Iris matched PCB to waveguide transition

BACKGROUND

Unless otherwise indicated herein, the materials described in this section are not prior art to the claims in this application and are not admitted to be prior art by inclusion in this section.

Radio detection and ranging (RADAR) systems can be used to actively estimate distances to environmental features by emitting radio signals and detecting returning reflected signals. Distances to radio-reflective features can be determined according to the time delay between transmission and reception. The radar system can emit a signal that varies in frequency over time, such as a signal with a time-varying frequency ramp, and then relate the difference in frequency between the emitted signal and the reflected signal to a range estimate. Some systems may also estimate relative motion of reflective objects based on Doppler frequency shifts in the received reflected signals. Directional antennas can be used for the transmission and/or reception of signals to associate each range estimate with a bearing. More generally, directional antennas can also be used to focus radiated energy on a given field of view of interest. Combining the measured distances and the directional information allows for the surrounding environment features to be mapped. The radar sensor can thus be used, for instance, by an autonomous vehicle control system to avoid obstacles indicated by the sensor information.

Some example automotive radar systems may be configured to operate at an electromagnetic wave frequency of 77 Giga-Hertz (GHz), which corresponds to millimeter (mm) electromagnetic wavelength (e.g., 3.9 mm for 77 GHz). These radar systems may use antennas that can focus the radiated energy into tight beams in order to enable the radar system to measure an environment with high accuracy, such as an environment around an autonomous vehicle. Such antennas may be compact (typically with rectangular form factors; e.g., 1.3 inches high by 2.5 inches wide), efficient (i.e., there should be little 77 GHz energy lost to heat in the antenna, or reflected back into the transmitter electronics), and inexpensive to manufacture.

SUMMARY

The present application discloses embodiments that relate to an electromagnetic apparatus. In one aspect, the present apparatus includes a circuit board configured to propagate an electromagnetic signal. The apparatus also includes a waveguide configured to propagate an electromagnetic signal. The apparatus further includes a coupling port configured to couple a signal between the circuit board and the waveguide, where the coupling port has dimensions based on a desired impedance of the port.

In another aspect, the present application describes a method. The method involves conducting electromagnetic energy by a circuit board. The method further includes radiating at least a portion of the electromagnetic energy by a radiating component of the circuit board. And, the method also includes coupling at least a portion of the radiated electromagnetic energy into a waveguide by a coupling port, where the coupling port is a passage between the waveguide and the circuit board and where the coupling port has dimensions based on a desired impedance of the port.

In yet another aspect, the present application describes another method. The method may include conducting electromagnetic energy by a waveguide. The method may also include coupling at least a portion of radiated electromagnetic energy from the waveguide by a coupling port as received electromagnetic energy, where the coupling port is a passage between the waveguide and a circuit board and wherein the coupling port has dimensions based on a desired impedance of the port. The method may further include coupling at least a portion of the received electromagnetic energy from the coupling port to a circuit board by a coupling component of the circuit board.

In still another aspect, a system is provided that includes means for conducting electromagnetic energy. The system further includes means for radiating at least a portion of the electromagnetic energy by a radiating means. And, the system also includes means for coupling at least a portion of the radiated electromagnetic energy into a guide means by a coupling means, where the coupling means is a passage between the guide means and the means for conducting electromagnetic energy and where the coupling means has dimensions based on a desired impedance of the coupling means.

In still another aspect, a system is provided that includes means for conducting electromagnetic energy by a guide means. The system may also include means for coupling at least a portion of the radiated electromagnetic energy from the guide means by a coupling means as received electromagnetic energy, where the coupling means is a passage between the guide means and a means for conducting electromagnetic energy and wherein the coupling means has dimensions based on a desired impedance of the coupling means. The method may further include means for coupling at least a portion of the received electromagnetic energy from the coupling means to the means for conducting electromagnetic energy by a coupling means.

The foregoing summary is illustrative only and is not intended to be in any way limiting. In addition to the illustrative aspects, embodiments, and features described above, further aspects, embodiments, and features will become apparent by reference to the figures and the following detailed description.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1A is a flowchart of an example method to couple electromagnetic energy into a guide.

FIG. 1B is a flowchart of an example method to couple electromagnetic energy from a guide.

FIG. 2A illustrates a first layer of an example antenna, in accordance with an example embodiment.

FIG. 2B illustrates a second layer of an example antenna, in accordance with an example embodiment.

FIG. 2C illustrates an assembled view of an example antenna, in accordance with an example embodiment

FIG. 2D illustrates an assembled view of an example antenna, in accordance with an example embodiment.

FIG. 2E illustrates conceptual waveguide channels formed inside an assembled example antenna, in accordance with an example embodiment.

FIG. 3A illustrates a network of wave-dividing channels of an example antenna, in accordance with an example embodiment.

FIG. 3B illustrates an alternate view of the network of wave-dividing channels of FIG. 3A, in accordance with an example embodiment.

FIG. 4A illustrates an example iris matched PCB to waveguide transition.

FIG. 4B illustrates top-down view of two PCB-mounted coupling structures, in accordance with an example embodiment.

FIG. 4C illustrates an example arrangement of PCB-mounted coupling structures, in accordance with an example embodiment.

DETAILED DESCRIPTION

In the following detailed description, reference is made to the accompanying figures, which form a part hereof. In the figures, similar symbols typically identify similar components, unless context dictates otherwise. The illustrative embodiments described in the detailed description, figures, and claims are not meant to be limiting. Other embodiments may be utilized, and other changes may be made, without departing from the scope of the subject matter presented herein. It will be readily understood that the aspects of the present disclosure, as generally described herein, and illustrated in the figures, can be arranged, substituted, combined, separated, and designed in a wide variety of different configurations, all of which are explicitly contemplated herein.

