US20170237180A1 - Laminar Phased Array Antenna - Google Patents
Laminar Phased Array Antenna Download PDFInfo
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- US20170237180A1 US20170237180A1 US15/267,689 US201615267689A US2017237180A1 US 20170237180 A1 US20170237180 A1 US 20170237180A1 US 201615267689 A US201615267689 A US 201615267689A US 2017237180 A1 US2017237180 A1 US 2017237180A1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
- H01Q21/061—Two dimensional planar arrays
- H01Q21/065—Patch antenna array
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
- H01Q21/22—Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/22—Supports; Mounting means by structural association with other equipment or articles
- H01Q1/2283—Supports; Mounting means by structural association with other equipment or articles mounted in or on the surface of a semiconductor substrate as a chip-type antenna or integrated with other components into an IC package
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/22—Supports; Mounting means by structural association with other equipment or articles
- H01Q1/24—Supports; Mounting means by structural association with other equipment or articles with receiving set
- H01Q1/241—Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM
- H01Q1/242—Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM specially adapted for hand-held use
- H01Q1/245—Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM specially adapted for hand-held use with means for shaping the antenna pattern, e.g. in order to protect user against rf exposure
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
- H01Q1/38—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/24—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/26—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/26—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
- H01Q3/30—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array
- H01Q3/34—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array by electrical means
- H01Q3/36—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array by electrical means with variable phase-shifters
- H01Q3/38—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array by electrical means with variable phase-shifters the phase-shifters being digital
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- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L5/00—Arrangements affording multiple use of the transmission path
- H04L5/14—Two-way operation using the same type of signal, i.e. duplex
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- H—ELECTRICITY
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- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L5/00—Arrangements affording multiple use of the transmission path
- H04L5/14—Two-way operation using the same type of signal, i.e. duplex
- H04L5/1469—Two-way operation using the same type of signal, i.e. duplex using time-sharing
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- H—ELECTRICITY
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- H04L5/00—Arrangements affording multiple use of the transmission path
- H04L5/14—Two-way operation using the same type of signal, i.e. duplex
- H04L5/16—Half-duplex systems; Simplex/duplex switching; Transmission of break signals non-automatically inverting the direction of transmission
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Abstract
Description
- This patent application claims priority from provisional U.S. Patent Application No. 62/220,522, filed Sep. 18, 2015, attorney docket number 4181/1002, entitled, “LAMINAR PHASED ARRAY ANTENNA,” and naming David Corman, Vipul Jain, Timothy Carey, and Nitin Jain as inventors, the disclosure of which is incorporated herein, in its entirety, by reference.
- This patent application is related to U.S. patent application Ser. No. ______, filed on even date herewith, attorney docket number 4181/1008, entitled, “LAMINAR PHASED ARRAY WITH POLARIZATION-ISOLATED TRANSMIT/RECEIVE INTERFACES,” and naming David Corman, Vipul Jain, Timothy Carey, and Nitin Jain as inventors, the disclosure of which is incorporated herein, in its entirety, by reference.
- The invention generally relates to phased array systems and, more particularly, the invention relates to laminar phased arrays/patch arrays.
- Antennas that emit electronically steered beams are known in the art as “phased array antennas.” Such antennas are used worldwide in a wide variety of commercial and radar applications. They typically are produced from many small radiating elements that are individually phase controlled to form a beam in the far field of the antenna.
- Among other things, phased array antennas are popular due to their ability to rapidly steer beams without requiring moving parts. One problem, however, is their cost. They can cost on the order of $1000 per element. Thus, for a 1000 element array, the cost can reach or exceed $1,000,000.
- In accordance with one embodiment of the invention, a phased array has a laminar substrate, a plurality of elements on the front side of the substrate, and a plurality of integrated circuits also on the front side of the substrate. This structure is arranged to form a patch phased array. The plurality of integrated circuits, which are configured to control receipt and/or transmission of signals by the plurality of elements in the phased array, preferably are wafer level chip scale packaging integrated circuits. Moreover, the plurality of integrated circuits are configured to operate the phased array at one or more satellite frequencies to have the capability of transmitting signals and/or receiving signals from a satellite.
- The plurality of elements may take on any of a variety of forms, such as those of a triangular, rectangular, or hexagonal lattice. To improve efficiency, each integrated circuit is configured to control at least two elements (e.g., four elements or more). For example, each integrated circuit may include a phase shifter to control the phase of signals transmitted by at least one of the elements. The phase shifter preferably is a four bit or smaller phase shifter.
