This disclosure relates in general to electromagnetic beamforming and in particular, by way of example but not limitation, to a folded parallel plate waveguide lens for electromagnetic beamforming.
So-called local area networks (LANs) have been proliferating to facilitate communication since the 1970s. Certain LANs (e.g., those operating in accordance with IEEE 802.3) have provided enhanced electronic communication through wired media for decades. Since the late 1990s, LANs have expanded into wireless media so that networks may be established without necessitating wire connections between or among various network elements. Such LANs may operate in accordance with IEEE 802.11 (e.g., 802.11(a), (b), (e), (g), etc.) or other wireless network standards.
Although standard LAN protocols, such as Ethernet, may operate at fairly high speeds with inexpensive connection hardware and may bring digital networking to almost any computer, wireless LANs can often achieve the same results more quickly, more easily, and/or at a lower cost. Furthermore, wireless LANs provide increased mobility, flexibility, and spontaneity when setting up a network for two or more devices.
In wireless communication (including wireless LANs), signals are sent from a transmitter to a receiver using electromagnetic waves that emanate from an antenna. These electromagnetic waves may be sent equally in all directions or focused in one or more desired directions. When the electromagnetic waves are focused in a desired direction, the pattern formed by the electromagnetic wave is termed a “beam” or “beam pattern.” Hence, the production and/or application of such electromagnetic beams are typically referred to as “beamforming.”
Beamforming may provide a number of benefits such as greater range and/or coverage per unit of transmitted power, improved resistance to interference, increased immunity to the deleterious effects of multipath transmission signals, and so forth. Beamforming can be achieved through a number of different approaches, including (i) using a finely tuned vector modulator to drive each antenna element to thereby arbitrarily form beam shapes, (ii) by implementing full adaptive beam forming, (iii) by connecting a transmit/receive signal processor to each port of a Butler matrix, and (iv) by connecting at least one transmit/receive signal processor to an electromagnetic lens.
Unfortunately, beamforming is typically constrained by the apparatus and schemes used to achieve it. For example, approaches (i) and (ii) are complex, costly, and/or power intensive. Approach (iii) has limited flexibility, and approach (iv) can be bulky and/or can introduce non-linearity into the electromagnetic signals. Other additional factors can adversely impact the applicability and usability of beamforming in wireless communication systems.
Accordingly, there is a need for apparatuses and/or schemes for improving the viability and versatility of wireless communication and beamforming options therefor.
In an exemplary apparatus implementation, an electromagnetic lens includes: an input section including multiple input probes and a curvilinear input reflector; an output section including multiple output probes and a curvilinear output reflector; and a coupling section including a coupling slot and a curvilinear coupling wall.
In another exemplary apparatus implementation, an electromagnetic lens includes: a first layer; a second layer adjacent to the first layer; the second layer including multiple input probes, a curvilinear input reflector, and a first curvilinear coupling wall; a third layer adjacent to the second layer, the third layer including a coupling slot; a fourth layer adjacent to the third layer; the fourth layer including multiple output probes, a curvilinear output reflector, and a second curvilinear coupling wall; and a fifth layer adjacent to the fourth layer.
Other method, system, apparatus (including electromagnetic lenses, access stations, etc.), media, arrangement, etc. implementations are described herein.
The same numbers are used throughout the drawings to reference like and/or corresponding aspects, features, and components.
In wireless communications environment 100, access station 102 is in wireless communication with remote clients 104(1), 104(2) . . . 104(n) via wireless communications or communication links 106(1), 106(2) . . . 106(n), respectively. Although not required, access station 102 is typically fixed, and remote clients 104 are typically mobile. Also, although three remote clients 104(1, 2 . . . n) are shown, access station 102 may be in wireless communication with many such remote clients 104.
With respect to a so-called Wi-Fi wireless communications system, for example, access station 102 and/or remote clients 104 may operate in accordance with any IEEE 802.11 or similar standard. With respect to a cellular system, for example, access station 102 and/or remote clients 104 may operate in accordance with any analog or digital standard, including but not limited to those using time division/demand multiple access (TDMA), code division multiple access (CDMA), spread spectrum, some combination thereof, or any other such technology.