The following detailed description discloses an apparatus including an antenna for a radar system for an autonomous vehicle, for instance, and a method for operating such an antenna. In some examples, the antenna may be a “dual open-ended waveguide” (DOEWG) antenna. The term “DOEWG” can refer to a short section of a horizontal waveguide channel plus a vertical channel that splits into two parts, where each of the two parts of the vertical channel includes an output port configured to radiate at least a portion of electromagnetic waves that enter the antenna.

An example DOEWG antenna may comprise, for example, two metal layers (e.g., aluminum plates) that can be machined with computer numerical control (CNC), aligned properly, and joined together. The first metal layer may include a first half of an input waveguide channel, where the first half of the first waveguide channel includes an input port that may be configured to receive electromagnetic waves (e.g., 77 GHz millimeter waves) into the first waveguide channel. The first metal layer may also include a first half of a plurality of wave-dividing channels. The plurality of wave-dividing channels may comprise a network of channels that branch out from the input waveguide channel and that may be configured to receive the electromagnetic waves from the input waveguide channel, divide the electromagnetic waves into a plurality of portions of electromagnetic waves (i.e., power dividers), and propagate respective portions of electromagnetic waves to respective wave-radiating channels of a plurality of wave-radiating channels. The DOEWG may also include at least a printed circuit board (PCB) backplane configured to perform at least one of absorbing some electromagnetic radiation and injecting electromagnetic radiation into the waveguide.

Further, the first metal layer may include a first half of the plurality of wave-radiating channels, where respective wave-radiating channels may be configured to receive the respective portions of electromagnetic waves from the wave-dividing channels, and where first halves of the respective wave-radiating channels include at least one wave-directing member configured to propagate sub-portions of electromagnetic waves to another metal layer.

Moreover, the second metal layer may include second halves of the input waveguide channel, the plurality of wave-dividing channels, and the plurality of wave-radiating channels. The second halves of the respective wave-radiating channels may include at least one pair of output ports partially aligned with the at least one wave-directing member and configured to radiate the sub-portions of electromagnetic waves propagated from the at least one wave-directing member out of the second metal layer. More particularly, a combination of a given wave-directing member with a corresponding pair of output ports may take the form of (and may be referred to herein as) a DOEWG, as described above.

While in this particular example the antenna includes multiple wave-dividing channels and multiple wave-radiating channels, in other examples the antenna may include only a single channel configured to propagate all the electromagnetic waves received by the input port to one or more wave-radiating channels. For instance, all the electromagnetic waves may be radiated out of the second metal layer by a single DOEWG. Other examples are possible as well.

Furthermore, while in this particular example, as well as in other examples described herein, the antenna apparatus may be comprised of at least two metal layers, it should be understood that in still other examples, one or more of the channels described above may be formed into a single metal layer, or into more than two metal layers that make up the antenna. Still further, within examples herein, the concept of electromagnetic waves (or portions/sub-portions thereof) propagating from one layer of a DOEWG antenna to another layer is described for the purpose of illustrating functions of certain components of the antenna, such as the wave-directing members. In reality, electromagnetic waves may not be confined to any particular “half” of a channel during certain points of their propagation through the antenna. Rather, at these certain points, the electromagnetic waves may propagate freely through both halves of a given channel when the halves are combined to form the given channel.

In some embodiments discussed herein, the two metal layers may be joined directly, without the use of adhesives, dielectrics, or other materials, and without methods such as soldering, diffusion bonding, etc. that can be used to join two metal layers. For example, the two metal layers may be joined by making the two layers in physical contact without any further means of coupling the layers.

In some examples, the present disclosure includes toward a printed circuit board (PCB) backplane configured to absorb some electromagnetic radiation. The previously-discussed radiating waveguides may be configured to receive an electromagnetic signal at the radiating waveguide input, propagate the electromagnetic signal down a length of the radiating waveguide, and couple to at least a portion of the electromagnetic signal to at least one radiating element configured to radiate the coupled electromagnetic signal. However, a portion of the electromagnetic signal may not be radiated and may be either reflected or contained within the waveguide. This electromagnetic energy may produce undesired effects in the radar system. Therefore, to reduce the effects from electromagnetic energy that was not radiated, it may be desirable to absorb the non-radiated electromagnetic energy into a load. The waveguides may each be coupled to a coupling port (or termination/attenuation port) configured to absorb non-radiated electromagnetic energy that is present in the waveguide.

In one example, each of the beamforming network outputs may have a corresponding waveguide shunt, that is the end of the waveguide, located on the opposite end of the waveguide from the respective beamforming network output. Of the shunts, one may be coupled to the beamforming network input. The remaining shunts may each be coupled to a respective coupling port. In some examples, each shunt, including the shunt with the feed, may be coupled to a coupling port. The coupling port may be aligned perpendicular to the main length of the waveguide. Additionally, the coupling port may include a geometry to impedance match the waveguide to the attenuation component. For example, the coupling port may be a hole in a waveguide block coupling a circuit board layer to a waveguide layer.

In one example, the coupling port may couple a waveguide of the beamforming network to an attenuation component located on the PCB via a coupling port. In another example, the coupling port may couple a feed on the PCB to a waveguide of the beamforming network via a coupling port.

The attenuation component may include metallic traces on the PCB. The metallic traces may function to couple the non-radiated electromagnetic energy out of the waveguide into the PCB. Once the non-radiated electromagnetic energy has coupled to the traces, various different means may be used to absorb the non-radiated electromagnetic energy. In one example, the traces may be coupled to other components that may dissipate the non-radiated electromagnetic energy. In one example, the traces may be coated with an electrically lossy material that will absorb electrical current present on the surface of the traces when it couples to the non-radiated electromagnetic energy. In another example, the PCB may have microstrip lines configured to absorb the non-radiated electromagnetic energy. The microstrip lines may absorb the non-radiated electromagnetic energy based on the lines being made from an electromagnetically lossy material, such as Nickel Chrome. In another example, the PCB may be constructed from an electromagnetically lossy material.