- As another example, each integrated circuit may include a splitter between a common arm and two side arms. In this case, each of the integrated circuits may have a side arm beam gain control of no more than about 5 db. Each integrated circuit may further include an active phase shifter (e.g., using no passive elements), and/or may be configured to use time division duplex waveforms to enable the phased array to be used for both transmission and receipt of signals.
- Some of the integrated circuits, which may be flip-chip bonded to the substrate, preferably are positioned on the substrate between at least two elements. The flip-chip bonding also may produce an open space between the bottom side of the integrated circuit and the substrate (e.g., if no fill is included in that space). To provide more structural protection and filter certain frequencies, the phased array also may position a polarizer between the substrate and a radome.
- In accordance with another embodiment, an apparatus for communicating with a satellite has a printed circuit board with a front side supporting a plurality of elements and a plurality of integrated circuits. These elements and integrated circuits form a patch phased array. As such, the plurality of integrated circuits have circuitry for controlling receipt and/or transmission of signals by the plurality of elements in the patch phased array. Moreover, the plurality of integrated circuits are wafer level chip scale packaging integrated circuits. To communicate effectively with at least one satellite, the plurality of integrated circuits have circuitry for operating the phased array at one or more frequencies of the Ka-band, Ku-band, and/or X-band.
- In accordance with other embodiments, a method of producing a phased array forms a plurality of elements on a front side of a laminar substrate to form a patch array. The method also flip chip mounts a plurality of wafer level chip scale packaged integrated circuits to the front side of the laminar substrate. At least two of the plurality of elements have at least one integrated circuit therebetween. The plurality of integrated circuits are configured to control receipt and/or transmission of signals by the plurality of elements in the patch phased array. In addition, the plurality of integrated circuits also are configured operate the phased array at one or more frequencies of the Ka-band, Ku-band, and/or X-band to communicate with at least one satellite. The method electrically connects each of the plurality of integrated circuits to at least two elements.
- Those skilled in the art should more fully appreciate advantages of various embodiments of the invention from the following “Description of Illustrative Embodiments,” discussed with reference to the drawings summarized immediately below.
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FIG. 1 schematically shows an active electronically steered antenna system (“AESA system”) configured in accordance with illustrative embodiments of the invention and communicating with a satellite. -
FIGS. 2A and 2B schematically show generalized diagrams of an AESA system that may be configured in accordance with illustrative embodiments of the invention. -
FIG. 3A schematically shows a plan view of a laminar printed circuit board portion of an AESA configured in accordance with illustrative embodiments of the invention. -
FIG. 3B schematically shows a close-up of a portion of the laminated printed circuit board ofFIG. 3A . -
FIG. 4 schematically shows a cross-sectional view of the laminated printed circuit board of 3A to highlight the mounting of its integrated circuits. -
FIG. 5 schematically shows a circuit diagram of a portion of an integrated circuit mounted on the laminated printed circuit board ofFIG. 3A . -
FIG. 6 shows a process of forming an AESA system in accordance with illustrative embodiments of the invention. - Illustrative embodiments form a low cost phased array with a high sensitivity to received signals. In addition, the phased array also efficiently transmits outgoing signals/beams to other communication devices at the required power levels. To that end, the phased array preferably has a laminar substrate with a front face supporting both 1) an array of antennas (also referred to as “elements” or “patches”), and 2) a corresponding array of wafer level chip scale packaged (“WLCSP”) integrated circuits. In addition to controlling the antennas, the WLCSP integrated circuits are configured to operate the phased array at one or more satellite frequencies, thus enabling communication with orbiting satellites. Details of illustrative embodiments are discussed below.