Access station 102 may be, for example, a nexus point, a trunking radio, a base station, a Wi-Fi switch, an access point, some combination and/or derivative thereof, and so forth. Remote clients 104 may be, for example, a hand-held device, a desktop or laptop computer, an expansion card or similar that is coupled to a desktop or laptop computer, a personal digital assistant (PDA), a mobile phone, a vehicle having a wireless communication device, a tablet or hand/palm-sized computer, a portable inventory-related scanning device, any device capable of processing generally, some combination thereof, and so forth. Remote clients 104 may operate in accordance with any standardized and/or specialized technology that is compatible with the operation of access station 102.
In a described implementation, access station 102 includes wireless I/O unit 206. Wireless I/O unit 206 includes an antenna array 208, electromagnetic lens 210, and one or more signal processors 212. Signal processors 212 are capable of facilitating transmission and/or reception and may include radio frequency (RF) and/or base band (BB) parts (not separately shown) that interface (e.g., via processor interface(s)) with electromagnetic lens 210. For example, multiple BB parts may be connected to respective multiple RF parts with the RF parts being coupled (directly or indirectly) to electromagnetic lens 210. Electromagnetic lens 210 comprises a beamformer and is described further herein below. In addition to signal processors 212, electromagnetic lens 210 is coupled to antenna array 208.
From a transmission perspective, input nodes or probes (not explicitly shown in
Antenna array 208 is implemented as two or more antennas or antenna elements, and optionally as a phased array of antennas and/or as a so-called smart antenna. Wireless I/O unit 206 is capable of transmitting and/or receiving (i.e., transceiving) signals (e.g., wireless communication(s) 106 (of
In wireless communication, signals may be sent from a transmitter to a receiver using electromagnetic waves that emanate from one or more antennas as focused in one or more desired directions, which contrasts with omni-directional transmission. This focusing of the electromagnetic waves in a desired direction and over a desired sector or other spatial area results in one or more beams or beam patterns, such as communication beams 202.
The production, usage, and/or application of such electromagnetic beams is typically referred to as beamforming. Beamforming usually entails employing at least one of any of a number of active and passive beamformers, such as electromagnetic lens 210. General examples of such active and passive beamformers include a tuned vector modulator (multiplier), a Butler matrix, a Rotman or other lens, a canonical beamformer, a lumped-element beamformer is with static or variable inductors and capacitors, and so forth. Also, beams may generally be formed using full adaptive beamforming.
In a described implementation, an employed beamformer comprises electromagnetic lens 210. By using electromagnetic lens 210 along with antenna array 208, multiple communication beams 202(1), 202(2) . . . 202(m) may be produced by wireless I/O unit 206. Although three beams 202(1, 2, m) are illustrated with three antennas of antenna array 208, it should be understood that the multiple antennas of antenna array 208 work in conjunction with each other to produce the multiple beams 202(1, 2 . . . m), where “m” generally corresponds to the number of processor or beam ports on electromagnetic lens 210. An exemplary set of communication beam patterns is described below with reference to
Communication beams 202(1) . . . 202(6) spread out over a 90° arc. The narrowest two beams are communication beams 202(3) and 202(4), and the beams become wider as they spread symmetrically outward from a central axis. For example, beam 202(5) is wider than beam 202(4), and beam 202(6) is wider still than beam 202(5). In a specific exemplary implementation, beams 202(3) and 202(4) are approximately 12° wide (e.g., at the half-power beamwidth), beams 202(2) and 202(5) are approximately 14° wide, and beams 202(1) and 202(6) are approximately 18° wide.
The increasing widths of the beams 202(3-2-1) and 202(4-5-6) as they spread outward from the central axis are due to real-world effects of the interactions between and among the wireless signals as they emanate from antenna array 208 (e.g., assuming a linear antenna array in a described implementation). It should be understood that the set of communication beam patterns illustrated in
The top view of electromagnetic lens 210 includes access to at least one input probe 402. Specifically, “I” input probes 402 are illustrated as input probes 402(1), 402(2), 402(3) . . . 402(I). Although not explicitly illustrated in
The sectional view of exemplary electromagnetic lens 210 shows an input probe 402(i) and an output probe 404(o). Input probes 402 are coupled (directly or indirectly) to one or more signal processors, such as signal processors 212 (of
In the particular cross-section of electromagnetic lens 210 in
In a described implementation, electromagnetic lens 210 includes an input section 406, a coupling section 408, and an output section 410. Input section 406 is formed from an input plate of the first layer and a common plate of the third layer, and it includes an input reflector 412 of the second layer. Output section 410 is formed from an output plate of the fifth layer and the common plate of the third layer, and it includes an output reflector 416 of the fourth layer. Coupling section 408 is formed from the common plate of the third layer, and it includes at least one coupling wall 414. As shown, coupling section 408 includes an input coupling wall 414I of the second layer and an output coupling wall 414O of the fourth layer.
