method proceeds by coupling wave energy onto the radiating element; propagating the wave along the radiating element in a propagation direction; coupling energy from the propagating wave onto a cavity by redirecting the wave to propagate along the cavity in a direction orthogonal to the propagation direction; and collecting the wave energy at a receiving port.

The antenna of the embodiments of FIGS. 1A, 1B and 2, can be used to transmit and receive a linearly or circularly polarized wave. FIG. 3A, on the other hand, depicts an embodiment of an antenna that may be used to transmit/receive two waves of cross polarization. Notably, in the embodiment of FIG. 3A, two excitation ports, 315 and 315′ are provided on the waveguide. A first wave, 320, of a first polarization enters the waveguide cavity via port 315, while another wave 320′, of different polarization, enters the waveguide cavity via port 315′. Both waves are radiated via radiating aperture 345, while maintaining their orthogonal polarization.

On the other hand, the embodiment of FIGS. 1A and 1B may also be used to transmit/receive two waves of cross polarization. This is explained with respect to FIG. 3B. FIG. 3B shows a cross section similar to that of FIG. 2, except that the height of the waveguide h_w is set to about λ/2. In this case, if the originating wave has vertical polarization, such as shown in FIG. 2, the transmitted wave will assume a horizontal polarization, as shown in FIG. 2. On the other hand, if the originating wave has a horizontal polarization, as shown in FIG. 3, the wave is coupled to the radiating element 305 and is radiated with a horizontal polarization that is orthogonal to the wave shown in FIG. 2. In this manner, one may feed either on or both waves so as to obtain any polarization required. It should be appreciated that the two polarizations can be combined into any arbitrary polarization by adjusting the phase and amplitude of the two wave sources which excite the antenna.

FIG. 4 depicts an antenna according to another embodiment of the invention. In FIG. 4, Antenna 400 comprises radiating element 405 coupled to waveguide 410, over coupling port 440. In this embodiment the radiating element 405 has generally a polygon cross-section. The height h_e of the element 405 may be selected as in the previous embodiments, e.g., 0.25λ. The bottom width w_L of the element determines the coupling efficiency of the element, while the bottom length L_L defines the lowest frequency at which the antenna can operate at. The area of the radiating aperture 445, i.e., w_u×L_u defines the gain of the antenna. The angle θ, as with the previous embodiments, defines the beam's shape and may be 90° or less. In the embodiment depicted, wave 420, having a first polarization, enters via the single excitation port 415. However, as discussed above with respect to the other embodiments, another excitation port may be provided, for example, instead of cavity boundary 415′. In such a case, a second wave may be coupled, having an orthogonal polarization to wave 420.

FIG. 5 depicts another embodiment of an antenna according to the subject invention. The embodiment of FIG. 5 is optimized for operation at two orthogonal polarizations. The radiating element 505 has a cross-section in the shape of a cross that is formed by two superimposed rectangles. In this manner, one rectangle is optimized for radiating wave 520, while the other rectangle is optimized for radiating wave 520′. Waves 520 and 520′ have orthogonal linear polarization. In the embodiment of FIG. 5 the two superimposed rectangles forming the cross-shape have the same length, so as to operate two waves of similar frequency, but cross-polarization. On the other hand, FIG. 6 illustrates an embodiment optimized for operation at two different frequencies and optionally two different polarizations. As can be seen, the main different between the embodiment of FIGS. 5 and 6 is that the radiating element of FIG. 6 has a cross-section in the shape of a cross formed by superimposed rectangles having different lengths. That is, length L1 is optimized for operation in the frequency of wave 620, while wave L2 is optimized for operation at frequency of wave 620′. Waves 620 and 620′ may be cross-polarized. The intersecting waveguides forming the cross may also be constructed using a centrally located ridge in each waveguide, with the dimensional parameters of the ridge along with L1 and L2 optimized to provide broadband frequency operation.

FIG. 7 depicts an embodiment of the invention using a radiating element 705 having flared sidewalls. Each element comprises a lower perpendicular section and an upper flared section. The sides 702 of the perpendicular section define planes which are perpendicular to the upper surface 730 of the waveguide 710, where the coupling aperture (not shown) is provided. The sides 704 of the flared section define planes which are angularly offset from, and non-perpendicular to the plane defined by the upper surface 730 of the waveguide 710. The element 705 of FIG. 7 is similar to the elements shown in FIGS. 5 and 6, in that it is optimized for operating with two waves having similar or different frequencies and optionally at cross polarization. However, by introducing the flare on the sidewalls, the design of the coupling aperture can be made independently of the design of the radiating aperture. This is similar to the case illustrated in the previous embodiments where the sidewalls are provided at an angle θ less than 90°.

According to one feature of the invention, wide band capabilities may be provided by a wideband XPD (cross polar discrimination), circular polarization element. One difficulty in generating a circular polarization wave is the need for a complicated feed network using hybrids, or feeding the element from two orthogonal points. Another possibility is using corner-fed or slot elements. Current technology using these methods negatively impacts the bandwidth needed for good cross-polarization performance, as well as the cost and complexity of the system. Alternate solutions usually applied in waveguide antennas (e.g., horns) require the use of an external polarizer (e.g., metallic or dielectric) integrated into the cavity. In the past, this has been implemented in single-horn antennas only. Thus, there is a need for a robust wideband circular polarization generator element, which can be built in into large array antennas, while maintaining easy installation and integration of the polarization element in the manufacturing process of the antenna.

FIG. 8A depicts an embodiment of an antenna 800 optimized for circularly polarized radiation. That is, when a planar wave 820 is fed to the waveguide 810, upon coupling to the radiating element 805 slots 890 would introduce a phase shift to the planar wave so as to introduce circular polarization so that the radiating wave would be circularly polarized. As shown, the slots 890 are provided at 45° alignments to the excitation port 815. Consequently, if a second planar wave, 820′ is introduced via port 815′, the radiating element 805 would produce two wave of orthogonal circular polarization.

FIG. 8B is a top view of the embodiment of FIG. 8A. As illustrated in FIG. 8B, for the purpose of generating a circular polarization field, the following polarization control scheme is presented. A planar wave is generated and caused to propagate in the waveguide's cavity, as shown by arrow Vt. A circular polarization is introduced to the planar wave by perturbing the cone element's fields and introducing a phase shift of 90 degrees between the two orthogonal E field components (e.g., the components that are parallel to the slot and the components that are perpendicular to the slot Vx, Vy). This creates a circularly polarized field. This is accomplished without effecting the operation of the array into which the circular polarization element is incorporated. It should be noted that in this example, the perturbation is in a 45 degree relationship to the polarized field that is propagating in the cavity just beneath the element.

In generating the slots, one should take into account the following. The thickness of the slot should be sufficiently large so as to cause the perturbation in the wave. It is recommended to be in the order of 0.05-0.1×. The size of the slots and the area A delimited between them (marked with broken lines) should be such that the effective dielectric constant generated is higher than that of the remaining area of the radiating element, so that the component Vy propagates at a slower rate than the component Vx, to thereby provide a circularly polarized wave of Vx+jVy. Alternatively, one may achieve the increased dielectric constant by other means to obtain similar results. For example, FIG. 8C depicts another embodiment of an antenna optimized for circularly polarized radiation. In FIG. 8C, the radiating element 805 is a cone similar to that of the embodiment of FIG. 1A. However, to generate the circular polarization, a retarder 891 in the form of a piece of material, e.g. Teflon, having higher dielectric constant than air is inserted to occupy an area similar to that of the slots and area A of FIG. 8B.

