An electromagnetically operational micro-truss structure and methods are disclosed. A micro-truss structure comprises a grid of interlocking elements, and a metallic coating selectively coats the grid. The metallic coating is configured to resonate an electromagnetic energy.

FIELD

Embodiments of the present disclosure relate generally to antennas. More particularly, embodiments of the present disclosure relate to antenna structures.

BACKGROUND

Current microwave and millimeter-wave frequency antennas generally comprise cumbersome structures such as waveguides, dish antennas, helical coils, horns, and other large non-conformal structures. Communication applications where at least one communicator is moving and radar applications generally require a steerable beam and/or steerable reception. Phased array antennas are particularly useful for beam steered applications since beam steering can be accomplished electronically without physical motion of the antenna. Such electronic beam steering can be faster and more accurate and reliable than gimbaled/motor-driven mechanical antenna steering.

SUMMARY

An electromagnetically operational micro-truss structure and methods are disclosed. A micro-truss structure comprises a grid of interlocking elements, and a metallic coating selectively coats the grid. The metallic coating is configured to resonate an electromagnetic energy.

In this manner, the electromagnetically operational micro-truss structure may be formed into various shapes operable to bear structural weight and provide, for example but without limitation, an antenna, a conformal antenna, a holographic antenna, a frequency selective surface, or other electromagnetic device.

In an embodiment, an electromagnetically operational micro-truss structure comprises a micro-truss structure and a metallic coating. The micro-truss structure comprises a grid of interlocking elements, and the metallic coating selectively coats the grid. The metallic coating is configured to resonate an electromagnetic energy.

In another embodiment, a method for operation of an electromagnetically operational micro-truss structure uses a micro-truss structure comprising a grid of interlocking elements selectively coated with a metallic coating. The method further resonates an electromagnetic energy using the metallic coating.

In a further embodiment, a method for providing an electromagnetically operational micro-truss structure provides a micro-truss structure comprising a grid of interlocking elements. The method further selectively coats the grid with a metallic coating, and configures the metallic coating to resonate an electromagnetic energy.

DETAILED DESCRIPTION

The following detailed description is exemplary in nature and is not intended to limit the disclosure or the application and uses of the embodiments of the disclosure. Descriptions of specific devices, techniques, and applications are provided only as examples. Modifications to the examples described herein will be readily apparent to those of ordinary skill in the art, and the general principles defined herein may be applied to other examples and applications without departing from the spirit and scope of the disclosure. The present disclosure should be accorded scope consistent with the claims, and not limited to the examples described and shown herein.

Embodiments of the disclosure may be described herein in terms of functional and/or logical block components and various processing steps. It should be appreciated that such block components may be realized by any number of hardware, software, and/or firmware components configured to perform the specified functions. For the sake of brevity, conventional techniques and components related to antennas, micro-truss structures, and other functional aspects of systems described herein (and the individual operating components of the systems) may not be described in detail herein. In addition, those skilled in the art will appreciate that embodiments of the present disclosure may be practiced in conjunction with a variety of hardware and software, and that the embodiments described herein are merely example embodiments of the disclosure.

Embodiments of the disclosure are described herein in the context of a practical non-limiting application, namely, a conformal antenna and frequency selective filter that can be meld into a vehicle structure of a vehicle. The vehicle may comprise, for example but without limitation, an unmanned aerial vehicles (UAVs), a piloted aircraft (e.g., a fixed wing or a rotorcraft), a satellite, a ship, a boat, a submarine, a surface vehicle (e.g., an automobile), a robotic vehicle, an autonomous robotic vehicle, or other vehicle. Embodiments of the disclosure, however, are not limited to such conformal antenna and frequency selective filter applications, and the techniques described herein may also be utilized in other applications. For example but without limitation, embodiments may be applicable to radomes, shielding, or other application.

As would be apparent to one of ordinary skill in the art after reading this description, the following are examples and embodiments of the disclosure and are not limited to operating in accordance with these examples. Other embodiments may be utilized and structural changes may be made without departing from the scope of the exemplary embodiments of the present disclosure.