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FIG. 1 schematically shows an active electronically steered antenna system (“AESAsystem 10”) configured in accordance with illustrative embodiments of the invention and communicating with an orbitingsatellite 12. A phased array (discussed below and identified by reference number “10A”) implements the primary functionality of the AESAsystem 10. Specifically, as known by those skilled in the art, thephased array 10A forms one or more of a plurality of electronically steerable beams that can be used for a wide variety of applications. As a satellite communication system, for example, the AESAsystem 10 preferably is configured operate at one or more satellite frequencies. Among others, those frequencies may include the Ka-band, Ku-band, and/or X-band. - The satellite communication system may be part of a cellular network operating under a known cellular protocol, such as the 3G, 4G, or 5G protocols. Accordingly, in addition to communicating with satellites, the system may communicate with earth-bound devices, such as smartphones or other mobile devices, using any of the 3G, 4G, or 5G protocols. As another example, the satellite communication system may transmit/receive information between aircraft and air traffic control systems. Of course, those skilled in the art may use the AESA system 10 (implementing the noted phased
array 10A) in a wide variety of other applications, such as broadcasting, optics, radar, etc. Some embodiments may be configured for non-satellite communications and instead communicate with other devices, such as smartphones (e.g., using 4G or 5G protocols). Accordingly, discussion of communication with orbitingsatellites 12 is not intended to limit all embodiments of the invention. -
FIGS. 2A and 2B schematically show generalized diagrams of theAESA system 10 configured in accordance with illustrative embodiments of the invention. Specifically,FIG. 2A schematically shows a block diagram of theAESA system 10, whileFIG. 2B schematically shows a cross-sectional view of a small portion of thesame AESA system 10 across line B-B. This latter view shows a single silicon integrated circuit 14 (controllingelements 18, discussed below) mounted onto asubstrate 16 between two transmit and/or receiveelements 18, i.e., on the same side of a supportingsubstrate 16 and juxtaposed with the twoelements 18. In alternative embodiments, however, theintegrated circuit 14 could be on the other side of thesubstrate 16. The phasedarray 10A also has apolarizer 20 to selectively filter signals to and from the phasedarray 10A, and aradome 22 to environmentally protect the phasedarray 10A. A separate antenna controller 24 (FIG. 2B ) electrically connects with the phasedarray 10A to calculate beam steering vectors for the overall phasedarray 10A, and to provide other control functions. -
FIG. 3A schematically shows a plan view of a primary portion of anAESA system 10 that may be configured in accordance with illustrative embodiments of the invention. In a similar manner,FIG. 3B schematically shows a close-up of a portion of the phasedarray 10A ofFIG. 3A . - Specifically, the
AESA system 10 ofFIG. 3A is implemented as a laminar phasedarray 10A having a laminated printed circuit board 16 (i.e., acting as the substrate and also identified by reference number “16”) supporting the above noted plurality ofelements 18 andintegrated circuits 14. Theelements 18 preferably are formed as a plurality of square or rectangular patch antennas oriented in a triangular patch array configuration. In other words, eachelement 18 forms a triangle with two otheradjacent elements 18. When compared to a rectangular lattice configuration, this triangular lattice configuration requires fewer elements 18 (e.g., about 15 percent fewer in some implementations) for a given grating lobe free scan volume. Other embodiments, however, may use other lattice configurations, such as a pentagonal configuration or a hexagonal configuration. Moreover, despite requiringmore elements 18, some embodiments may use a rectangular lattice configuration. Like other similar phased arrays, the printedcircuit board 16 also may have a ground plane (not shown) that electrically and magnetically cooperates with theelements 18 to facilitate operation. - Indeed, the array shown in
FIGS. 3A and 3B is a small phasedarray 10A. Those skilled in the art can apply principles of illustrative embodiments to laminar phasedarrays 10A with hundreds, or even thousands ofelements 18 andintegrated circuits 14. In a similar manner, those skilled in the art can apply various embodiments to smaller phasedarrays 10A. - As a patch array, the
elements 18 have a low profile. Specifically, as known by those skilled in the art, a patch antenna (i.e., the element 18) typically is mounted on a flat surface and includes a flat rectangular sheet of metal (known as the patch and noted above) mounted over a larger sheet of metal known as a “ground plane.” A dielectric layer between the two metal regions electrically isolates the two sheets to prevent direct conduction. When energized, the patch and ground plane together produce a radiating electric field. As discussed below with regard toFIG. 6 , illustrative embodiments may form the patch antennas using conventional semiconductor fabrication processes, such as by depositing one or more successive metal layers on the printedcircuit board 16. Accordingly, using such fabrication processes, each radiatingelement 18 in the phasedarray 10A should have a very low profile. - The