The circularly-polarizing radiating element of the above embodiments may also be constructed of any other shape. For example, FIG. 8D illustrate a top view of a square circularly polarizing radiating element, while FIG. 8E illustrates a top view of a cross-shaped circularly polarizing radiating element.

Some advantages of this feature may include, without limitation: (1) an integrated polarizer; (2) cross polar discrimination (XPD) greater than 30 dB; (3) adaptability to a relatively flat antenna; (4) very low cost; (5) simple control; (6) wideband operation; and (6) the ability to be excited to generate simultaneous dual polarization. Some adaptations of this feature include, without limitation: (1) a technology platform for any planar antenna needing a circular polarization wideband field; (2) DBS fixed and mobile antennas; (3) VSAT antenna systems; and (4) fixed point-to-point and point-to-multipoint links.

FIG. 9 illustrates a linear antenna array according to an embodiment of the invention. In general, the linear array has 1×m radiating element, where in this example 1×3 array is shown. In FIG. 9 radiating elements 905₁, 905₂, and 905₃, are provided on a single waveguide 910. In this embodiment cone-shaped radiating elements are used, but any shape can be used, including any of the shapes disclosed above. FIG. 10 provides a cross-section of the embodiment of FIG. 9. As illustrated in FIG. 10, the wave 1020 propagates inside the cavity of waveguide 1010 in direction Vt, and part of its energy is coupled to each of the radiating elements as in the previous embodiments. The amount of energy coupled to each radiating element can be controlled by the geometry, as explained above with respect to a single element. Also, as explained above, the distance Ly from the back of the cavity to the last element in the array should be configured so that a reflective wave, if any, would be reflected in phase with the traveling wave. If each radiating element couples sufficient amount of energy so that no energy is left to reflect from the back of the cavity, then the resulting configuration provides a traveling wave. If, on the other hand, some energy remains and it is reflected in phase from the back of the cavity, a standing wave results.

The selection of spacing Sp between the elements enables introducing a tilt to the radiating beam. That is, if the spacing is chosen at about 0.9-1.0λ, then the beam direction is at boresight. However, the beam can be tilted by changing the spacing between the elements. For example, if the beam is to be scanned between 20° and 70° by using a scanning feed, it is beneficial to induce a static tilt of 45° by having the spacing set to about 0.5λ, so that the active scan of the feed is limited to 25° of each side of center. Moreover, by implementing such a tilt, the loss due to the scan is reduced. That is, the effective tilt angle can be larger than the tilt in the x and y components, according to the relationship θ₀=Sqrt(θ_x²+θ_y²).

FIG. 11 illustrates a linear array 1100 fed by a sectoral horn 1190 as a source, according to an embodiment of the invention. In the embodiment shown, rectangular radiating elements 1105 are used, although other shapes may be used. Also, the feed is provided using an H-plan sectoral horn 1190, but other means may be used for wave feed. As before, the spacing Sp can be used to introduce a static tilt to the beam.

As can be understood from the embodiments of FIGS. 9, 10 and 11, a linear array may be constructed using radiating elements incorporating any of the shapes disclosed herein, such as conical, rectangular, cross-shaped, etc. The shape of the array elements may be chosen, at least in part, on the desired polarization characteristics, frequency, and radiation pattern of the antenna. The number, distribution and spacing of the elements may be chosen to construct an array having specific characteristics, as will be explained further below.

FIG. 12A illustrates an example of a two-dimensional array 1200 according to an embodiment of the invention. The array of FIG. 12A is constructed by a waveguide 1210 having an n×m radiating elements 1205. In the case that either n or m is set to 1, the resulting array is a linear array. As with the linear array, the radiating elements may be of any shape designed so as to provide the required performance. The array of FIG. 12A may be used for polarized radiation and may also be fed from two orthogonal directions to provide a cross-polarization, as explained above. Also, by providing proper feeding, beam steering and the generation of multiple simultaneous beams can be enabled, as will be explained below.

The example of the rectangular cone array antenna 1200 shown in FIG. 12A is a based on the use of a cone element 1205 as the basic component of the array. The antenna 1200 is being excited by a plane wave source 1208, which may be formed as a slotted waveguide array, microstrip, or any other feed, and having a feed coupler 1295 (e.g. coaxial connector). In this example, a slotted waveguide array feed is used and the slots on the feed 1208 (not shown), are situated on the wider dimension of the waveguide 1210, thus exciting a vertical polarized plane wave. The wave then propagates into the cavity, where on the top surface 1230 of the cavity the cone elements 1205 are situated on a rectangular grid of designed fixed spacing along the X and Y dimensions. As with the linear array, the spacing is calculated to either provide a boresight radiation or tilted radiation. Each cone 1205 couple a portion of the energy of the propagating wave, and excite the upper aperture of the cone 1205, once the wave has reached all the cones in the array, each of the cones function as a source for the far field of the antenna. In the far field of the antenna, one gets a Pencil Beam radiation pattern, with a gain value that is proportional to the number of elements in the array, the spacing between them, and related to the amplitude and phase of their excitations. However, unlike the prior art, the wave energy is coupled to the array without the need to elaborate waveguide network. For example, in the prior art an array of 4×4 elements would require a waveguide network having 16 individual waveguides arranged in a manifold leading to the port. The feeding network is eliminating by coupling the wave energy directly from the cavity to the radiating elements.

FIG. 12B illustrates a two-dimensional array according to another embodiment of the invention configured for operation with two sources. FIG. 12C is a top view of the array illustrated in FIG. 12B. The waveguide base and radiating elements are the same as in FIG. 12A, except that two faces of the waveguide are provided with sources 1204 and 1206. In this particular example a novel pin radiation source with a reflector is shown, but other sources may be used. In this example, source 1204 radiates a wave having vertical polarization, as exemplified by arrows 1214. Upon coupling to the radiation elements 1205 the wave assumes a horizontal polarization in the Y direction, as exemplified by arrows 1218. On the other hand, source 1206 radiates a planar wave, which is also vertically polarized, however upon coupling to the radiating elements assumes a horizontal polarization in the X direction. Consequently, the antenna array of FIG. 12B can operate at two cross polarization radiations. Moreover, each source 1204 and 1206 may operate at different frequency.

Each of sources 1204 and 1206 is constructed of a pin source 1224 and 1226 and a curved reflector 1234 and 1236. The curve of the reflectors is designed to provide the required planar wave to propagate into the cavity of the waveguide. Focusing reflectors 1254 and 1256 are provided to focus the transmission from the pins 1204 and 1206 towards the curved reflectors 1234 and 1236.

The embodiments described above use a rectilinear waveguide base. However, as noted above, other shapes may be used. For example, according to a feature of the invention, a circular array antenna can be constructed using a circular waveguide base and radiating elements of any of the shapes disclosed herein. The circular array antenna may also be characterized as a “flat reflector antenna.” To date, high antenna efficiency has not been provided in a 2-D structure. High efficiencies can presently only be achieved in offset reflector antennas (which are 3-D structures). The 3-D structures are bulky and also only provide limited beam scanning capabilities. Other technologies such as phased arrays or 2-D mechanical scanning antennas are typically large and expensive, and have low reliability.