Embodiments of the disclosure provide an electromagnetically operational micro-truss structure operable to resonate an electromagnetic energy. The electromagnetically operational micro-truss structure comprises a micro-truss structure comprising a grid of interlocking elements, and a metallic coating selectively coating the grid. As mentioned above, the electromagnetically operational micro-truss structure may be formed into various shapes to provide, for example but without limitation, an antenna operable to bear structural weight, a conformal antenna, a holographic antenna, frequency selective surface, or other electromagnetic device.

FIG. 1is an illustration of an exemplary electromagnetically operational micro-truss structure (structure100) according to an embodiment of the disclosure. The structure100comprises a micro-truss structure102and a metallic coating104.

The micro-truss structure102comprises a structural grid of interlocking elements (e.g., truss member212inFIG. 2). The micro-truss structure102provides a high-impedance surface upon which the metallic coating104is applied. The micro-truss structure102may comprise a non-metallic material such as, but without limitation, a plastic, a composite, a ceramic, a polymer, or other non-metallic material.

The metallic coating104is coupled to the micro-truss structure102. The metallic coating104may be applied to the micro-truss structure102by various methods comprising, for example but without limitation, partial metallization by sputter deposition with a mask, electroless plating, a paint dip, or other method for coating a surface.

A holographic antenna can be created by making a conformal antenna by guiding surface waves along a periodically varying high-impedance surface comprising the high-impedance surface provided by the micro-truss structure102. A partial metallization of the micro-truss structure102creates the structure100as a high-impedance structure comprising a periodic array of metallic bent crosses106coated by the metallic coating104in the structure100that is capable of supporting a surface wave. A size of each of the metallic bent crosses106can be varied to create the holographic antenna as explained in more detail below. When integrated into terrestrial or aerospace vehicle structures, the structural antenna100can increase design flexibility, decrease weight and increase strength. Embodiments of the disclosure can also be used to integrate structural antennas into complex shapes, thus increasing design flexibility.

FIG. 2is an illustration of an exemplary side view200and top view210of the structure100ofFIG. 1according to an embodiment of the disclosure. In the side view200, the micro-truss structure102is coated by the metallic coating104(FIG. 1) at locations such as a first location202and a second location204. The micro-truss structure102is transformed into an electromagnetically resonating structure such as a structural holographic antenna by selectively and partially coating truss members such as a truss member212with a metal at locations such as the first location202and the second location204. In the top view210, the micro-truss structure102is coated by the metallic coating104at locations such as a third location206and a fourth location208.

FIG. 3is an illustration of an exemplary conformal antenna300(structural antenna300) formed from the electromagnetically operational micro-truss structure100ofFIG. 1according to an embodiment of the disclosure. A light region302and a dark region304shown on the structural antenna300correspond to areas where the metallic coating104extends over smaller and larger portions of the micro-truss structure102respectively.

The conformal antenna300comprises a patterning of a metallic coating104of the structure100. When truss members such as the truss member212are uniformly coated as shown inFIG. 1, the metallic coating104forms a periodic array of metallic bent crosses106(FIG. 1) that act as the high-impedance surface mentioned above and is capable of supporting surface-wave transmission at a propagation surface wave number determined by a period of a relative size of the metallic bent crosses106of the micro-truss structure102. In general, a wavelength of a propagating surface wave decreases with a size of each of the metallic bent crosses106relative to the micro-truss period of the periodic array. A relative size of each of the metallic bent crosses106is determined by an amount of metallization applied locally to the micro-truss structure102.

A holographic antenna is typically designed by applying a pattern to a surface wave propagation index nsw(x) locally according to a specific formula designed to create a radiation pattern peaked at a desired frequency f, and angle θ0. Such a formula can take a following form for the surface wave propagation index:
nsw(x)=n0+δncos(kpx); wherekp=2πf/c(n0−sin(θ0))  (1)

where n0is a mean surface-wave index, δn is a modulation amplitude of the surface-wave index, and c is the speed of light.

When a functional dependence of the surface-wave propagation index nsw(x) relative to the size of each of the bent crosses106is known, an antenna such as the conformal antenna300can be designed into the structure100according to Eqn. (1).