AESA system 10 can have one or more of any of a variety of different functional types ofelements 18. For example, theAESA system 10 can have transmit-only elements 18, receive-only elements 18, and/or dual mode receive and transmit elements 18 (referred to as “dual-mode elements 18”). The transmit-only elements 18 are configured to transmit outgoing signals (e.g., burst signals) only, while the receive-only elements 18 are configured to receive incoming signals only. In contrast, the dual-mode elements 18 are configured to either transmit outgoing burst signals, or receive incoming signals, depending on the mode of the phasedarray 10A at the time of the operation. Specifically, when using dual-mode elements 18, the phasedarray 10A can be in either a transmit mode, or a receive mode. Thenoted controller 24 at least in part controls the mode and operation of the phasedarray 10A, as well as other array functions. - The
AESA system 10 has a plurality of the above noted integrated circuits 14 (noted with regard toFIG. 2B ) for controlling operation of theelements 18. Those skilled in the art often refer to theseintegrated circuits 14 as “beam steering integrated circuits.” Prior art beam steering integrated circuits known to the inventors took up a lot of real estate on the printedcircuit board 16. This is contrary to one general goal of maximizing the surface area of theelements 18 on the front face of thesubstrate 16. To solve this problem, those in the art relegated prior art integrated circuits known to the inventors to the opposite side of thecircuit board 16—i.e., the side opposite theelements 18. While it may have helped maximize/optimize element area, it caused certain noise issues due to the relatively long transmission line to theelements 18. The inventors recognized both of these problems and, consequently, modified the phasedarray 10A, including theintegrated circuits 14, to enable them to be mounted on the same side as theelements 18; namely, on the front side of the printedcircuit board 16. - To that end, each
integrated circuit 14 preferably is configured with at least the minimum number of functions to accomplish the desired effect. Indeed,integrated circuits 14 fordual mode elements 18 are expected to have some different functionality than that of theintegrated circuits 14 for the transmit-only elements 18 or receive-only elements 18. Accordingly,integrated circuits 14 for such non-dual-mode elements 18 typically have a smaller footprint than theintegrated circuits 14 that control the dual-mode elements 18. Despite that, some or all types ofintegrated circuits 14 fabricated for the phasedarray 10A can be modified to have a smaller footprint. - As an example, depending on its role in the phased
array 10A, eachintegrated circuit 14 may include some or all of the following functions: -
- phase shifting,
- amplitude controlling/beam weighting,
- switching between transmit mode and receive mode,
- output amplification to amplify output signals to the
elements 18, - input amplification for received RF signals (e.g., signals received from the satellite 12), and
- power combining/summing and splitting between
elements 18.
- Indeed, some embodiments of the
integrated circuits 14 may have additional or different functionality, although illustrative embodiments are expected to operate satisfactorily with the above noted functions. Those skilled in the art can configure theintegrated circuits 14 in any of a wide variety of manners to perform those functions. For example, the input amplification may be performed by a low noise amplifier, the phase shifting may use conventional active phase shifters, and the switching functionality may be implemented using conventional transistor-based switches. Additional details of the structure and functionality ofintegrated circuits 14 are discussed below with reference toFIG. 5 . - As noted above, the
AESA system 10 preferably communicates with one or more orbitingsatellites 12 and thus, uses satellite frequencies for that communication. Accordingly, the plurality ofintegrated circuits 14 preferably are configured operate the phasedarray 10A at one or more frequencies of the Ka-band, Ku-band, and/or X-band to communicate with at least onesatellite 12. Of course, as satellite communication technology progresses, future implementations may modify the frequency bands of theintegrated circuits 14 to communicate using new satellite frequencies. - The inventors recognized that the cost of the phased
array 10A is directly related to the number ofelements 18 andintegrated circuits 14. Moreover, the number ofintegrated circuits 14 also has a direct relation to the size of the printedcircuit board 16. In fact, the total number ofintegrated circuits 14 used and the size of the printedcircuit board 16 accounts for a substantial majority of the total array costs. The inventors thus designed the array so thatmultiple elements 18 share theintegrated circuits 14, thus reducing the required total number ofintegrated circuits 14. This reduced number ofintegrated circuits 14 correspondingly reduces the required size of the printedcircuit board 16, which reduces the cost of theAESA system 10. In addition, more surface area on the top face of the printedcircuit board 16 may be dedicated to theelements 18. - To that end, each