In one example, at least a portion of the couplings port may function to couple electromagnetic energy to a component configured to absorb non-radiated electromagnetic energy. In a different example, each coupling port may function to route the non-radiated electromagnetic energy to an attenuation component configured to absorb energy from more than one coupling port.

The antenna apparatus may include coupling port configured to function as a waveguide feed. The waveguide feed may be a coupling port in the metallic structure that enables an electromagnetic wave to enter the antenna apparatus. When the electromagnetic wave enters the antenna apparatus, it may be divided and radiated as previously discussed.

In yet further examples, the coupling port may function as a bidirectional port. It may both provide a feed signal to the waveguide and and remove non-radiated electromagnetic energy from the waveguide.

Each coupling port of the antenna apparatus may have an associated port impedance. The port impedance may affect the percentage of the electromagnetic energy that the port can couple into or out of the antenna apparatus. Therefore, it may be desirable to optimize the port impedance so energy can efficiently enter or leave the antenna apparatus. There may be several methods by which the port impedance may be optimized. In some examples, a port geometry may be altered in order to adjust the port impedance. For example, a coupling port may be located in a bottom block of the previously described split-block construction apparatus. The coupling port may be located in the bottom block between a waveguide and a circuit board. In order to achieve the desired port impedance, the port may be machined from both a top side and bottom side of the bottom block. A more narrow waveguide portion may increase the waveguide inductance while a wider waveguide portion may increase the waveguide capacitance.

Referring now to the figures, FIG. 1A is a flowchart of an example method 100 to couple electromagnetic energy into a guide. And, FIG. 1B is a flowchart of an example method 110 to couple electromagnetic energy from a guide. It should be understood that other methods of operation not described herein are possible as well.

It should also be understood that a given application of such an antenna may determine appropriate dimensions and sizes for various machined portions of the two metal layers described above (e.g., channel size, metal layer thickness, etc.) and/or for other machined (or non-machined) portions/components of the antenna described herein. For instance, as discussed above, some example radar systems may be configured to operate at an electromagnetic wave frequency of 77 GHz, which corresponds to millimeter electromagnetic wave length. At this frequency, the channels, ports, etc. of an apparatus fabricated by way of method 100 and method 110 may be of given dimensions appropriated for the 77 GHz frequency. Other example antennas and antenna applications are possible as well.

Although the blocks are illustrated in a sequential order, these blocks may also be performed in parallel, and/or in a different order than those described herein. Also, the various blocks may be combined into fewer blocks, divided into additional blocks, and/or removed based upon the desired implementation.

Moreover, the method 100 of FIG. 1A and the method 110 of FIG. 1B may be implemented by the devices described in conjunction with FIGS. 2A-2E, 3A, 3B, and 4A-4C.

At block 102, the method 100 includes conducting electromagnetic energy (e.g., 77 GHz millimeter electromagnetic waves) by a circuit board. In various examples, the electromagnetic energy may propagate in at least one of several different modes depending on the various embodiments. In one example, the electromagnetic energy may propagate along a differential pair of lines on the circuit board. In another example, the electromagnetic energy may propagate along a single line on the circuit board. The electromagnetic energy may be a signal for transmission by an antenna and/or a radar unit. In various examples, different types of signaling may be used to form the electromagnetic energy. In practice, the method 100 may be a method performed during the transmission of radar signals.

At block 104, the method 100 includes radiating at least a portion of the electromagnetic energy by a radiating component of the circuit board. The circuit board may have at least one component that radiates electromagnetic energy. In some examples, this radiating component may be functionally similar to a circuit board mounted patch antenna. Various other types of components may be used to radiate electromagnetic energy from the circuit board as well. Various antennas, patches, slots, or other radiating components may be used within the context of the present disclosure as well. The radiating component may also function as a component that may receive electromagnetic energy from the coupling port (i.e. the component may function in a bidirectional manner).

The radiating component is configured to convert at least a portion of the electromagnetic energy propagating on the circuit board into radiated electromagnetic energy (i.e. electromagnetic energy that is not contained on trace of or within the circuit board).

At block 106, the method 100 includes coupling at least a portion of the radiated electromagnetic energy into a waveguide by a coupling port. The coupling port may be a passage between the waveguide and the circuit board. The passage allows electromagnetic energy from the circuit board to enter the waveguide. The coupling port may have dimensions based on a desired impedance of the port. The impedance of the port may, in part, contribute to the percentage of the electromagnetic energy from the circuit board that couples into the waveguide. Because the port impedance may affect the percentage of the electromagnetic energy that the the port can couple into or out of the antenna apparatus, it may be desirable to optimize the port impedance so energy can efficiently enter or leave the antenna apparatus. The optimizations of the port impedance may be controlled by adjusting the port dimensions.

In some examples, the circuit board may be coupled to the block that forms the antenna (i.e. radar) unit of the present system. For example, and as discussed with respect to the following figures, the system may be constructed in a block. The waveguide and associated beamforming network may be created on a plane of the block. In various examples, the circuit board may be mounted on the bottom of the bottom block and the coupling port may be through the bottom of the bottom block. In anther example, the circuit board may be mounted to a side of the block. In this example, the coupling port may be through the side of one of or both of the top block and bottom block.