According to an embodiment, the structural antenna300can be used to meld antennas into a vehicle structure. The structural antenna300provides design flexibility, reduced weight and increased strength, and can be easily formed into shapes with complex curvature. When used on an aircraft, embodiments of the disclosure offer advantages in that a size of an antenna aperture is less constrained, and may be as large as or larger than wings and fuselage of an aircraft.

Some existing antennas incorporate an exciting element such as a slot aperture into a structure, with a disadvantage that the structure must be modified with an aperture, and a radiation pattern is determined by a geometry of the structure. In contrast, according to embodiments of the disclosure, a radiation pattern is tailored to suit an application by tailoring shapes and patterns of the partial metallization in the structure100.

FIG. 4is an illustration of an exemplary multilayer electromagnetically operational micro-truss structure400(structure400) according to an embodiment of the disclosure. The structure400comprises a micro-truss structure402, a first metal coated layer404and a second metal coated layer406(layers404/406). The structure400may be configured to comprise a structural frequency selective surface whose geometry filters electromagnetic radiation. The structure400can be configured as a frequency selective surface by directly writing a metallic pattern on a surface of the structure100(FIG. 1). In this manner, the structure400may also be referred to as a frequency selective surface400herein.

The micro-truss structure402can be transformed into a structural frequency selective surface by selectively and partially coating truss members such as the truss member212with metal as explained in the context of discussion ofFIG. 1. The partial metallization creates the periodic array of the metallic bent crosses106(FIG. 1) in the micro-truss structure402that enables frequency selectivity. In some embodiments, a single layer such as the first layer404may be used to form a frequency selective surface on the micro-truss structure402.

In some embodiments, multiple layers such as the first layer404and the second layer406may be used to form a frequency selective surface on the micro-truss structure402. For example, the first layer404may comprise a higher pass filter with a first cutoff frequency, and the second layer406may comprise a low pass filter with a second cutoff frequency higher than the first cutoff frequency. Thereby, the first layer404and the second layer406may comprise a band pass filter. A frequency selective surface may employ a band pass filter for frequency selectivity.

FIG. 5is an illustration of an exemplary flowchart showing a process500for operating an electromagnetically operational micro-truss structure according to an embodiment of the disclosure. The various tasks performed in connection with process500may be performed mechanically, by software, hardware, firmware, a computer-readable medium having computer executable instructions for performing the processes methods, or any combination thereof. For illustrative purposes, the following description of the process500may refer to elements mentioned above in connection withFIGS. 1-4.

It should be appreciated that the process500may include any number of additional or alternative tasks, the tasks shown inFIG. 5need not be performed in the illustrated order, and the process500may be incorporated into a more comprehensive procedure or process having additional functionality not described in detail herein. In practical embodiments, portions of the process500may be performed by different elements of the structure100,400and the structural antenna300such as: the micro-truss structure102and the metallic coating104the, etc. Process500may have functions, material, and structures that are similar to the embodiments shown inFIGS. 1-4. Therefore, common features, functions, and elements may not be redundantly described here.

Process500may begin by using a micro-truss structure such as the micro-truss structure102comprising a grid of interlocking elements such as a truss member212selectively coated with a metal coating such as the metallic coating104(task502).

Process500may continue by providing structural support using the micro-truss structure102(task504).

Process500may continue by resonating an electromagnetic energy using the metallic coating104(task506).

Process500may continue by radiating electromagnetic energy from the metallic coating104(task508). Thereby, the metallic coating104and the micro-truss structure102function as an antenna such as the structural antenna300.

Process500may continue by filtering electromagnetic radiation using the metallic coating104(task510). Thereby, the metallic coating104and the micro-truss structure102function as a frequency selective surface such as the frequency selective surface400.

Process500may continue by radiating electromagnetic energy from each of a plurality of layers of the metallic coating104such as the layers404/406, wherein each of the layers404/406radiates in a respective frequency band (task512).

Process500may continue by reflecting electromagnetic radiation from each of the layers404/406, wherein each of the layers404/406reflects a respective frequency band (task514).

FIG. 6is an illustration of an exemplary flowchart showing a process600for providing an electromagnetically operational micro-truss structure according to an embodiment of the disclosure. The various tasks performed in connection with the process600may be performed mechanically, by software, hardware, firmware, a computer-readable medium having computer executable instructions for performing the processes methods, or any combination thereof. For illustrative purposes, the following description of the process600may refer to elements mentioned above in connection withFIGS. 1-4.