The circular array antenna described herein provides a low-cost, easily manufactured antenna, which enables built-in scanning capabilities over a wide range of scanning angles. Accordingly, a circular cavity waveguide antenna is provided having high aperture efficiency by enabling propagation of electromagnetic energy through air within the antenna elements (the cross sections of which can be cones, crosses, rectangles, other polygons, etc.). The elements are situated and arranged on the constant phase curves of the propagating wave. In the case of a cylindrical cavity reflector, the elements are arranged on pseudo arcs. By controlling the cavity back wall cross-section function (parabolic shape or other), the curves can transform to straight lines, thus providing the realization of a rectangular grid arrangement. The structure may be fed by a cylindrical pin (e.g., monopole type) source that generates a cylindrical wave. For one example the cones couple the energy at each point along the constant phase curves, and by carefully controlling the cone radii and height, one can control the amount of energy coupled, changing both the phase and amplitude of the field at the aperture of the cone. Similar mechanism can be applied to any shape of element.

FIG. 13 illustrates and example of a circular array antenna 1300 according to an embodiment of the invention. As shown, the base of the antenna is a circularly-shaped waveguide 1310. A plurality of radiating elements 1305 are arranged on top of the waveguide. In this example, the cone-shaped radiating elements are used, but other shapes may also be used, including the circular-polarization inducing elements. The radiating elements 1305 are arranged in arcs about a central axis. The shape of the arcs depends on the feed and the desired characteristics of radiation. In this embodiment the antenna is fed by an omni-directional feed, in this case a single metallic pin 1395 placed at the edge of the plate, which is energize by a coaxial cable 1390, e.g. a 50′Ω coaxial line. This feed generates a cylindrical wave that propagates inside the cavity. The radiating elements 1305 are arranged along fixed-phase arcs so as to couple the energy of the wave and radiate it to the air. Since the wave in the waveguide propagates in free space and is coupled directly to the radiating elements, there is very little insertion loss. Also, since the wave is confined to the circular cavity, most of the energy can be used for radiation if the elements are carefully placed. This enables high gain and high efficiency of the antenna well in excess of that achieved by other flat antenna embodiments and offset reflector antennas.

FIG. 14 is a top view of another embodiment of a circular array antenna 1400 of the invention. This embodiment also uses a circular waveguide 1410, but the radiating elements 1405 are arranged in different shape arcs, which are symmetrical about the central axis. The feed may also be in the form of a pin 1495 provided at the edge of the axis, defining the boresight.

According to a feature of the invention, the various array antennas can enable beam scanning. For example, in order to scan the beam of a circular waveguide the source can be placed in different angular locations along the circumference of the circular cavity, thus creating a phase distribution along previously constant phase curves. At each curve there will be a linear phase distribution in both the X and Y directions, which in turn will tilt the beam in the Theta and Phi directions. This achieves an efficient thin, low-cost, built-in scanning antenna array. Arranging a set of feeds located on an arc enables a multi-beam antenna configuration, which simplifies beam scanning without the need for typical phase shifters.

Some advantages of this aspect of the invention may include, without limitation: (1) a 2-D structure which is flat and thin; (2) extremely low cost and low mechanical tolerances fit for mass production; (3) built-in reflector and feed arrangement, which enables wide-beam scanning without the need for expensive phase shifters or complicated feeding networks; (4) scalable to any frequency; (5) can work in multi-frequency operation such as two-way or one-way applications; (6) can accommodate high-power applications. Some associated applications may include, without limitation: (1) one-way DBS mobile or fixed antenna system; (2) two-way mobile IP antenna system (3) mobile, fixed, and/or military SATCOM applications; (4) point-to-point or point-to-multipoint high frequency (up to approximately 100 GHz) band systems; (5) antennas for cellular base stations; (6) radar systems.

FIG. 15 illustrates a process of designing an array according to an embodiment of the invention. In step 1500 the parameters desired gain, G, efficiency, ζ, and frequency, f₀, are provided as input into the gain equation to obtain the required effective area Aeff. Then in steps 1510 and 1520 the desired static tilt angles (θ₀x, θ₀y) of the beam along y and x direction are provide as input, so as to determine the spacing of the elements along the x and y directions (see description relating to FIG. 10). By introducing static tilt in x and y direction, the beam can be statically tilted to any direction in (r,θ) space. Using the area and the spacing, one obtains the number of elements (Nx, Ny) in the x and y directions in step 1530. Then, at Step 1535 if the radiating element chosen is circular, the lower radius is determined at Step 1540, i.e., the radius of the coupling aperture, and using the height determined at Step 1545 (e.g., 0.3λ) the upper radius, i.e., the radiating aperture, is generated at Step 1550. On the other hand, if at Step 1535 a polygon cross section is selected, at steps 1555 and 1560 the lower width and length of the element, i.e., the area of the coupling aperture, are determined. Then the height is selected based on the wavelength at step 1565. If flare is desired, the upper width and length may be tuned to obtain the proper characteristics as desired.

According to a method of construction of the antennas and arrays of the various embodiments described herein, a rectangular metal waveguide is used as the base for the antenna. The radiating element(s) may be formed by extrusion on a side of the waveguide. Each radiating element may be open at its top to provide the radiating aperture and at the bottom to provide the coupling aperture, while the sides of the element comprise metal extruded from the waveguide. Energy traveling within the waveguide is radiated through the element and outwardly from the element through the open top of the element. This method of manufacture is simple compared with other antennas and the size and shape of the element(s) can be controlled to achieve the desired antenna characteristics such as gain, polarization, and radiation pattern requirements.

According to another method, the entire waveguide-radiating element(s) structure is made of plastic using any conventional plastic fabrication technique, and is then coated with metal. In this way a simple manufacturing technique provides an inexpensive and light antenna.

An advantage of the array design is the relatively high efficiency (up to about 80-90% efficiency in certain situations) of the resulting antenna. The waves propagate through free space and the extruded elements do not require great precision in the manufacturing process. Thus the antenna costs are relatively low. Unlike prior art structures, the radiating elements of the subject invention need not be resonant thus their dimensions and tolerances may be relaxed. Also, the open waveguide elements allow for wide bandwidth and the antenna may be adapted to a wide range of frequencies. The resulting antenna may be particularly well-suited for high-frequency operation. Further, the resulting antenna has the capability for an end-fire design, thus enabling a very efficient performance for low-elevation beam peaks.

A number of wave sources may be incorporated into any of the embodiments of the inventive antenna. For example, a linear phased array micro-strip antenna may be incorporated. In this manner, the phase of the planar wave exciting the radiating array can be controlled, and thus the main beam orientation of the antenna may be changed accordingly. In another example, a linear passive switched Butler matrix array antenna may be incorporated. In this manner, a passive linear phased array may be constructed using Butler matrix technology. The different beams may be generated by switching between different inputs to the Butler matrix. In another example a planar waveguide reflector antenna may be used. This feed may have multi-feed points arranged about the focal point of the planar reflector to control the beam scan of the antenna. The multi-feed points can be arranged to correspond to the satellites selected for reception in a stationary or mobile DBS system. According to this example, the reflector may have a parabolic curve design to provide a cavity confined structure. In each of these cases, one-dimensional beam steering is achieved (e.g., elevation) while the other dimension (e.g., azimuth beam steering) is realized by rotation of the antenna, if required.