Turning to FIG. 1B, at block 112, the method 110 includes conducting electromagnetic energy by a waveguide. The electromagnetic energy in the waveguide may have been received from outside of the system by at least one antenna of the waveguide. In practice, the method 110 may be a method performed during the reception of radar signals. The antenna(s) coupled to the waveguide may receive reflected electromagnetic energy and propagate the electromagnetic energy along the waveguide.

At block 114, the method 110 includes coupling at least a portion of the radiated electromagnetic energy from the waveguide by a coupling port as received electromagnetic energy. As previously discussed, the coupling port may be a passage between the waveguide and the circuit board. As part of method 110, the passage allows electromagnetic energy from the waveguide to leave the waveguide and couple to a component of the circuit board.

The coupling port of method 110 may function in a similar manner to the coupling port of method 100, but operating in the opposite direction (e.g. method 100 causes electromagnetic energy to enter the guide from the circuit board while method method 110 causes electromagnetic energy to leave the guide to the circuit board). Similar to method 100, the coupling port of method 110 may have dimensions based on a desired impedance of the port. The impedance of the port may, in part, contribute to the percentage of the electromagnetic energy from the circuit board that couples into the waveguide. Because the port impedance may affect the percentage of the electromagnetic energy that the the port can couple into or out of the antenna apparatus, it may be desirable to optimize the port impedance so energy can efficiently enter or leave the antenna apparatus. The optimizations of the port impedance may be controlled by adjusting the port dimensions.

At block 116, the method 110 includes coupling at least a portion of the received electromagnetic energy from the coupling port to a circuit board by a coupling component of the circuit board. The circuit board may have at least one component that receives electromagnetic energy. In some examples, this receiving component may be functionally similar to a circuit board mounted patch antenna. Various other types of components may be used to radiate electromagnetic energy from the circuit board as well. Various antennas, patches, slots, or other radiating components may be used within the context of the present disclosure as well. The receiving component may also function as a component that may radiate electromagnetic energy into the coupling port (i.e. the component may function in a bidirectional manner).

The receiving component is configured to convert at least a portion of the electromagnetic energy from the coupling port into the circuit board (i.e. cause electromagnetic energy to propagate along a trace or within the circuit board).

The arrangement of the components of FIGS. 2A-E are shown as example systems and arrangements in which the present disclosure may be used. Other shapes, alignments, positions, styles, and other arrangements of waveguides and antennas may be used with the PCB transition coupling port disclosed herein.

FIG. 2A illustrates an example first metal layer 200 including a first half of a plurality of waveguide channels 202. These waveguide channels 202 may comprise multiple elongated segments 204. At a first end 206 of each elongated segment 204 may be a plurality of collinear wave-directing members 208, each with sizes similar or different from other wave-directing members. In line with the description above, the first ends 206 of the elongated segments 204 may be referred to herein as a first half of wave-radiating channels.

At a second end 210 of the channels 202 opposite the first end 206, one of the elongated segments 204 may include a through-hole 212 (i.e., coupling port). A given amount of power may be used to feed a corresponding amount of electromagnetic waves (i.e., energy) into the apparatus, and the through-hole 212 may be the location where these waves are fed into the apparatus. In line with the description above, the single channel/segment of the waveguide channels 202 that includes the input port may be referred to herein as an input waveguide channel. Further, the second end 210 of the channels 202 may be coupled to attenuation components (not shown here), as discussed throughout this disclosure.

Upon entering the apparatus, the electromagnetic waves may generally travel in the +x direction, as shown, towards an array of power dividers 214 (i.e., a “beam-forming network”). The array 214 may function to divide up the electromagnetic waves and propagate respective portions of the waves to respective first ends 206 of each elongated segment 204. More specifically, the waves may continue to propagate in the +x direction after leaving the array 214 toward the wave-directing members 208. In line with the description above, the array 214 section of the waveguide channels may be referred to herein as wave-dividing channels.

As the portions of the electromagnetic waves reach the wave-directing members 208 at the first end 206 of each elongated segment 204 of the waveguide channels 202, the wave-directing members 208 may propagate through respective sub-portions of the electromagnetic energy to a second half of the waveguide channels (i.e., in the +z direction, as shown). For instance, the electromagnetic energy may first reach a wave-directing member that is recessed, or machined further into the first metal layer 200 (i.e., a pocket). That recessed member may be configured to propagate a smaller fraction of the electromagnetic energy than each of the subsequent members further down the first end 206, which may be protruding members rather than recessed members.

Further, each subsequent member may be configured to propagate a greater fraction of the electromagnetic waves travelling down that particular elongated segment 204 at the first end 206 than the member that came before it. As such, the member at the far end of the first end 206 may be configured to propagate the highest fraction of electromagnetic waves. Each wave-directing member 208 may take various shapes with various dimensions. In other examples, more than one member (or no members) may be recessed. Still other examples are possible as well. In addition, varying quantities of elongated segments are possible.

A second metal layer may contain a second half of the one or more waveguide channels, where respective portions of the second half of the one or more waveguide channels include an elongated segment substantially aligned with the elongated segment of the first half of the one or more waveguide channels and, at an end of the elongated segment, at least one pair of through-holes partially aligned with the at least one wave-directing member and configured to radiate electromagnetic waves propagated from the at least one wave-directing member out of the second metal layer.

Within examples, the elongated segment of the second half may be considered to substantially align with the elongated segment of the first half when the two segments are within a threshold distance, or when centers of the segments are within a threshold distance. For instance, if the centers of the two segments are within about ±0.051 mm of each other, the segment may be considered to be substantially aligned.

In another example, when the two halves are combined (i.e., when the two metal layers are joined together), edges of the segments may be considered to be substantially aligned if an edge of the first half of a segment and a corresponding edge of the second half of the segment are within about ±0.051 mm of each other.