It should be appreciated that the process600may include any number of additional or alternative tasks, the tasks shown inFIG. 6need not be performed in the illustrated order, and the process600may be incorporated into a more comprehensive procedure or process having additional functionality not described in detail herein. In practical embodiments, portions of the process600may be performed by different elements of the structure100,400and the antenna structure300such as: a micro-truss structure102and a metallic coating104etc. Process600may have functions, material, and structures that are similar to the embodiments shown inFIGS. 1-4. Therefore, common features, functions, and elements may not be redundantly described here.

Process600may begin by providing a micro-truss structure such as the micro-truss structure102comprising a grid of interlocking elements such as a truss member212(task602).

Process600may continue by coating selectively the grid with a metallic coating such as the metallic coating104(task604).

Process600may continue by configuring the metallic coating104to resonate an electromagnetic energy (task606).

Process600may continue by configuring the metallic coating104to comprise an antenna such as the structural antenna300(task608).

Process600may continue by configuring the metallic coating104to comprise a frequency selective surface such as the frequency selective surface400(task610).

Process600may continue by configuring each of a plurality of layers such as the layers404/406to reflect a respective frequency band, wherein the metallic coating comprises the layers404/406(task612).

Process600may continue by configuring each of the layers404/406to radiate in a respective frequency band (task614).

In this manner, embodiments of the disclosure provide an electromagnetically operational micro-truss structure that may be formed into various shapes to provide, for example but without limitation, an antenna operable to bear structural weight, a conformal antenna, a holographic antenna, a frequency selective surface, or other electromagnetic devices. Conventional methods may be difficult to incorporate into complex curvatures where design, manufacture and maintenance costs increase with shape complexity. Embodiments of the disclosure are a significant departure in that the structure is the antenna or is the frequency-selective surface, unlike existing methods where an antenna or frequency selective surface are a conventional separate device from a structure.

In this document, the terms “computer program product”, “computer-readable medium”, “computer readable storage medium”, and the like may be used generally to refer to media such as, for example, memory, storage devices, or storage unit. These and other forms of computer-readable media may be involved in storing one or more instructions for use by a controller to cause the controller to perform specified operations. Such instructions, generally referred to as “computer program code” or “program code” (which may be grouped in the form of computer programs or other groupings), when executed, enable a method for electromagnetic operation of the micro-truss structure100.

Terms and phrases used in this document, and variations thereof, unless otherwise expressly stated, should be construed as open ended as opposed to limiting. As examples of the foregoing: the term “including” should be read as meaning “including, without limitation” or the like; the term “example” is used to provide exemplary instances of the item in discussion, not an exhaustive or limiting list thereof; and adjectives such as “conventional,” “traditional,” “normal,” “standard,” “known” and terms of similar meaning should not be construed as limiting the item described to a given time period or to an item available as of a given time, but instead should be read to encompass conventional, traditional, normal, or standard technologies that may be available or known now or at any time in the future.

Likewise, a group of items linked with the conjunction “and” should not be read as requiring that each and every one of those items be present in the grouping, but rather should be read as “and/or” unless expressly stated otherwise. Similarly, a group of items linked with the conjunction “or” should not be read as requiring mutual exclusivity among that group, but rather should also be read as “and/or” unless expressly stated otherwise. Furthermore, although items, elements or components of the disclosure may be described or claimed in the singular, the plural is contemplated to be within the scope thereof unless limitation to the singular is explicitly stated. The presence of broadening words and phrases such as “one or more,” “at least,” “but not limited to” or other like phrases in some instances shall not be read to mean that the narrower case is intended or required in instances where such broadening phrases may be absent.

As used herein, unless expressly stated otherwise, “operable” means able to be used, fit or ready for use or service, usable for a specific purpose, and capable of performing a recited or desired function described herein. In relation to systems and devices, the term “operable” means the system and/or the device is fully functional and calibrated, comprises elements for, and meets applicable operability requirements to perform a recited function when activated. In relation to systems and circuits, the term “operable” means the system and/or the circuit is fully functional and calibrated, comprises logic for, and meets applicable operability requirements to perform a recited function when activated.