Turning to RF feeds or sources, the subject invention provides advantageous feed mechanisms that may be used in conjunction with the various inventive radiating elements described herein, or in conjunction with a conventional antenna using, e.g., micro-strip array, slotted cavity, or any other conventional radiating elements. Since the type of radiating elements used in conjunction with the innovative feed mechanism is not material, the radiating elements will not be explicitly illustrated in some of the figures relating to the feed mechanism, but rather “x” marks will be used instead to illustrate their presence.

FIG. 16 illustrates an embodiment of an RF feed according to an embodiment of the invention. In FIG. 16 a two dimensional array antenna 1600 is bounded at sides 1620, 1625, and 1630, to define cavity 1660, which receives radiation from side 1635. Antenna 1600 has a plurality of radiating elements 1605, the location of each of which is generally indicates by “x”, which may be of any conventional type, or of any of the inventive radiating elements described herein. The embodiment of FIG. 16 illustrates a single point feed arrangement, so it has a single radiating source and a single beam. In this example, radiation pin 1615 is provided in the area between open (feed) side 1635 and reflector 1610. The radiating pin 1615 radiates energy so as to generate a planar wave front at the entry face 1635 to the cavity 1660, propagating in a direction and with phase and amplitude distribution that is according to the design of the reflector 1610 and the location of the pin. When the pin is situated along the axis of symmetry, AS, the radiation direction is boresight, as shown in FIG. 16. If the pin is moved to the left along arrow L, the beam would tilt to the right and, conversely, if the pin is moved to the right the beam would tilt to the left. That is, beam tilt may be controlled by the location of the radiating pin. Thus, for example, by mechanically moving the radiating pin, one can control the beam tilt.

The reflector 1610 is made of an RF reflective material, such as metal or plastic coated with metallic layer, and is designed as a function f(x,y) so as to generate the desired beam shape, i.e., aperture, which includes amplitude and phase. FIG. 16A illustrate a reflector that may follow a parabolic or cylindrical function, while FIG. 16B illustrates a reflector that follows a 3-dimensional, toroidal shape. Additionally, in FIG. 16 an optional counter reflector 1640 is used so as to have the radiation from the pin reflected back towards the reflector 1610, generating a focusing effect. While the counter reflector is not necessary, it provides an improved performance.

In FIG. 16, the reflector 1610 is shown extending from one side of the antenna. However, in order to reduce the “footprint” of the antenna, the feeding-reflector arrangement may be “folded” under the antenna. An example is illustrated in FIGS. 16C and 16D. FIG. 16C illustrate a perspective view from under the antenna, showing the folded feed-reflector arrangement, while FIG. 16D illustrate a cross-section along line A-A of FIG. 16C. In FIGS. 16C and 16D, the feed coupler, e.g., a coaxial connector 1645, is provided from the bottom of the antenna to deliver/collect RF power to/from the radiating pin 1615 to the transmission line, e.g., coaxial cable 1644. This arrangement provides the same radiation characteristics as that of FIG. 16, except that the total area of the device is reduced.

FIG. 16E illustrates an embodiment of the innovative reflector feed used in conjunction with a patch array. In FIG. 16E the RF cavity 1660 is similar to that of FIG. 16, and similarly has end wall 1630 opposite the curved reflector 1610. A radiation source, such as radiating pin 1615 is coupled to a transmission line, e.g., coaxial cable, 1644 via coupler 1645. The top part of the cavity 1660 is covered with an insulator 1680. Conductive patches 1605 are provided on top of the insulator 1680, serving as radiating elements. Energy from the cavity 1660 is coupled to the radiating patches via conductive pins 1607 extending from each patch into the cavity 1660.

FIG. 17 illustrate an embodiment of an RF feed that is similar to that of FIG. 16, except that multiple RF radiation pins 1715 are used. The absolute location of each pin determines the beam tilt generated by radiation from that pin. Thus for each pin location there is a distinct beam location in space. In the rectangular grid embodiment of FIG. 17, each pin location will scan the beam in a plane that is parallel to the axis upon which the pins are arranged. Therefore, if the pins are energized serially, one obtains a beam scan in the direction between sides 1720 and 1725. On the other hand, one may energize all of the pins simultaneously, resulting in the following. If the amplitude and phase distribution is equal to all pins, multiple beams are radiated, with lower gain on each beam since the energy is split among the pins. Consequently, the radiation pattern will look like a set of hills and valleys, with gain at the peaks equal to the gain of one beam less 10 log (number of pins excited). According to another embodiment, one main beam pin is used in conjunction with two or more very close side pins, so as to shape the main beam. This is termed beam shaping. In one embodiment the energy to the adjacent beams is weighted, thereby improving the beam slop and thus improving interference satellite rejection or any other needed rejection, or shape the beam to a desired shape. In yet a further embodiment, one or more pins are fed at any given time, each pin corresponding to one beam tilted at a designed angle so as to point to a particular location in the sky, i.e., each pin corresponding to one satellite in the sky.

FIG. 18 illustrate an embodiment having dual-feed arrangement. In FIG. 18 two reflectors 1810 and 1820 are used to provide dual polarization radiation into the cavity of array elements 1805. The resulting beam is therefore scanned along the diagonal D as illustrated. When one side is fed horizontal polarization and the other vertical polarization, one may generate circularly polarized radiation.

FIG. 19 illustrates the principle of beam tilt/scanning over the diagonal of a symmetrical array 1900. In this example, radiating pin 1915 generates a plane wave 1917 of horizontal polarization, which propagates into the array as shown by arrow H. Radiating pin 1955 generates a plane wave 1957 of vertical polarization, which propagates into the array as shown by arrow V. To generate circular polarization, a 90 degrees phase is introduce between the horizontal and vertical polarized waves. This is done prior to feeding the pins 1915 and 1955 by, for example, using a hybrid or other electrical element illustrated generically as D. In this manner, the wave fronts arriving from the directions H and V at any element of the diagonal traverse the same distance d_v=d_H, and are therefore summed up over the diagonal V+H. Similarly, wave fronts arriving at elements that are placed symmetrically about the diagonal are also summed up due to the symmetry. For example, the distance traveled by wavefront V to element 1980 is d_v, while for wavefront H the distance is 2d_H. Similarly, the distance traveled by wave front V to element 1985 is 2d_v, while for wavefront H the distance is d_H. Now, since d_v=d_H, the radiation from these two elements would sum up. Note that for proper operation of this embodiment, the radiating elements should have a symmetrical geometry, e.g., circular or square, and their distribution over the array should be symmetrical about the diagonal.

FIGS. 20A and 20B illustrate an embodiment wherein the inventive reflector feed is utilized for an array operating in two frequencies of different bands. Notably, this array can simultaneously operate at two frequencies that are vastly different, for example one at Ka band, while another at Ku band. In this embodiment, radiating elements 2005 are optimized to operate at one frequency, e.g., at Ka band, while radiating elements 2003 are optimized to operate at the other frequency, e.g., at Ku band. The radiating elements 2005 form one array that is symmetrical about diagonal D, and the radiating elements 2003 form a second array also symmetrical about diagonal D. The radiating elements 2005 are fed from reflector feeds 2010 and 2012, while radiating elements 2003 are fed from reflector feed 2014 and 2016. It should be appreciated that in the cross-section image of FIG. 20B the reflector feeds are folded, while in the top elevation of FIG. 20A the reflectors are not folded.