In still other examples, when joining the two metal layers, one layer may be angled with respect to the other layer such that their sides are not flush with one another. In such other examples, the two metal layers, and thus the two halves of the segments, may be considered to be substantially aligned when this angle offset is less than about 0.5 degrees.

In some embodiments, the at least one pair of through-holes may be perpendicular to the elongated segments of the second half of the one or more waveguide channels. Further, respective pairs of the at least one pair of through-holes may include a first portion and a second portion. As such, a given pair of through-holes may meet at the first portion to form a single channel. That single channel may be configured to receive at least the portion of electromagnetic waves that was propagated by a corresponding wave-directing member and propagate at least a portion of electromagnetic waves to the second portion. Still further, the second portion may include two output ports configured as a doublet and may be configured to receive at least the portion of electromagnetic waves from the first portion of the pair of through-holes and propagate at least that portion of electromagnetic waves out of the two output ports.

FIG. 2B illustrates the second metal layer 220 described above. The second metal layer 220 may include a second half of the plurality of waveguide channels 202 of the first metal layer 200 shown in FIG. 2A (i.e., a second half of the input waveguide channel, the wave-dividing channels, and the wave-radiating channels). As shown, the second half of the waveguide channels 202 may take on the general form of the first half of the channels, so as to facilitate proper alignment of the two halves of the channels. The elongated segments of the second half 222 may include second halves of the array of power dividers 224. As described above, electromagnetic waves may travel through the array 224, where they are divided into portions, and the portions then travel (i.e., in the +x direction, as shown) to respective ends 226 of the second halves of the elongated segments 222.

Further, an end 226 of a given elongated segment may include multiple pairs of through-holes 228, which may be at least partially aligned with the wave-directing members 208 of the first metal layer 200. More specifically, each pair of through-holes may be at least partially aligned with a corresponding wave-directing member, also referred to as a reflecting element, such that when a given sub-portion of electromagnetic waves are propagated from the first metal layer 200 to the second metal layer 220, as described above, those sub-portions are then radiated out of the pair of through-holes (i.e., a pair of output ports) in the −z direction, as shown. Again, the combination of a given wave-directing member and a corresponding pair of output ports may form a DOEWG, as described above.

Moreover, a combination of all the DOEWGs may be referred to herein as a DOEWG array. In antenna theory, when an antenna has a larger radiating aperture (i.e., how much surface area of the antenna radiates, where the surface area includes the DOEWG array) that antenna may have higher gain (dB) and a narrower beam width. As such, in some embodiments, a higher-gain antenna may include more channels (i.e., elongated segments), with more DOEWGs per channel. While the example antenna illustrated in FIGS. 2A and 2B may be suitable for autonomous-vehicle purposes (e.g., six elongated segments, with five DOEWGs per segment), other embodiments may be possible as well, and such other embodiments may be designed/machined for various applications, including, but not limited to, automotive radar.

For instance, in such other embodiments, an antenna may include a minimum of a single DOEWG. With this arrangement, the output ports may radiate energy in all directions (i.e. low gain, wide beam width). Generally, an upper limit of segments/DOEWGs may be determined by a type of metal used for the first and second metal layers. For example, metal that has a high resistance may attenuate an electromagnetic wave as that wave travels down a waveguide channel. As such, when a larger, highly-resistive antenna is designed (e.g., more channels, more segments, more DOEWGs, etc.), energy that is injected into the antenna via the input port may be attenuated to an extent where not much energy is radiated out of the antenna. Therefore, in order to design a larger antenna, less resistive (and more conductive) metals may be used for the first and second metal layers. For instance, in embodiments described herein, at least one of the first and second metal layers may be aluminum. Further, in other embodiments, at least one of the first and second metal layers may be copper, silver, or another conductive material. Further, aluminum metal layers may be plated with copper, silver, or other low-resistance/high-conductivity materials to increase antenna performance. Other examples are possible as well.

The antenna may include at least one fastener configured to join the first metal layer to the second metal layer so as to align the first half of the one or more waveguide channels with the second half of the one or more waveguide channels to form the one or more waveguide channels (i.e., align the first half of the plurality of wave-dividing channels with the second half of the plurality of wave-dividing channels, and align the first half of the plurality of wave-radiating channels with the second half of the plurality of wave-radiating channels). To facilitate this in some embodiments, the first metal layer, a first plurality of through-holes (not shown in FIG. 2A) may be configured to house the at least one fastener. Additionally, in the second metal layer, a second plurality of through-holes (not shown in FIG. 2B) may be substantially aligned with the first plurality of through-holes and configured to house the at least one fastener for joining the second metal layer to the first metal layer. In such embodiments, the at least one fastener may be provided into the aligned first and second pluralities of through-holes and secured in a manner such that the two metal layers are joined together.

In some examples, the at least one fastener may be multiple fasteners. Mechanical fasteners (and technology used to facilitate fastening) such as screws and alignment pins may be used to join the two metal layers together. Further, in some examples, the two metal layers may be joined directly to each other, with no adhesive layer in between. Still further, the two metal layers may be joined together using methods different than adhesion, diffusion bonding, soldering, brazing, and the like. However, it is possible that, in other examples, such methods may be used in addition to or alternative to any methods for joining metal layers that are known or not yet known.

In some embodiments, one or more blind-holes may be formed into the first metal layer and/or into the second metal layer in addition to or alternative to the plurality of through-holes of the first and/or the second metal layer. In such embodiments, the one or more blind-holes may be used for fastening (e.g., housing screws or alignment pins) or may be used for other purposes.