In operation, an electromagnetic signal is provided at input probe 402(i) from a signal processor 212. The electromagnetic signal or wave emanates from input probe 402(i) and is guided along input section 406 using two parallel plates (i.e., the input plate and the common plate of the first and third layers, respectively) in conjunction with input reflector 412. When the electromagnetic wave reaches coupling section 408 from input section 406, it is redirected through a slot (e.g., that is formed from the common plate of the third layer) to output section 410 via input and output coupling walls 414I and 414O. The electromagnetic wave is guided along output section 410 using two parallel plates (i.e., the common plate and the output plate of the third and fifth layers, respectively) in conjunction with output reflector 416. Output probe 404(o), along with other output probes 404, receives the electromagnetic wave and forwards it to antenna array 208.
The (i) locations of input/output probes 402/404 and/or the (ii) shapes and locations of reflectors 412 and 416 and of coupling wall 414 are configured so as to modify the phase of the electromagnetic wave as it propagates through electromagnetic lens 210. Moreover, electromagnetic lens 210 is adapted to shift the phase of the electromagnetic wave as it impacts output probes 404 as compared to the phase of the electromagnetic wave as it is launched from input probe(s) 402.
The phase shifting is accomplished while establishing (including maintaining) a linear phase front of the electromagnetic wave as it reaches output probes 404. Although shown using an air medium for electromagnetic signal propagation, electromagnetic lens 210 may alternatively include one or more dielectric materials. For example, input section 406 and/or output section 410 (and possibly coupling section 408) may be fully or partially implemented as and/or filled with a dielectric material. With a dielectric material, the overall size of electromagnetic lens 210 may be reduced, but the insertion loss concomitantly increases.
Reflectors 412 and 416 and coupling wall 414 may each be shaped as curvilinear sections, which may be convex or concave when curved. Curvilinear sections as described herein may be extrapolated curves (including those having multiple foci), linear sections, non-circular conics, and so forth. Non-circular conic sections include parabolic sections, hyperbolic sections, elliptical sections, and so forth. Specific exemplary curvilinear section implementations for reflectors 412, 414, and 416 are described further below.
In this exemplary implementation, input probes 402 are secured to common plate 506. Although not visible in
As illustrated, input reflector 412H is hyperbolic in shape, coupling wall 414P is parabolic in shape, and output reflector 416L is linear in shape. Specifically, input reflector 412H and (first or input) coupling wall 414P are formed from and/or established by input spacer 504, and output reflector 416L and (second or output) coupling wall 414P are formed from and/or established by output spacer 508.
In a described implementation, input plate 502, common plate 506, and output plate 510 are fabricated from 0.050-inch aluminum sheet stock. Input spacer 504 and output spacer 508 are fabricated from 0.125-inch aluminum sheet stock. As a general guideline, plates 502, 506, and 510 are sufficiently thick so as to prevent or at least limit penetration by an electromagnetic wave propagating therebetween. Spacers 504 and 508, on the other hand, are sufficiently thin (e.g., less than or equal to half the wavelength of the electromagnetic wave (λ/2)) so as to provide a waveguide that supports a transverse electromagnetic (TEM) mode of propagation.
In a described implementation, six input probes 402(1), 402(2), 402(3), 402(4), 402(5), and 402(6) are utilized. These six input probes 402(1 . . . 6) correspond to six communication beams 202(1 . . . 6) as established via antenna array 208, and they are coupled to between one and six different signal processors 212 (depending on the configuration/capabilities of signal processor(s) 212). To couple the six input probes 402(1 . . . 6) to signal processor(s) 212, the six input probes 402(1 . . . 6) are exposed through six orifices 602(1), 602(2), 602(3), 602(4), 602(5), and 602(6), respectively. To avoid electromagnetic signal interaction, the six input probes 402(1 . . . 6) are insulated from input plate 502 (e.g., with air or another non-conductor).