FIG. 20C is a basic cross section of the unit cell of the mixed array concept, according to an embodiment of the invention. In forming the array according to this embodiment, the higher band elements 2005 are designed first, so as to have the ability to couple the high band energy propagating inside the waveguide structure 2060. The lower diameter of elements 2005 presents frequency cutoff conditions, basically filtering the low frequency energy that propagates inside cavity 2060 without interruption or coupling to elements 2005. At the other section of the array, where the low band cones 2003 are situated, the low band elements can couple and support both the high and low frequency bands, and couple the energy for both bands, thus enabling the use of the whole area for the higher band, and the use of only the lower frequency array for the lower band.

In the design of the embodiment of FIG. 20C, the height h_HB of the cavity 2060 at the area where the high band elements are provided is designed for the frequency at the high band, while the height h_LB of the cavity 2060 is higher and designed according to the frequency of the low band. Also, the distance between elements, dx_HB is designed to be equal or lower than the high band wavelength λg_HB, while the length dx_LB is designed to be equal or lower than the low band wavelength λg_LB, wherein λg corresponds to the wavelength λ₀ as transformed in the cavity 2060. The diameter d_r, of the opening of the high band cones 2005 are designed to present a short for the wavelength of the low band, thereby operating as a cutoff or filter.

Using the design of FIG. 20C, both high band array and low band array are square arrays that can produce a standard radiation pattern. The low frequency band gain and radiation patterns are governed only by the low frequency band array, but the high band gain and radiation pattern and frequency beam scanning is governed by both the high band and low band arrays and is weighted by controlling the spacing and cone size on both the high and low band arrays. In fact by doing so we mitigate the frequency scanning effects on the high band.

In addition, the feeds can be either situated along all four faces of the array, or situated just as two feeds, and the low and high Band collection points can be located at the same side of the array or spread between a four feed arrangements. FIGS. 20D and 20E illustrate variations for the reflector feeds for the mixed array concept. In FIG. 20D the feed for both the high band and low band is done from the same side, i.e., reflector feed 2010 is used for both high and low bands for one polarization, while reflector feed 2012 is used for both high and low bands for the other polarization. On the other hand, FIG. 20E illustrate symmetrical reflector feeding arrangement, wherein the same size reflector feeds are provided about all four corners of the array.

As discussed to above, the location of the RF source with respect to the reflector determines the tilt of the beam. Therefore, one may use different sources at different locations to have beams tilted at different angles. For example, in FIG. 20D five sources, here in the form of pins, are used so have the array point to five different satellites. The sources and the distances between them are designed so that, in this example, the array may be used for digital television transmission using SAT 99, SAT 101 (at boresight), SAT 103, SAT 110, and SAT 119.

FIG. 20 F illustrates a flow chart for the design of a mixed array antenna. At first the radiating elements for the high and low bands are designed according to the design embodiment described above. Then the spacing of the high and low band elements are determined so as to provide maximum efficiency. This follow by fine-tuning the high band and low band array spacing and element dimensions in order to weight and control radiation pattern and gain on both bands. In one embodiment, the fine-tuning is done in favor of the high band. While accepting the resulting gain and performance of the low band. The high band radiation pattern is a superposition of the pattern generated by the high band array and the low band array. The low band array generates a grating lobe pattern in the high band, that is summed up with the pattern generated by the high band array and helps reduce the frequency scanning effect. The design and layout is then finalized by providing the reflector or other type of RF feed.

FIGS. 21A and 21B illustrate another embodiment of the invention enabling simultaneous dual polarization with wide-angle reception in one direction with a very short but wide form factor which presents a small form factor for the human eye. The antenna of FIGS. 21A and 21B is beneficial in that it can be easily attached inconspicuously and need not be aimed precisely. The antenna of FIGS. 21A and 21B may beneficially utilize circularly polarizing elements such as, for example, the one illustrated in FIG. 8C, in conjunction with the inventive reflector feed. In this example, two long antennas 2100 and 2101 are made abutting each other. Antenna 2100 utilizes elements 2105 which provide, e.g., right hand circular polarization (RHCP), while antenna 2101 utilizes elements 2103 which provide counter circular polarization, i.e., left hand circular polarization (LHCP). Antenna 2100 utilizes reflector feed 2110 with radiating pin 2117, while antenna 2101 utilizes reflector feed 2112 with radiating pin 2115. Notably, in FIG. 21A the reflector feed is shown extending from the side of the antennas, while in FIG. 21B the reflector feed is folded.

It should be appreciated that any of the embodiments of the reflector feed described herein may use a fixed radiating pin, a movable radiating pin, or multiple radiating pins. In fact, the radiation does not necessarily be a pin. FIG. 22 illustrates an example of a reflector feed using a horn as an RF source. For this example, the embodiment of FIG. 16E is utilized, but it should be readily apparent that any of the other embodiment may be used as well. The array is constructed using a cavity 2260 having an insulating layer 2280 provided on its top, and patch radiating elements 2205 are provided on top of the insulating layer. The cavity 2260 is fed by reflector feed 2210 having a horn 2215 as an RF radiating source. The horn 2215 is fed with an RF energy by RF source 2245 in a conventional manner.

FIG. 23 illustrates an example of a patch radiation source which may be used with the reflector feed of the invention. The path feed of FIG. 23 may be used in any reflector feed constructed according to the invention. The patch radiation source of FIG. 23 is constructed of an insulating substrate 2310 having a conductive patch 2305 provided on one face thereof. The path is fed by a conductive trace 2325. The patch radiation source is affixed to the antenna so that the conductive patch faces the reflector. In one embodiment, as shown in FIG. 23, a conductive layer 2320 is provided on the backside of the substrate 2310. This functions to prevent any radiation from the patch to propagate directly into the cavity. In essence the conductive layer 2320 functions similarly to the counter reflector of FIG. 16.

As can be understood, all of the above embodiments relate to an antenna that utilizes a parallel plate waveguide having a planar wave propagating therein and being coupled into radiating elements via openings in one of the parallel plates. However, as will be shown in the following embodiments, the structure can also be used as a feed for a conventional dish antenna. The embodiments shown below can relate to any dish antenna; however, some of these embodiments are particularly suitable for dish antennas which communicate in more than one frequency band. Example of such dish antenna can be the television dish, such as used by Dish Networks™ and DirectTV™.

An explanation of the operation of an antenna feed will now be provided in the case of a reception of a signal, but it should be apparent that the exact reverse operation occurs during transmission of a signal. When a received signal (of a particular frequency band) from the reflector dish is split between more than one feed elements (forming an array), then the antenna feed is often referred to as a split-feed array. In the subsequent description, the terms “Array” and “Split-Feed Array” are synonymous and used interchangeably.