integrated circuit 14 preferably operates on at least oneelement 18 in the array. For example, oneintegrated circuit 14 can operate on two or fourdifferent elements 18. Of course, those skilled in the art can adjust the number ofelements 18 sharing anintegrated circuit 14 based upon the application. For example, a singleintegrated circuit 14 can control twoelements 18, threeelements 18, fiveelements 18, sixelements 18, sevenelements 18, eightelements 18, etc., or some range ofelements 18. Sharing theintegrated circuits 14 betweenmultiple elements 18 in this manner reduces the required total number ofintegrated circuits 14, correspondingly reducing the required size of the printedcircuit board 16. - As noted above, the dual-
mode elements 18 may operate in a transmit mode, or a receive mode. To that end, theintegrated circuits 14 may generate time division diplex or duplex waveforms so that a single aperture or phasedarray 10A can be used for both transmitting and receiving. In a similar manner, some embodiments may eliminate a commonly included transmit/receive switch in the side arms (discussed below with regard toFIG. 5 ) of theintegrated circuit 14. Instead, such embodiments may duplex at theelement 18. This process can be performed by isolating one of theelements 18 between transmit and receive by an orthogonal feed connection. The inventors discovered that such a feed connection may eliminate about a 0.8 dB switch loss and improve G/T (i.e., the ratio of the gain or directivity to the noise temperature) by about 1.3 dB for some implementations. Additional details of the orthogonal feed connection are discussed below with regard toFIG. 5 . - RF interconnect and/or
beam forming lines 26 electrically connect theintegrated circuits 14 to theirrespective elements 18. To further minimize the feed loss, illustrative embodiments mount theintegrated circuits 14 as close to theirrespective elements 18 as possible. Specifically, this close proximity preferably reduces RF interconnect line lengths, reducing the feed loss. To that end, eachintegrated circuit 14 preferably is packaged either in a flip-chipped configuration using wafer level chip scale packaging (WLCSP), or a traditional package, such as quad flat no-leads package (QFN package). While other types of packaging may suffice, WLCSP techniques are preferred to minimize real estate on thesubstrate 16. - In addition to reducing feed loss, using WLCSP techniques reduces the overall footprint of the
integrated circuits 14, enabling them to be mounted on the top face of the printedcircuit board 16 with theelements 18—providing more surface area for theelements 18. The inventors thus discovered that using WLCSP techniques, coupled with other innovations discussed herein, and able the system to operate within acceptable operation specifications. - It should be reiterated that although
FIGS. 3A and 3B show theAESA system 10 with some specificity (e.g., the layout of theelements 18 and integrated circuits 14), those skilled in the art may apply illustrative embodiments to other implementations. For example, as noted above, eachintegrated circuit 14 can connect to more orfewer elements 18, or the lattice configuration can be different. Accordingly, discussion of the specific configuration of theAESA system 10 ofFIG. 3A (and other figures) is for convenience only and not intended to limit all embodiments. -
FIG. 4 schematically shows a cross-sectional view of the layout of components on the laminated printedcircuit board 16 of 3A to highlight the flip-chip mounting of itsintegrated circuits 14. Theintegrated circuit 14 in this drawing intentionally is enlarged to show details of a flip-chip mounting technique. Unlike techniques that permit input/output (“I/O”) only on the edge of theintegrated circuit 14, flip-chip mounting permits I/O on interior portions of theintegrated circuit 14. - As shown, the
integrated circuit 14 has a plurality ofpads 28 aligned with a plurality ofcorresponding pads 28 on the printedcircuit board 16. These opposingpads 28 on theintegrated circuit 14 and the printedcircuit board 16 may be considered to form pairs ofpads 28. Solder 30 (e.g., solder balls) electrically connects each the pads in corresponding pairs ofpads 28. Interconnect lines, traces, and other electrical interconnects on/in the printed circuit board 16 (e.g., lines 26) thus permit theintegrated circuit 14 to communicate withother elements 18 through this electrical interface. - The embodiment shown in
FIG. 4 forms a space or void (identified by reference number “32”) between the bottom of the integrated circuit 14 (from the perspective of this drawing) and the top surface of the printedcircuit board 16. Thisspace 32 may remain an open void—containing no material. Some embodiments may take advantage of thisextra space 32 to add further components, such as additional circuit elements, without requiring more circuit board space. Alternatively, thisspace 32 may contain fill material (not shown) for further stability and thermal management of theintegrated circuit 14. - Other embodiments, however, still may use similar