Input plate 502, input spacer 504, and common plate 506 (see
Coupling slot 702 may be one continuous gap or opening. However, coupling slot 702 is illustrated as including optional bridges 704. One or more bridges 704 serve to mechanically reinforce coupling slot 702 and therefore also common plate 506. Three bridges 704 are shown in
In a described implementation, eight output probes 404(1), 404(2), 404(3), 404(4), 404(5), 404(6), 404(7), and 404(8) are utilized. These eight output probes 404(1 . . . 8) correspond to eight antenna elements of antenna array 208, and they are coupled thereto. To couple the eight output probes 404(1 . . . 8) to antenna array 208, the eight output probes 404(1 . . . 8) are exposed through eight orifices 802(1), 802(2), 802(3), 802(4), 802(5), 802(6), 802(7), and 802(8), respectively. To avoid electromagnetic signal interaction, the eight output probes 404(1 . . . 8) are insulated from output plate 510 (e.g., with air or another non-conductor).
Output plate 510, output spacer 508, and common plate 506 (see
Input section 406A includes hyperbolic input reflector 412H and six input probes 402. Input probes 402 are located a quarter wavelength (λ/4) away from the tangent to the hyperbolic shape defined by input reflector 412H and lying along the normal to the tangent. The six input probes 402 are separated along this parabolic contour with spacing that is dependent on the geometric aspects of the hyperbolic shape of input reflector 412H and the parabolic shape defined by coupling wall 414P of coupling section 408A. The six input probes 402 are placed symmetrically about the axis of hyperbolic input reflector 412H. The number of input probes 402 may vary according to the desired number of communication beams 202 used for sector coverage.
As more clearly shown in
Common plate 506, at coupling section 408A, includes coupling slot 702 that mirrors the parabolic shape of coupling wall 414P. Thus, coupling slot 702 also has a parabolic shape in this implementation. Coupling slot 702 includes five bridges 704 for stability. Although three bridges 704 are shown in
Output section 410A includes eight output probes 404 and output reflector 416L, which has a linear shape. Output probes 404 are located a quarter wavelength (λ/4) from output reflector 416L. Output probes 404 are proximate to output reflector 416L as compared to (output) coupling wall 414P, and input probes 402 are proximate to input reflector 412H as compared to (input) coupling wall 414P. In this context, proximate implies that the input/output probes 402/404 are closer to one barrier (e.g., input/output reflectors 412H/416L) than another barrier (e.g., coupling wall 414P).
The parabolic shape of coupling wall 414P and coupling slot 702 is capable of collimating the electromagnetic wave so as to cause rays 902 to be parallel and to present a linear phase wave front 904. Specifically, exemplary rays 902-I(1), 902-I(2) . . . 902-I(n) in input section 406A are shown launching from a single input probe 402′. The distance that ray 902-I(n) traverses from the emanating input probe 402′ to coupling slot 702 is shorter than the distance that ray 902-I(2) traverses from the emanating input probe 402′ to coupling slot 702. Furthermore, the distance that ray 902-I(2) traverses from the emanating input probe 402′ to coupling slot 702 is shorter than the distance that ray 902-I(1) traverses from the emanating input probe 402′ to coupling slot 702.
As a result of the differing distances traversed by rays 902, ray 902-I(n) arrives at coupling slot 702 prior to when ray 902-I(2) arrives thereat, and ray 902-I(2) arrives at coupling slot 702 prior to when ray 902-I(1) arrives thereat. Consequently, ray 902-I(1) is time delayed with respect to ray 902-I(2), and ray 902-I(2) is time delayed with respect to ray 902-I(n). These time delays correspond to phase variations at coupling section 408A.
Coupling section 408A, via coupling slot 702 and parabolic coupling wall 414P, couples rays 902 from input section 406A to output section 410A. The parabolic shape of (input and output) coupling wall 414, along with coupling slot 702, causes the propagating rays 902-I from input section 406A to be collimated as they are coupled via coupling section 408A to output section 410A as rays 902-O. Hence, rays 902-O(1), 902-O(2) . . . 902-O(n) are parallel to each other. It should be understood that rays 902-O are likely not exactly parallel; however, rays 902-O are sufficiently parallel so as to create a substantially-linear phase relationship for wave front 904.