FIG. 24 schematically illustrates an embodiment of the invention which utilizes the parallel-plate structure as a feeder for a dish antenna. As shown in FIG. 24, a dish reflector 2404 has a focal point 2406. A wave guide cavity antenna 2408 is positioned at the focal point 2406, so as to serve as a feeder to the dish. One or more supports 2412 may be provided to physically hold the feeder 2408 at the focal point 2406. It will be appreciated that the focal point of the dish reflector 2404 may vary; thus, the location of the feeder 2408 relative to the dish reflector 2404 may also vary. Accordingly, the coupling of the feeder 2408 to the dish reflector 2404 may also vary. For example, one support may be provided at the bottom of the dish 2404 to couple the feeder 2408 at a focal point 2406A (not shown) located at a point lower than the focal point 2406 shown in FIG. 24.

FIG. 25 illustrates a simplified form of the dish antenna according to an embodiment of the invention. A feed assembly 2510 is provided at the focal point of the reflector dish 2504. The feed assembly is basically formed of a parallel-plate cavity 2514 and a single radiating element 2512 provided over an opening in the top plate of cavity 2514. The structure of this feed assembly can be such as shown in FIG. 2 or FIGS. 8A, 8B and 8C. A coaxial cable 2516 is coupled to a pin radiator that extends into the parallel plate cavity 2514. The dish can be any conventional solid or wire dish.

FIGS. 26A and 26B illustrate exemplary antenna feeders that can be used with the reflector dish, especially in situations where communication is in two different frequency bands. For example, with the increasing bandwidth demand for satellite TV transmission, TV satellite broadcasting is expanding to the Ka band in addition to the Ku band. Therefore, there's a need for new design for dish antenna that is capable of receiving transmission at both frequencies in different satellite locations and also in the same satellite location generally referred to KaKu co-location. The current solution is to place two (or more) LNB's (low noise block converters), wherein each one is somewhat offset from the focus point of the dish, thereby operating in less than optimal conditions. That is, since each frequency requires its own LNB from reception, and since each LNB has a given physical size, it is impossible to position more than one LNB at the focal point of the dish. Therefore, at least one LNB must be positioned offset from the focal point of the dish. The embodiment of FIGS. 26A and 26B, on the other hand, enables reception at two bands, wherein transmission from both bands is collected at the focal point of the dish.

As shown in FIGS. 26A and 26B, the antenna feeder 2600 includes a first parallel-plate cavity 2604 having a first set of reflecting elements 2612A and 2612B, and a second parallel-plate cavity 2614 having a single reflecting element 2608. The entire assembly is positioned such that the geometrical center of element 2608 is at the focal point of the dish. The two elements 2612A and 2612B are coupled to the same transmission line and are positioned symmetrically about the geometrical center of element 2608, such that the phase center of their cumulative signal coincides with the geometrical center of the single element 2608, and thereby also coincides with the focal point of the dish. In FIGS. 26A and 26B, the middle reflecting element 2608 receives transmission in two orthogonal polarization, one collected by pin and transmission line 2607A and the other by 2607B. Similarly, the reflecting elements 2612A and 2612B receive transmission in two orthogonal polarization, one collected by pin and transmission line 2606A and the other by 2606B. For example, RHP signal received from both elements 2612A and 2612B are collected by pin and transmission line 2606A, while LHP signal received from both elements 2612A and 2612B are collected by pin and transmission line 2606B. In this sense, elements 2612A and 2612B together form a one by two elements array. There is no demand to be positioned only at the actual focal point of the dish, since the co-location of bands using the described method can be positioned in also other satellite locations off-boresight away from the focal point. However, in such application as well, the phase center of the combined reception of the two elements 2612A and 2612B coincide with the phase center of the reception of element 2608, so that they are said to be co-located. That is, while they are not co-located physically In space, their phase center is co-located.

FIG. 26C illustrates the transmission/reception cone of each of the feeders, and the resulting combined cone. That is, the transmission/reception cone C08 of element 2608 has its center conceding with the geometrical center of the element 2608. Curves C12A and C12B illustrate the transmission/reception cone of each of elements 2612A and 2612B, respectively. However, as can be appreciated, since both elements for an array, their transmission/reception is additive, such that the resulting transmission/reception cone is illustrated by curve C12C, having its phase center point coinciding with the center point of element 2608, which also coincides with the focal point of the reflector dish or other desired point on the focal plane of the dish (e.g., in case the beam is scanned or the satellite reception is off boresight of the dish). Consequently, the phase center of both element 2608 and the array of elements 2612A and 2612B coincide and can be placed at any reception point of reflection from the dish, e.g., at the focal point of the reflector dish, even though none of elements 2612A and 2612B is at focal point of the reflector dish.

As can be understood from the above, when feed elements 2612A and 2612B are arranged in a split-feed array, it is possible to locate the phase center point of the combined split-feed array elements, where the signal integrity and strength is optimum. Most effective signal reception/transmission occurs when the phase center point of the split-feed array coincides with the focal point of the reflector dish of the antenna. Note that, for a plurality of satellites sending signals to a common reflector dish, each satellite may have a unique “focal” point where signal strength is optimum, based on the directionality of the dish. A plurality of satellites located very close to each other can also be thought of having the same “focal” point. For examples, multiple satellites at WL 101 position may be thought of having the same “focal” point associated with a fixed position of the dish. Feed assemblies for different satellites may be arranged on a common housing, each feed assembly physically located at the respective optimal “focal” point corresponding to the satellite. In effect, multiple antennas may be integrated physically sharing the same reflector dish.

FIG. 27 illustrates an embodiment employing two 1×2 arrays to receive communication at two different bandwidths, while both arrays having their phase center at the focal point of the reflector dish. As shown in FIG. 25, elements 2712A and 2712B have larger dimensions than elements 2708A and 2708B, so that each array operates at a different frequency band. For example, one array may operate at Ku band, while the other at Ka band. Similarly to the arrangement of FIG. 26, reception from elements 2708A and 2708B are added such that the phase center of the combined reception is in the middle between the two elements, and reception from elements 2712A and 2712B are added such that the phase center of the combined reception is in the middle between the two elements, and the two arrays are positioned such that the middle of both coincides on the same axis. This assembly is positioned such that the middle coincides with the focal point of the dish reflector. In this way, while none of the elements are physically positioned at the focal point, the center of the reception cones of both arrays are at the focal point.

In the specific example of FIG. 27, elements 2708A and 2708B are shown as having retarder elements 2716, thereby circularly polarizing the wave energy. Consequently, one polarized reception from both elements, e.g., RHP reception, can be collected at one end of the parallel plate waveguide 2714 additively, while the other rotation, e.g., LHP, can be collected at the other end of the waveguide. Similarly, retarders are provided for elements 2712A and 2712B, such that two circularly polarized transmission can be received, one at each end of the parallel plate waveguide 2704. Therefore, this arrangement provides four independent feeders to the reflector dish, each having it's own coaxial cable connection. In this manner, the system can communicate with four different satellite signals concurrently and all reception is done at the focal point of the reflector dish.

Of course, in all the embodiments, the same size elements may be used, so that communication for all of the elements is in the same frequency band. Also, in the embodiments shown above, the receptors are pins that are coupled with co-axial cables; however, it will be appreciated that other receptors may be used.