integrated circuits 14, but not use flip-chip mounting techniques. Instead, other mounting techniques may couple theintegrated circuits 14 with thesubstrate 16. Among other things, those techniques may incorporate surface mounting, or wirebond mounting with theintegrated circuit 14 rotated 180 degrees from the orientation ofFIG. 4 . Accordingly, discussion of flip chip mounting techniques is but one of a variety of different techniques that may be used with various embodiments of the invention. - As noted above, each
integrated circuit 14 preferably has a minimal amount of circuitry to perform its required function. To that end,FIG. 5 schematically shows relevant portions of one integratedcircuit 14 that may be configured in accordance with illustrative embodiments of the invention to control twoelements 18. This exemplaryintegrated circuit 14 is shown and described as connected to twodifferent elements 18 identified as element E1 and element E2. Of course, principles described with regard toFIG. 5 can apply equally tointegrated circuits 14 controlling more than twoelements 18, such as fourelements 18. - As shown, the
integrated circuit 14 has afirst vector modulator 34 for controlling receipt and transmission of signals of a first element E1, and asecond vector modulator 34 for controlling receipt and transmission of signals of a second element E2. The twovector modulators 34 each have a receivearm 36, coupled to theirrespective elements 18, for receiving signals. InFIG. 5 , because they transmit signals away from their elements E1 or E2, the receivearms 36 have arrows pointing away from their respective elements E1 and E2. To that end, each receivearm 36 has a phase shift modulator 38 (also referred to as a “phase shifter 38”) for changing the phase of the incoming signals, and anamplifier 40 for amplifying the incoming signal. Among other things, theamplifiers 40 in the receivearms 36 are implemented as low noise amplifiers. - In illustrative embodiments, the
amplifier 40 is a fixed gain amplifier. Accordingly, to control the amplification with more precision, each receivearm 36 also has anactive gain controller 42 that increases or decreases the amplification provided by theamplifier 40. Alternatively, theamplifier 40 may be a variable gain amplifier. Accordingly, in that case, theactive gain controller 42 may be omitted. As known by those skilled in the art, the amplifier(s) 40 and thephase shifter 38 cooperate to control incoming received signals. - In a corresponding manner, the two
vector modulators 34 also each have a transmitarm 44 coupled to theirrespective elements 18. In an opposite manner to the receivearms 36, the transmitarms 44 inFIG. 5 have arrows pointing toward theirrespective elements 18. Each transmitarm 44 thus has aphase shifter 38 for changing the phase of the incoming signals, and anamplifier 40 for amplifying the incoming signal. The transmitarms 44 also may have anactive gain controllers 42 if the transmitamplifiers 40 have a fixed gain. Alternatively, the transmitarms 44 may omit theactive gain controllers 42 if theamplifier 40 is a variable gain amplifier. As known by those skilled in the art, the amplifier(s) 40 and thephase shifter 38 cooperate to steerably beam outgoing signals to other devices, such as to thesatellite 12 ofFIG. 1 . - As noted above, the inventors recognized that reducing the overall footprint of the
integrated circuit 14 should improve overall performance. To that end, the inventors discovered that if they provided a sufficient number ofelements 18 in theAESA system 10, they could reduce the sizes of thephase shifters 38. For example, after testing, the inventors discovered that use of a 4bit phase shifter 38 would provide sufficient results with a sufficient number ofelements 18. The 4bit phase shifter 38 thus provides up to 16 different vectors for transmitting a beam from a given element. In illustrative embodiments, each of the 16 different vectors is substantially evenly partitioned between zero and 360 degrees (e.g., 0 degrees, 22.4 degrees, 45 degrees, etc.). Other embodiments, however, may use smaller phase shifters 38 (e.g., 3 bit phase shifters 38) or larger phase shifters 38 (e.g., 5 or 6 bit phase shifters 38). Again, this number should be coordinated with the number ofelements 18, as well as the gain of theamplifiers 40. - The inventors further discovered that the receive and transmit
arms vector modulators 34 could use relativelylow gain amplifiers 40 if they appropriately selected of other element parameters. For example, theamplifiers 40 may have active gain control from 1 dB up to 3 dB, 4 dB, 5 dB, or greater (e.g., 6 dB). Again,low gain amplifiers 40 used in this application should further reduce the size of theintegrated circuit 14. - The receive