FIG. 2C illustrates an assembled view of an example antenna 240. The example antenna 240 may include the first metal layer 200 and the second metal layer 220. The second metal layer 220 may include a plurality of holes 242 (through-holes and/or blind-holes) configured to house alignment pins, screws, and the like. The first metal layer 200 may include a plurality of holes as well (not shown) that are aligned with the holes 242 of the second metal layer 220.

Further, FIG. 2C illustrates a DOEWG array 244 of a given width 246 and a given length 248, which may vary based on the number of DOEWGs and channels of the antenna 240. For instance, in an example embodiment, the DOEWG array may have a width of about 11.43 mm and a length of about 28.24 mm. Further, in such an example embodiment, these dimensions, in addition to or alternative to other dimensions of the example antenna 240, may be machined with no less than about a 0.51 mm error, though in other embodiments, more or less of an error may be required. Other dimensions of the DOEWG array are possible as well. Further, in some examples, other shaped outputs may be used for the radiating elements. Although shown as ovals in FIG. 2C, the radiating elements can take any shape and the shape is not critical to the present disclosure. In some examples, the radiating elements may be square, circular, linear, z-shaped, etc.

In some embodiments, the first and second metal layers 200, 220 may be machined from aluminum plates (e.g., about 6.35 mm stock). In such embodiments, the first metal layer 200 may be at least 3 mm in thickness (e.g., about 5.84 mm to 6.86 mm). Further, the second metal layer 220 may be machined from a 6.35 mm stock to a thickness of about 3.886 mm. Other thicknesses are possible as well.

In some embodiments, the joining of the two metal layers 200, 220 may result in an air gap or other discontinuity between mating surfaces of the two layers. In such embodiments, this gap or continuity can be proximate to (or perhaps as close as possible to) a center of the length of the antenna apparatus and may have a size of about 0.05 mm or smaller.

FIG. 2D illustrates another assembled view of the example antenna 240. As shown, the first metal layer 200 may include a plurality of holes 250 (through-holes and/or blind-holes) configured to house alignment pins, screws, and the like. One or more of the plurality of holes 250 may be aligned with the holes 242 of the second metal layer 220. Further, FIG. 2D shows an input coupling port 212, where the antenna 240 may receive electromagnetic waves into the one or more waveguide channels 202. In addition, FIG. 2D features multiple coupling ports 252. The coupling ports 252 may couple from waveguides within the first metal layer 200 to components on a PCB (not shown in FIG. 2D) that couple electromagnetic energy from the respective coupling port. The coupling ports 212, 252 may take the form of coupling port 404 of FIG. 4A.

FIG. 2E illustrates conceptual waveguide channels 260 formed inside an assembled example antenna. More particularly, the waveguide channels 260 take the form of the waveguide channels 202 of FIGS. 2A and 2B. For instance, the channels 260 include an input port 262 to the input waveguide channel 264. The channels 260 also include wave-dividing channels 266 and a plurality of radiating doublets 268 (i.e., a DOEWG array). As described above, when electromagnetic waves enter the channels 260 at the input coupling port 262, they may travel in the +x direction through the input waveguide channel 264 and be divided into portions by the wave-dividing channels 266 (e.g., by the power dividers). Those portions of electromagnetic waves may then travel in the +x direction to respective radiating doublets 268, where sub-portions of those portions are radiated out each DOEWG through pairs of output ports, such as pair 270, for instance.

In a particular wave-radiating channel, a portion of electromagnetic waves may first be propagated through a first DOEWG with a recessed wave-directing member 272 (i.e., an inverse step, or “well”), as discussed above. This recessed wave-directing member 272 may be configured to radiate the smallest fraction of energy of all the members of the DOEWGs of the particular wave-radiating channel. In some examples, subsequent wave-directing members 274 may be formed (e.g., protruded, rather than recessed) such that each subsequent DOEWG can radiate a higher fraction of the remaining energy than the DOEWG that came before it. Phrased another way, each wave-directing member 272, 274 may generally be formed as a “step cut” into a horizontal (+x direction) channel (i.e., a wave-radiating channel, or the “first end” of an “elongated segment” as noted above) and used by the antenna to tune the amount of energy that is radiated vs. the amount of energy that is transmitted further down the antenna.

In some embodiments, a given DOEWG may not be able to radiate more than a threshold level of energy and may not be able to radiate less than a threshold level of energy. These thresholds may vary based on the dimensions of the DOEWG components (e.g., the wave-directing member, a horizontal channel, a vertical channel, a bridge between the two output ports, etc.), or may vary based on other factors associated with the antenna.

In some embodiments, the first and second metal layers may be machined such that various sides of the waveguide channels 260 have rounded edges, such as edge 276, 278, and 280, for example.

Further shown in FIG. 2E are both coupling ports 282 and PCB-based coupling components 284. The PCB-based coupling components 284 may be coupled to the coupling ports 282. And the coupling ports 282 may be coupled to the elongated segments 222 of the wave-dividing channels 266. The design of the PCB-based coupling components 284 and coupling ports 282 are discussed further with respect to FIGS. 4A and 4B.

FIG. 3A illustrates a network of wave-dividing channels 300 of an example antenna, in accordance with an example embodiment. FIG. 3B illustrates an alternate view of the network of wave-dividing channels 300, in accordance with an example embodiment.

In some embodiments, the network (e.g., beam-forming network, as noted above) of wave-dividing channels 300 may take the form of a tree of power dividers, as shown in FIG. 3A. Energy may enter the antenna through the input waveguide channel and is divided (i.e., split) into smaller portions of energy at each power divider, such as power divider 302, and may be divided multiple times via subsequent power dividers so that a respective amount of energy is fed into each of the wave-radiating channels (energy A-F, as shown). The amount of energy that is divided at a given power divider may be controlled by a power division ratio (i.e., how much energy goes into one channel 304 versus how much energy goes into another channel 306 after the division). A given power division ratio may be adjusted based on the dimensions of the corresponding power divider.