FIG. 28 illustrates another feed assembly for a dish antenna. A parallel-plate waveguide 2800 supports radiating elements arranged in individual arrays that are designed to operate in different frequency bands. An array 2802 of 2×3 radiating elements 2804 are fed from two reflectors 2806a and 2806b. An array 2812 of 2×2 elements 2814 is fed from reflectors 2816a and 2816b. A 1×2 array of elements 2824 is fed by reflectors 2826a and 2826b; 1×2 array of elements 2834 is fed by reflectors 2836a and 2823b; and 1×2 array of elements 2844 is fed by reflectors 2846a and 2846b. As shown, the elements of arrays 2802, 2812 and 2834 are of one side, corresponding to one frequency band, while the elements of arrays 2824 and 2844 are of a different size, corresponding to a different frequency band. In this manner, each array can communicate with one satellite, while array 2814 is positioned at the focal center of the reflector dish. Also, if retarders, such as 2803, are provided for each element, then each element can communicate at two polarizations, thereby doubling the capacity of the array.

FIG. 29 illustrates yet another embodiment of a feed for a dish antenna. FIG. 29 shows the external view of an example antenna feed assembly 2900 mounted on a common housing 2920. Portions 2925, 2926 and 2927 are parts of the housing 2920 that provide structural support as well as provide coupling of feed elements with respective waveguides (not shown). Elements 2928 are co-axial connectors attached to the housing 1120. Though not described in detail here, various feed elements in the feed assembly 2900 have external structures (such as cylindrical or square apertures) to enhance signal collection, as shown in FIG. 29, and described in various embodiments above. In assembly 2900, feed element 2912 communicates with a frequency band Δf_i of a first satellite (for example, Ka band of a satellite at 99 WL position). Feed element 2913 communicates with a frequency band Δf₂ of a second satellite. The frequency band Δf₂ may be the same as the frequency band Δf₁, but coming from a different satellite (for example, Ka band of a satellite at 103 WL position). In that case, elements 2912 and 2913 may be physically of the same dimension, but are located at different positions optimized for the respective satellites. Each of feed elements 2912 and 2913 can be thought of forming respective 1×1 arrays.

Feed elements 2908a-b form a 2×1 split-feed array, collectively referred to as array 2908, communicating with a frequency band Δf₃ of a third satellite. Note that, the frequency band Δf₃ may be the same as any the frequency bands Δf_l or Δf₂, but coming from a different (third) satellite located at a different position. For example, array 2908 may be communicating with the Ku band of a satellite at WL 101 position. Feed element 2907 forms a 1×1 array communicating with a frequency band Δf₄ of the third satellite or another satellite located very close to the third satellite. Frequency band Δf₄ may be the same as any the frequency bands Δf_i, or Δf₂, but will be different from Δf₃. For example, if array 2908 is communicating with the Ku band of a WL 101 satellite, element 2907 will be communicating with the Ka band of the same WL 101 satellite or another WL 101 satellite. The physical center point of element 2907 is also the phase center point of element 2907. Effective phase center point of array 2908 is co-located with the phase center point of element 2907. The co-located phase center points of both array 2908 and element 2907 are at the focal point of the reflector dish optimized for the WL 101 satellite position.

FIG. 30A shows top schematic view of the feed elements and associated components of the Δf₃ and Δf₄ bands, as discussed with respect to FIG. 29. FIG. 30B shows top schematic view of the feed elements and associated components of the Δf₃ band only, as discussed with respect to FIG. 29, removing the components associated with the Δf₄ band. For the sake of clarity, feed elements for the Δf₁ and Δf₂ bands are removed from the views shown in FIGS. 30A and 30B. Feed element 3007 is coupled to waveguide 3004. Feed elements 3008a-b are coupled to arms 3014a-b of split waveguide 3014. Waveguides 3014 and 3004 are stacked vertically in z direction to reduce footprint, but are physically separated from each other. Arms 3014a-b of split waveguide 3014 are coupled to common waveguide portion 3015, which is coupled to feed pin 3016. Feed pins 3016 are coupled with co-axial cables to transmit received signals to a receiver unit (not shown).

The embodiments discussed above utilize a special combination of parallel plate and radiating element to form the feed to a dish antenna. However, other radiating elements can also be used to implement embodiments of the invention. For example, slotted waveguide or radiating patches can also be used. The following are some examples of embodiment that use other radiating elements to implement the invention.

In the example embodiments shown in FIGS. 31-33, micro-slot-type antenna feed assemblies are shown from top. The antenna feed assemblies are coupled to a reflector dish. The reflector dish receives signals from one or more satellites. The antenna feed assemblies collect the received signal from the reflector dish, and transmit the signal to a receiver (that may be a set-top box.)

The antenna feed assembly 3100 in FIG. 31 comprises a thin, conductive plate 3105 including two micro-slot split-feed arrays 3101f and 3102f. Any number of split-feed arrays can be used. Each split-feed array may include any number of feed elements. In the example shown in FIG. 31, the split-feed array 3101f is a 2×1 array and the split-feed array 3102f is a 2×2 array.

In FIG. 31, micro-slots 301a-b are the individual feed elements of split-feed array 301f. Each of micro-slots 301a-b has a dimension L1 corresponding to a first band of frequency from a particular satellite. The phase center of split-feed array 301f is at the point 301e. Similarly, micro-slots 302a-d are the individual feed elements of split-feed array 302f. Each of micro-slots 302a-d has a dimension L2 corresponding to a second band of frequency of the same satellite. The phase center of split-feed array 302f is at the point 302e. As the phase centers 301e and 302e both can not be located at the focal point of a reflector dish, signal integrity of at least one of the frequency bands may be compromised.

FIG. 32 shows a solution to this problem. In FIG. 32, the antenna feed assembly 3200 comprises a thin, conductive plate 3205 including two micro-slot split-feed arrays 401f and 402f. Slots 401a-b are the individual feed elements of split-feed array 401f. Each of micro-slots 401a-b has a dimension L1 corresponding to the first band of frequency. The phase center of split-feed array 401f is at the point 401e. Similarly, micro-slots 402a-d are the individual feed elements of split-feed array 402f. Each of micro-slots 402a-d has a dimension L2 corresponding to the second band of frequency. The phase center of split-feed array 402f is at the point 402e. As the phase centers 401e and 402e are co-located at the focal point of a reflector dish, signal integrity of both the frequency bands may be optimized. A separation D included in split-feed array 401f is large enough to physically accommodate split-feed array 402f. However, it is possible to have the effective array phase center points be co-located even if separation D is not large enough to physically accommodate split-feed array 402f, because it may not be necessary to physically position an array element at the phase center point.

Split-feed arrays can be two dimensional rectangular array, or a linear array, or even a single element. For example, FIG. 33 shows an antenna feed assembly 3300 having a conductive plate 3305, where array 402f is a 1×1 array, i.e. consisting of a single element 402a, whose phase center is at the common point 401e, 402e.

To illustrate the versatility of the inventive concept, the following embodiments utilize microstrip elements and arrays to form the feed to the dish antenna. The antenna feed assembly 3406 in FIG. 34 comprises a thin insulating plate 3405 including an array 601f. Array 601f may include any number of elements. In the example shown in FIG. 34, array 601f is a 2×2 array. Array elements 601a-d are conductive patches defined on the face of plate 605. Conductive microstrip lines 601g distribute signal to the patches. Plate 3405 may form a part of a cavity into which signal is fed. Array 601f has a phase center point at 601e.