Wave front 904, and rays 902-O(1), 902-O(2) . . . 902-O(n) thereof, propagate toward and reach output probes 404 (possibly via linear output reflector 416L). Each ray 902-O has a different phase shift. Consequently, each output probe 404 receives a ray 902-O having a different phase shift. The signals output from output probes 404 can therefore already have appropriate phase shifts for forwarding to antenna array 208 to produce directional communication beams 202.
In order to minimize or eliminate additional phase adjustment after the output of electromagnetic lens 210, output rays 902-O of wave front 904 of the electromagnetic wave presents a linear phase relationship to output probes 404. This linear phase front establishes varying phase shifts for the electromagnetic signal, which emanated from input probe 402′, at output probes 404 using the folded parallel plate waveguide lens. The established varying phase shifts are appropriate for correct production of communication beams 202 by the antenna elements of antenna array 208.
This additional area does precipitate multi-bounce(s) and concomitant side-lobe degeneration, especially for those signals associated with input probes 402 that are closest to regions 1002. However, input section 406A′ represents one example of an alternative configuration for input section 406A (and thus output section 410A similarly). In other words, and by way of example only, the side walls of input section 406A (and output section 410A) are not necessarily parallel to the direction of propagation of the electromagnetic wave that is of primary interest. Other wall, angle, spacing, etc. alternatives may also be implemented.
At block 1102, an electromagnetic wave is emanated from an input probe. For example, an electromagnetic wave having rays 902-I may be launched from input probe 402′ within input section 406A. It should be understood that different electromagnetic wave signals may be (at least approximately) simultaneously launched from different input probes 402 and propagated through electromagnetic lens 210 for simultaneous reception at multiple output probes 404.
At block 1104, the electromagnetic wave is guided toward a coupler using a hyperbolic reflector. For example, parallel input and common plates 502 and 506 may guide rays 902-I toward coupling slot 702 of coupling section 408A using hyperbolic-shaped input reflector 412H.
At block 1106, the electromagnetic wave is collimated at the coupler using a parabolic wall. For example, rays 902-I may be collimated by parabolic-shaped coupling wall 414P of coupling section 408A such that rays 902 of the electromagnetic wave become substantially parallel to each other. Rays 902-I may also be directed/redirected from input section 406A to output section 410A as rays 902-O via coupling slot 702.
At block 1108, the electromagnetic wave is guided from the coupler toward multiple output probes. For example, parallel common and output plates 506 and 510 may guide rays 902-O from coupling slot 702 toward output probes 404 using coupling wall 414P.
At block 1110, the electromagnetic wave is collected at the multiple output probes using a linear reflector. For example, rays 902-O may be received at output probes 404 using linear-shaped output reflector 416L. It should be understood that at least a portion of the electromagnetic wave may be collected by output probes 404 before any reflection(s).
Each output probe receives the electromagnetic wave at a different time delay and therefore with a different phase shift. For example, the electromagnetic wave having a linear phase wave front 904 may impact output probes 404 at an angle (e.g., with a normal of wave front 904 that is not perpendicular to output reflector 416L or to a line on which output probes 404 lie) such that each output probe 404 receives an electromagnetic signal having a different time delay/phase shift.
The electromagnetic wave signals may thereafter be forwarded from electromagnetic lens 210 and/or directly provided to antenna array 208 for creation of communication beams 202. The above description with reference to
With particular reference to
With an implementation described above with reference to
More generally, input reflector 412 may comprise at least a portion of any non-circular conic. Non-circular conics include parabolas, hyperbolas, and ellipses. Although coupling wall 414 is concave to facilitate collimation, and output reflector 416 is linear as illustrated, the non-circular conics for input reflector 412 may be concave or convex.