arms 36 and the transmitarms 44 may be considered to be “side arms” that combine and/or distribute signals at a summation point (also referred to as a “splitter” when splitting signals). Specifically, the two receivearms 36 meet at a receiving summing node 46A that combines the received signals from both the first andsecond elements 18. In a corresponding manner, the two transmitarms 44 also meet at a transmitting summing node 46B that, in an opposite manner to that of the receiving summing node 46A, distributes the transmit signals of the first andsecond elements 18 for transmission. Among other things, the summingnodes 46 may be implemented as a compact Wilkinson power divider/summer, which, as its name suggests, distributes/divides and/or sums signals. Indeed, the summingnodes 46 may be implemented by other active components and thus, a Wilkinson power divider/summer is but one example. - In addition to connecting with the side arms, each summing node 46A also connects with a main arm (aka “common arm”) that itself may have an amplifier and/or active gain controller (not shown). In illustrative embodiments, the gain of the amplifier in the main arm is greater than those in the side arms. The main arm also has a
switch 48 that switches between the transmit mode to the receive mode. - Illustrative embodiments preferably do not have switches on the side arms. To that end, the transmit and receive sides of each
vector modulator 34 preferably are physically coupled with adjacent sides of itselement 18. Specifically, if theelements 18 are sized so that they are about half a wavelength from side-to-side, then opposite sides will be about 180 degree out of phase with each other. Adjacent sides, however, are about 90 degrees out of phase with each other. In this manner, the transmitarms 44 may be considered to be polarized a first way (e.g., “vertically polarized”), while the receivearms 36 may be considered to be polarized a second, orthogonal way (e.g., “horizontally polarized”). - Accordingly, the receive
arms 36 inFIG. 5 connect with a top portion of theirrespective elements 18, while the transmitarms 44 ofFIG. 5 connect with a side (orthogonal) portion of theirrespective elements 18. Indeed, other embodiments may polarize the transmit and receivearms 36 differently. As such, the specific polarization discussed above is but one example and not intended to limit various embodiments. - When coupled as shown, illustrative embodiments avoid the need for a switch on the side arms by using a duplexing/diplexing signal for transmit and receive (noted above). For example, illustrative embodiments may use time division diplex waveforms or frequency division diplex waveforms to both transmit and receive signals. In that case, to permit asymmetric transmit and receive data transmission, the transmit and receive signals may be allocated to different time slots in the same frequency band. For example, one or more of the
elements 18 may couple with a frequency diplexer (not shown) that splits its relevant signal into a first frequency signal and a second frequency signal. Each of the generated frequency signals is then routed to its own independent circuit that either receives or transmits to or from theelement 18. - The duplex/diplex waveforms may be generated in a number of different ways. In some embodiments, the
integrated circuits 14 are configured to produce those waveforms. In other embodiments, one or more diplexers or duplexers on thesubstrate 16 at least in part produce those waveforms.FIG. 3B schematically shows one such diplexer or duplexer, identified byreference number 27. This diplexer/duplexer 27 communicates with other components, such as theintegrated circuits 14, using the transmission lines (e.g., traces, vias, lines, etc.) on thesubstrate 16. - During operation, the
switch 48 in the main arm may be in the transmit mode. Accordingly, the main arm receives a transmit signal through the switch. Next, that signal is distributed to the two transmitarms 44 through the transmitting summing node 46B. In this capacity, the transmitting summing node 46B acts like a distribution node as it distributes the signal to be transmitted to each side arm. Next, each side arm in therespective vector modulators 34 then shift and amplify its received signal as needed, and transmit that conditioned signal through itsrespective element 18 to the orbitingsatellite 12. - After the transmission process is completed, the
switch 48 on the main arm may be actuated to the receive mode. Accordingly, each receivearm 36 shifts and amplifies the signal received by its respective element E1 or E2. The receiving summing node 46A then sums or combines these two conditioned signals to produce a combined signal that is forwarded to other components through theswitch 48 in the main arm. - Of course, it should be noted that the specific configuration of
elements 18 inFIG. 5 is but one of a wide variety of different configuration to accomplish the desired effect. Accordingly, when implementing various embodiments, those skilled in the art can add other components, remove components, or rearrange the noted components. The specific configuration ofFIG. 5 therefore is intended to be illustrative and not intended to limit various embodiments the invention. -