FIG. 35 illustrates a dish reflector feed assembly 3507 where another array 701f is positioned on plate 3505 within array 601f. Phase center 701e of array 701f has the same x-y co-ordinate with phase center 601e of array 601f. But the z coordinate of the centers are different. There is a layer of dielectric electrically isolating microstrip 601g from microstrip 701g in the z direction. Array elements 601a-d may correspond to a first frequency band, while array elements 701a-d may correspond to a second frequency band.

FIG. 36 illustrates an embodiment wherein different arrays corresponding to different frequency bands do not have to comprise same type of feed elements. For example, in FIG. 36, array 301f may be a microstrip type array on a conductive plate 3605, while array 1008f may be an open parallel-plate waveguide type array as described in other embodiments, such as, e.g., FIG. 2 or FIGS. 8A, 8B and 8C, including conical radiating elements 1008a-b. Both arrays share a common phase center point 301e, 1001e. Conductive plate 3505 may constitute the top plate of the open waveguide.

Finally, it should be understood that processes and techniques described herein are not inherently related to any particular apparatus and may be implemented by any suitable combination of components. Further, various types of general purpose devices may be used in accordance with the teachings described herein. It may also prove advantageous to construct specialized apparatus to perform the method steps described herein. The present invention has been described in relation to particular examples, which are intended in all respects to be illustrative rather than restrictive. Those skilled in the art will appreciate that many different combinations of hardware, software, and firmware will be suitable for practicing the present invention. For example, the described software may be implemented in a wide variety of programming or scripting languages, such as Assembler, C/C++, perl, shell, PHP, Java, HFSS, CST, EEKO, etc.

It should be understood that processes and techniques described herein are not inherently related to any particular apparatus and may be implemented by any suitable combination of components. Further, various types of general purpose devices may be used in accordance with the teachings described herein. The present invention has been described in relation to particular examples, which are intended in all respects to be illustrative rather than restrictive. Those skilled in the art will appreciate that many different combinations will be suitable for practicing the present invention.

Moreover, other implementations of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. Various aspects and/or components of the described embodiments may be used singly or in any combination. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims.

It should also be noted that antenna radiation is a two-way process. Therefore, any description herein for transmitting radiation is equally applicable to reception of radiation and vice versa. Describing an embodiment with using only transmission or reception is done only for clarity, but the description is applicable to both transmission and reception. Additionally, while in the examples the arrays are shown symmetrically, this is not necessary. Other embodiments can be made having non-symmetrical arrays such as, for example, rectangular arrays.

Claims

1. An antenna comprising: a reflector dish defining a focal point; anda feed assembly at the focal point, the feed assembly comprising a parallel-plate waveguide cavity, wherein a top plate of the parallel-plate waveguide cavity has at least one opening and a radiating element disposed about each opening.

2. The antenna of claim 1, wherein the top plate has a plurality of openings and at least one radiating element is sized to couple energy at Ka frequency band and is provided about one of the openings, and at least one second radiating element is sized to couple energy at Ku frequency band and is provided about a second opening.

3. The antenna of claim 2, wherein the cavity comprises a first height at an area under the at least one radiating element and a second height at an area under the second radiating element.

4. The antenna of claim 3, wherein the first height is optimized for guiding wave energy at the first frequency band and the second height is optimized for guiding wave energy at the second frequency band.

5. The antenna of claim 1, wherein the radiating element is optimized for operation at a first frequency band; and further comprising a plurality of second radiating elements each optimized for operation at a second band of frequencies and provided on the top surface of the waveguide cavity and having a phase center coinciding with the focal point or any other desired point at the focal plane of the reflector.

6. The antenna of claim 1, further comprising retarders for configuring the radiating element to receive circularly polarized wave energy.

7. The antenna of claim 1, further comprising a second parallel-plate waveguide cavity, wherein a top plate of the second parallel-plate waveguide cavity has a plurality of openings and a plurality of radiating elements each disposed about one of the openings, wherein the phase center of the radiating elements coincides with the focal point.

8. An antenna comprising: a reflector dish;a first array of radiating elements configured to operate in a first frequency band, wherein the first array has a first phase center point;a second array of radiating elements configured to operate in a second frequency band, wherein the second array has a second phase center point coinciding with the first phase center point; and,wherein the phase center points of the first and second arrays are located at a focal point of the reflector dish or any other desired point aimed to receive a certain signal from a certain satellite angular location other than boresight reception.

9. The antenna of claim 8, wherein the radiating elements of the first array comprise one of slots, microstrips, patches, or conical sections coupled over an opening in a top plate of a parallel plate cavity.

10. The antenna of claim 8, wherein the second array comprises a single radiating element physically located at the center point of the phase center of the first array.

11. The antenna of claim 8, wherein a separation between two feed elements of the first array can physically accommodate one or more feed elements of the second array.

12. The antenna of claim 8, wherein the first array comprises one or more conical sections each coupled about an opening in a top plate of a first parallel plate cavity, and the second array comprises one or more conical sections each coupled about an opening in a top plate of a second parallel plate cavity, wherein the first parallel plate cavity and the second parallel plate cavity are parallel to each other.

13. The antenna of claim 12, wherein the first parallel plate cavity and the second parallel plate cavity are vertically stacked separate waveguides.

14. The antenna of claim 12, wherein the first parallel plate cavity and the second parallel plate cavity are horizontally stacked portions of a common waveguide.

15. An antenna comprising: a reflector dish defining a focal point; anda feed assembly at the focal point, the feed assembly comprising: a first parallel-plate waveguide cavity having a top surface with at least one opening thereon, and a first-size radiating element provided about the opening;a second parallel-plate waveguide cavity having a top surface with at least one opening thereon, and a second-size radiating element provided about the opening.

16. The antenna of claim 15, wherein the first-size element is optimized for operation at a first frequency band and the second-size element is optimized for operation at a second frequency band.

17. The antenna of claim 15, wherein the first parallel-plate waveguide cavity comprises a first height and the second parallel-plate waveguide cavity comprises a second height different from the first height.

18. The antenna of claim 15, wherein the at least one first radiating element is sized to couple energy at Ka frequency band, and each of the second radiating elements is sized to couple energy at Ku frequency band.

19. A feed assembly for a parabolic dish comprising: a parallel-plate waveguide locatable about the focal point of the parabolic dish, a top plate of the parallel-plate waveguide having an aperture thereon;a radiating element optimized for operation at a first frequency band and provided on the top plate about the aperture and structure to couple wave energy directly from the parallel-plate waveguide via the opening.

20. The feed assembly of claim 19, wherein the radiating element is sized to couple energy at Ka frequency band, and further comprising a second radiating element provided on the top plate about a second aperture and sized to couple energy at Ku frequency band or any other set of bands.

21. The feed assembly of claim 20, wherein the waveguide comprises a first height at an area under the radiating element and a second height at an area under the second radiating element.

22. The feed assembly of claim 21, wherein the first height is optimized for guiding wave energy at the first frequency band and the second height is optimized for guiding wave energy at the second frequency band.

23. The feed assembly of claim 19, further comprising at least one additional radiating element provided on the top plate about another aperture.

24. The feed assembly of claim 19, wherein the waveguide is configured to couple a planar wave onto the radiating element.