In other implementation(s), input reflector 412, coupling wall 414, and output reflector 416 may comprise any curvilinear shape. A (convex or concave) curvilinear section as used herein may be a non-circular conic section, a linear section, or an extrapolated curve section with multiple foci or with a relationship thereto. In such an extrapolated curve implementation, input reflector 412 comprises a multi-foci extrapolated curve (MFEC), coupling wall 414 comprises a linear section, and output reflector 416 comprises a curve that is related to the MFEC such that a linear phase relationship for guided electromagnetic waves is established in the vicinity of (including at) output probes 404. An exemplary extrapolated curve implementation is described further below with reference to
The MFEC shape of input reflector 412MFEC may be designed/determined as follows. First, a number of so-called perfect foci are selected. For example, three, four, or five foci are selected for inclusion in the MFEC shape. Second, for each selected focus, a curve (e.g., a parabolic curve) is created to establish the selected focus. This is indicated as the foci zones along input reflector 412MFEC. Third, an overall curve is created by extrapolating between the foci zones. This is indicated as extrapolation zone(s) along input reflector 412MFEC. Fourth, input probes 402(1 . . . 6) are then placed in the vicinity of one or more of the selected foci and located approximately a quarter wavelength (λ/4) from the surface of input reflector 412MFEC.
The REC shape of output reflector 416REC is designed/determined in dependence upon the MFEC shape of input reflector 412MFEC. Specifically, the REC shape is adapted so that a linear phase front is presented for output probes 404 after the electromagnetic wave reflects from output reflector 416REC. A curvature that is capable of establishing a linear phase relationship for rays propagating toward output probes 404 may be ascertained, for example, by ray tracing analysis or by using an electromagnetic 3D modeler. An example of a suitable electromagnetic 3D modeler is the Ansoft High Frequency Structure Simulator (HFSS).
There is therefore a relationship between the MFEC shape of input reflector 412MFEC and the REC shape of output reflector 416REC. In other words, given that input probes 402 launch an electromagnetic wave and are located in the vicinity of at least one focus of the multiple foci of input reflector 412MFEC, the curvature of output reflector 416REC is adapted to cause a linear phase relationship at output probes 404 for the electromagnetic wave that has been coupled by coupling section 408B from input section 406B into output section 410B and directed toward output probes 404 as well as output reflector 416REC using coupling slot 702 and coupling wall 414L.
At block 1302, an electromagnetic wave is emanated from an input probe. For example, individual electromagnetic waves may be launched from individual respective input probes 402 of one or more of input probes 402(1 . . . 6) within input section 406B.
At block 1304, the electromagnetic wave is guided toward a coupler using an MFEC reflector. For example, parallel input and common plates 502 and 506 (see
At block 1306, the electromagnetic wave is redirected at the coupler using a linear wall and slot. For example, the individual electromagnetic wave may be redirected by linear-shaped coupling wall 414L (also of input spacer 504 of the second layer of electromagnetic lens 210) and linear-shaped coupling slot 702 of coupling section 408B such that the individual electromagnetic wave may be coupled from input section 406B to output section 410B.
At block 1308, the electromagnetic wave is guided from the coupler toward multiple output probes. For example, parallel common and output plates 506 and 510 of third and fifth layers of electromagnetic wave 210 may guide the individual electromagnetic wave from coupling slot 702 toward output probes 404 using coupling wall 414L of output spacer 508 of a fourth layer of electromagnetic lens 210.
At block 1310, the electromagnetic wave is collected at the multiple output probes using an REC reflector. For example, the individual electromagnetic wave may be received at output probes 404(1 . . . 8) using REC-shaped output reflector 416REC (also of output spacer 508 of the fourth layer of electromagnetic lens 210). Each output probe 404 receives the individual electromagnetic wave at a different time delay and therefore with a different phase shift.
The REC reflector is adapted with regard to the MFEC reflector so as to establish a linear phase relationship for the electromagnetic wave at the multiple output probes. For example, output reflector 416REC is adapted with regard to input reflector 412MFEC so as to establish a linear phase relationship for each of the individual electromagnetic waves, which were launched from respective individual input probes 402(1 . . . 6), at output probes 404(1 . . . 8). It should be noted that a phase relationship may be considered linear if it is sufficiently close to linear such that communication beams 202 of a desired quality (e.g., with respect to shape, length, width, power, etc.) are produced from an associated antenna array 208.
Portions of the diagrams of
Although methods, systems, apparatuses (including electromagnetic lenses, access stations, etc.), arrangements, schemes, approaches, and other implementations have been described in language specific to structural and functional features and/or flow diagrams, it is to be understood that the invention defined in the appended claims is not necessarily limited to the specific features or flow diagrams described. Rather, the specific features and flow diagrams are disclosed as exemplary forms of implementing the claimed invention.
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