Within examples, a technique for dividing energy between two channels 304, 306 may be to use a structure of channels (e.g., a “four-port branchline coupler”) such as that shown at the bottom of FIG. 3A. Such a technique and structure design may include attenuation components 310 and coupling ports 308 at the end of a channel, as shown in FIGS. 3A and 3B, where each of the coupling ports 308 is configured to couple energy that returns backwards through the channel to one of the attenuation components 310. The attenuation components 310 may be configured to absorb the returned energy. The design of the attenuation components 310 and coupling ports 308 are discussed further with respect to FIG. 4B.

FIG. 4A illustrates an example waveguide 402 termination comprising coupling port 404, attenuation components 410, and the coupling component 408. The attenuation components 410 may be mounted on a PCB 406 (e.g. the attenuation components 410 may be metallic traces on a PCB). The PCB may be mounted to a bottom surface of an antenna like that shown in FIG. 2D. Furthermore, FIG. 4A illustrates one example use of a coupling port 404. The coupling port 404 may also be used in instances other than the presently disclosed antenna apparatus. For example, the coupling port 404 may be used in any instance where an electromagnetic signal is being coupled into and/or out of a waveguide. Further, the coupling port 404 as disclosed herein may also be used to efficiently couple a signal from a PCB to a radiating structure, like an antenna, without the use of the waveguide beamforming network.

Although FIG. 4A is shown with the coupling component 408 as a differential pair connected to attenuation components 410, in other examples, the coupling component 408 may be a different shape, such as a single patch (as discussed with respect to FIG. 4B). Additionally, the coupling component 408 may be a bidirectional component that may be able to both feed an electromagnetic signal for transmission by the antenna unit and couple an electromagnetic signal from the waveguide to an attenuation component.

The waveguide 402 of FIG. 4A may be a portion of a waveguide elongated segments, such as elongated segments 204 of FIG. 2A. More specifically, the waveguide 402 of FIG. 4A may be one of the elongated segments that does not include the feed. As previously discussed, during the operation of the antenna some electromagnetic energy that is not radiated by the radiation components may be reflected back into the waveguide. In order to remove the reflected electromagnetic energy, the waveguide 402 may be coupled to an coupling port 404. The coupling port 404 may be aligned perpendicularly, and out of the plane of the waveguide 402. The coupling port 404 may be configured to couple the reflected electromagnetic energy to an attenuation component (shown here as lines 410) located on a PCB 406 by way of a coupling component 408.

In some examples, such as shown in FIG. 4A, each coupling port 404 may be shaped in a way to to match (or approximately match) an impedance of the waveguide. By impedance matching, the amount of the reflected electromagnetic energy that is coupled from the waveguide 402 to the coupling port 404 may be maximized. For example, the coupling port 404 may have portions that are of different dimensions to achieve the correct impedance matching. Further, in instances where an antenna unit has multiple coupling ports, each coupling port may have its own dimensions based on the impedance match desired for each respective coupling port.

The coupling port 404 is shown having a neck 418 that has a narrower dimension than the rest of the coupling port 404. In this example by narrowing the neck 418 the inductance of the coupling port 404 is increased. The increase in inductance may be used to match (or more approximately match) the impedance of the coupling component 408 with the impedance of the waveguide 402. When the impedance is matched, the power transfer of the electromagnetic energy between the waveguide 402 and the coupling component 408 may be maximized. A widening of the width of the coupling port 404 may increase the capacitance of coupling port 404. Depending on the specific embodiment, the dimensions of the coupling port 404 may be designed for an impedance match between the waveguide 402 and the coupling component 408.

Additionally, the coupling port 404 and coupling component 408 are shown coupling to the bottom of the waveguide. In other examples, the alignment of the the coupling port 404, PCB 406, and coupling component 408 may have a different alignment. For example, the coupling may be to a side or end of a waveguide as well (i.e. coupled orthogonally to the direction of the plane of the waveguide layer).

To create the coupling port 404, the coupling port 404 may be machined from both the top side of the coupling port 404 and the bottom side of the coupling port 404. By designing a coupling port 404 that has dimensions that can be machined from both sides, a coupling port 404 may be created that performs the impedance matching function while also being relatively simple to manufacture. More complex versions of the coupling port may be designed as well, but having a port that may be machined from both the top and bottom side of the coupling port may decrease machining complexity.

As previously discussed, the coupling component 408 is configured to couple at least a portion of the reflected electromagnetic energy from the waveguide to the attenuation component 410 through the coupling port 404. In this way, when the coupling component 408 couples the at least a portion of the reflected electromagnetic energy, the coupling component 408 may essentially act as a receiving antenna. The coupling component 408 receives the at least a portion of the reflected electromagnetic energy from the waveguide and couples it through the coupling port.

In other examples, the the coupling port 404 may function to inject electromagnetic energy into the waveguide. In this example, component 408 is configured to couple at least a portion of the electromagnetic energy from feed traces (not shown) on the PCB 406 to the waveguide 402 through the coupling port 404. In this way, when the coupling component 408 couples the at least a portion of the electromagnetic energy, the coupling component 408 may essentially act as a transmitting antenna. The coupling component 408 transmits at least a portion of the electromagnetic energy from the feed traces and couples it through the coupling port.

In various different examples, the coupling component 408 may take different forms. For example, the coupling component 408 may be a metallic loop-shaped structure, as shown in FIG. 4A. The coupling component 408 may function similarly to an antenna, that is the coupling component 408 may be able to transmit or receive electromagnetic energy (i.e. a wave). Functionally, in one example, the coupling component 408 may be a component configured to convert a guided wave from a waveguide to a guided wave outside of the waveguide (e.g. couple the wave to an attenuation component). In another example, the coupling component 408 may be a component configured to convert a guided wave from outside the waveguide to a guided wave in a waveguide.