FIG. 6 shows a process of forming the phasedarray 10A/AESA system 10 in accordance with illustrative embodiments of the invention. It should be noted that this process is substantially simplified from a longer process that normally would be used to form theAESA system 10. Accordingly, the process of forming theAESA system 10 is expected to have many steps, such as testing steps, soldering steps, or passivation steps, which those skilled in the art may use. In addition, some of the steps may be performed in a different order than that shown, or at the same time. Those skilled in the art therefore can modify the process as appropriate. Moreover, as noted above and below, the discussed materials and structures are merely examples. Those skilled in the art can select the appropriate materials and structures depending upon the application and other constraints. Accordingly, discussion of specific materials and structures is not intended to limit all embodiments. - The process of
FIG. 6 begins atstep 600, which forms the array ofelements 18 on thesubstrate 16/printedcircuit board 16. As noted above, theelements 18 preferably are formed from metal deposited onto thesubstrate 16 in a triangular lattice. This step also may formpads 28 andlines 26 on the printedcircuit board 16 to extend to the elements 18 (from the pads 28). As discussed below, theselines 26 electrically connect theintegrated circuits 14 with theelements 18. - In preferred embodiments, the
elements 18 are spaced apart from each other as a function of the wavelength of the signals expected to be transmitted and received by theAESA system 10. For example, the distances between theelements 18 may be spaced apart a distance equal to between 40-60 percent of the wavelength of the relevant signals. Some embodiments, however, may vary the spacing of theelements 18. See, for example, co-pending provisional U.S. Patent Application No. 62/376,442, filed on Aug. 18, 2016 and entitled, “Hybrid Laminated Phased Array,” for further spacing and other details of similar embodiments. The disclosure of that provisional patent application (U.S. Patent application Ser. No. 62/376,442) is incorporated herein, in its entirety, by reference. - Those skilled in the art can select the appropriate numbers of
elements 18, based upon the application. Specifically, a given application may require a specified minimum equivalent isotropically radiated power (“EIRP”) for transmitting signals. In addition, that same application may have a specified minimum G/T for receiving signals. Thus, step 600 may form the array to have a minimum number ofelements 18 to meet either or both the EIRP and the G/T requirements of the application. For example, after establishing the feed loss and the noise figure of the receiveamplifier 40 of the vector receivearms 36, one in the art can set the array size to a desired G/T. Of course, the phasedarray 10A may havemore elements 18 beyond that minimum number. - Other embodiments may use other requirements for selecting the appropriate number of
elements 18. Accordingly, discussion of the specific means for selecting the appropriate number ofelements 18, and their spacing, is for descriptive purposes only and not intended to limit various embodiments of the invention. - At
step 602, the process mounts theintegrated circuits 14 to the printedcircuit board 16/substrate 16. To that end, as noted above, when using WLCSPintegrated circuits 14, illustrative embodiments may use conventional flip-chip mounting processes. Such a process directly electrically connects theintegrated circuits 14 to the elements 18 (step 604). To that end, such embodiments may deposit solder paste (e.g., powdered solder and flux) on thepads 28 of the printedcircuit board 16, and position theintegrated circuits 14 on theirrespective board pads 28. Then, the printedcircuit board 16 may be heated (e.g., using a reflow oven or process) to physically and electrically couple thepads 28 with thesolder 30. - Some embodiments that do not use flip-chip mounted WLCSP
integrated circuits 14, however, may require the additional step ofstep 604 to electrically connect theintegrated circuits 14 to theelements 18. For example, a wirebond operation may be required to solder wirebonds between theintegrated circuits 14 and theelements 18. - The process concludes by adding the polarizer 20 (step 606) and securing the radome 22 (step 608) to the apparatus in a conventional manner.
- Accordingly, contrary to the conventional wisdom, the inventors recognized that despite the possibility of reducing the element area, which is generally undesirable, they could mount WLCSP
integrated circuits 14 to the front side of the printedcircuit board 16 to produce more cost efficient satellitecommunication AESA system 10. Moreover, as noted, theAESA system 10 can have improved G/T and/or EIRP values despite the tradeoff incurred by the loss of element area. - Although the above discussion discloses various exemplary embodiments of the invention, it should be apparent that those skilled in the art can make various modifications that will achieve some of the advantages of the invention without departing from the true scope of the invention.
Claims (27)
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Also Published As
Publication number | Publication date |
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EP3381085A4 (en) | 2019-09-04 |
US11011853B2 (en) | 2021-05-18 |
US20170085006A1 (en) | 2017-03-23 |
US20210320427A1 (en) | 2021-10-14 |
WO2017078851A2 (en) | 2017-05-11 |
US11349223B2 (en) | 2022-05-31 |
WO2017078851A3 (en) | 2017-07-20 |
EP3381085A2 (en) | 2018-10-03 |
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