In various examples, the coupling component 408 may be made in various ways and with various materials. As shown in FIG. 4B, the coupling component may be a metallic trace (or patch) on the circuit board 406. However, in other examples, the coupling component may be a discrete component attached to the PCB. For example, the coupling component may be formed of a ceramic that is coated, plated, or otherwise overlaid with metal. The coupling component 408 may also be formed from stamped metal, bent metal, or other another metal structure. In some additional examples, the coupling component 408 may itself be a metallic strip or component on a second circuit board that may be surface mounted to PCB 406.

Therefore, there are many structures that can function to cause the conversion of the wave from a wave in the waveguide to a wave not in the waveguide and can take the place of coupling component 408 (or coupling component 412).

In some examples, the coupling component 408 may be a bi-directional coupler that functions to both (i) couple a signal from outside the waveguide into the waveguide and (ii) couple signal from inside the waveguide out of the waveguide.

In some further examples, the coupling component 408 may be configured to couple a differential mode signal from outside the waveguide into the waveguide. In some additional examples, the coupling component 408 may be configured to couple signal from inside the waveguide out of the waveguide as a differential mode signal.

In some additional examples, the coupling component 408 may be configured to couple a single mode signal from outside the waveguide into the waveguide. In some additional examples, the coupling component 408 may be configured to couple signal from inside the waveguide out of the waveguide as a single mode signal.

In various embodiments, the coupling component 408 may be designed to have an impedance that optimizes the percentage of electromagnetic energy that the coupling component 408 couples between its input and output.

FIG. 4B shows a top-down view of two different types of coupling components 408 and 412 on a circuit board 406. As previously discussed, coupling components 408 are a differential pair. Coupling component 412 is a patch on PCB 406. As shown in FIG. 4B, the coupling components 408 are coupled to differential pair lines 416A. The differential pair lines 416A may be configured to dissipate the reflected electromagnetic energy from coupling components 408, feed electromagnetic energy to coupling components 408, or both feed and dissipate electromagnetic energy when coupling components 408 are operated in bidirectional mode. Similarly, the single line 416B may be configured to dissipate the reflected electromagnetic energy from coupling component 412, feed electromagnetic energy to coupling component 412, or both feed and dissipate electromagnetic energy when coupling component 412 is operated in bidirectional mode.

Further shown in FIG. 4B are grounding points 414. The grounding points 414 are points that may be used to introduce an electrical ground to the PCB 406. The grounding points 414 may form an electrical contact with the waveguide block, such as the bottom of waveguide block shown in FIG. 2D.

The attenuation component 410 is disposed on a circuit board 406 located outside of, or on an external surface of, the waveguide block structure. The attenuation component 410 may receive the at least a portion of the reflected electromagnetic energy from the coupling component 408. In some examples, a surface of the attenuation component 410 may be configured to comprising absorb the portion of the reflected electromagnetic energy. In some further examples, the attenuation component may include at least one microstrip line on the circuit board. Yet further, the attenuation component may include conductive ink printed on the circuit board.

It should be understood that other shapes and dimensions of the waveguide channels, portions of the waveguide channels, sides of the waveguide channels, wave-directing members, and the like are possible as well. In some embodiments, a rectangular shape of waveguide channels may be highly convenient to manufacture, though other methods known or not yet known may be implemented to manufacture waveguide channels with equal or even greater convenience.

It should be understood that arrangements described herein are for purposes of example only. As such, those skilled in the art will appreciate that other arrangements and other elements (e.g. machines, apparatuses, interfaces, functions, orders, and groupings of functions, etc.) can be used instead, and some elements may be omitted altogether according to the desired results. Further, many of the elements that are described are functional entities that may be implemented as discrete or distributed components or in conjunction with other components, in any suitable combination and location.

While various aspects and embodiments have been disclosed herein, other aspects and embodiments will be apparent to those skilled in the art. The various aspects and embodiments disclosed herein are for purposes of illustration and are not intended to be limiting, with the scope being indicated by the following claims.

Number	Name	Date	Kind
4901040	Ahlborn et al.	Feb 1990	A
5668512	Mohwinkel	Sep 1997	A
6191670	Nguyen	Feb 2001	B1
6794950	du Toit et al.	Sep 2004	B2
8723616	Hirota	May 2014	B2
8912859	Leiba et al.	Dec 2014	B2
9538658	Shen	Jan 2017	B2
9979094	Izadian	May 2018	B1
20020009264	Koteles	Jan 2002	A1
20030076188	Dawn et al.	Apr 2003	A1
20040150554	Stenger	Aug 2004	A1
20060132374	Wang	Jun 2006	A1
20070182505	Fujita	Aug 2007	A1
20080129409	Nagaishi	Jun 2008	A1
20080258848	Quan	Oct 2008	A1
20100245155	Miyazato	Sep 2010	A1
20110057741	Dayan et al.	Mar 2011	A1
20130183902	McCarthy et al.	Jul 2013	A1
20150155847	Baret et al.	Jun 2015	A1

Number	Date	Country
2000013110	Jan 2000	JP
2009288545	Dec 2009	JP
2015192293	Nov 2015	JP
2017136098	Aug 2017	WO

Iris matched PCB to waveguide transition

Information

Patent Number

Date Filed

Date Issued

Inventors

Original Assignees

Examiners

Agents

CPC

Field of Search

CPC

International Classifications

Term Extension

Abstract

Description

Claims

US Referenced Citations (19)

Foreign Referenced Citations (4)

Non-Patent Literature Citations (1)

Related Publications (1)