The present disclosure relates to low-K materials for use in radio frequency applications and more particularly to additively manufactured periodic structures for use in radomes and other radio frequency applications.
Specialized materials, such as syntactic foams, are used in a host of commercial and military radio frequency (RF) applications as a structural or semi-structural element. Very commonly these materials are used to provide mechanical support while remaining transparent to the RF radiation being transmitted or received. These materials are commonly used in RF antenna radomes and other RF beam-shaping devices. What makes these materials ideal for these applications is the fact that they have very low permittivity (e.g. “Low-K”) and low loss. However, these materials often start out as a powder and must undergo a series of labor-intensive and costly processes to be formed into the final complex shape needed for these RF applications.
Wherefore it is an object of the present disclosure to overcome the above- mentioned shortcomings and drawbacks associated with conventional low-K materials for use in radio frequency applications, such as syntactic foams.
One aspect of the present disclosure is a method of manufacturing periodic structures to achieve effective low-k and low loss materials in radio frequency applications comprising: providing a layer of bulk material; providing a subsequent layer of bulk material onto the layer of bulk material; bonding the layer of bulk material to the subsequent layer of bulk material using additive manufacturing methods; and repeating the process to form a three-dimensional component comprising a lattice and having an overall dielectric constant that is lower than that of the bulk material.
One embodiment of the method of manufacturing periodic structures to achieve effective low-k and low loss materials in radio frequency applications is wherein the lattice comprises repeating unit cells.
Another embodiment of the method of manufacturing periodic structures to achieve effective low-k and low loss materials in radio frequency applications is wherein the additive manufacturing method is stereolithography. In some cases, the bulk material further comprises a dopant.
In certain embodiments, the component is a radome and/or antenna aperture. In some cases, the periodic structure further comprises a spatial gradient.
Another aspect of the present disclosure is a periodic structure for use in radio frequency applications comprising: a three-dimensional component manufactured using additive manufacturing comprising a lattice and having a dielectric constant that is lower than that of a bulk material used to manufacture the component.
One embodiment of the periodic structure for use in radio frequency applications is wherein the lattice comprises repeating unit cells. In some cases, the method of additive manufacturing is stereolithography.
Another embodiment of the periodic structure for use in radio frequency applications is wherein the bulk material further comprises a dopant. In certain embodiments, the component is a radome. In some cases, the periodic structure further comprises a gradient.
These aspects of the disclosure are not meant to be exclusive and other features, aspects, and advantages of the present disclosure will be readily apparent to those of ordinary skill in the art when read in conjunction with the following description, appended claims, and accompanying drawings.
The foregoing and other objects, features, and advantages of the disclosure will be apparent from the following description of particular embodiments of the disclosure, as illustrated in the accompanying drawings in which like reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the disclosure.
A radome is a structural, weatherproof enclosure that protects a radar antenna. A radome is generally constructed of material that minimally attenuates the electromagnetic signal transmitted or received by the antenna, so as to be effectively transparent to radio waves. In one embodiment of the present disclosure, additive manufacturing is used to create complex shapes necessary for such application with an inexpensive automated process. However, current materials used in additive manufacturing do not have the required RF material properties (i.e., low-K) in their bulk form as compared to traditional syntactic foams to allow for direct replacement of the traditional low-K materials.
Thus, in certain embodiments of the present disclosure additive manufacturing allows for the direct fabrication of very complex geometries such as uniform and non-uniform (i.e. gradient) periodic lattice structures. By carefully engineering these complex lattice structures, being largely comprised of air, the arbitrarily shaped RF components can be fabricated such that they possess effective material properties that are custom tuned and dissimilar from the properties of the host bulk material while remaining mechanically robust.
In some cases, unit cell sizes and the geometry of the periodic structure are engineered to achieve the desired wave propagation characteristics for the specific frequencies of operation. It is also worth noting that the addition of various RF-relevant dopant materials to the 3D-printable bulk material may significantly extend the effective RF material properties for a resultant structure leading to a variety of other new applications. For example, the addition of carbon-based dopants (e.g. dispersed carbon nanotubes) into a 3D-printable host material could have significant advantages in RF absorbing applications (e.g. superior anechoic chamber design). Additionally, the use of high-dielectric ceramic materials, in powder form, could be doped into the 3D-printable host material at specific concentrations to fine-tune the effective properties of the cellular lattice structure or extend the operating range.
The solution of the present disclosure is superior to traditional uses of low-K RF foam materials because it is fabricated in a single automated process and hence could have significant advantages in material costs, labor costs, system performance and manufacturing time in addition to being customizable for specific applications. In essence, the described method offers access to a continuous range of material properties that are not offered on the commercial market.
Referring to
Referring to
Referring to
Referring to
One aspect of the present disclosure is to take advantage of additive manufacturing's ability to generate extraordinarily complex 3-dimensional geometries to create engineered material property behavior unavailable in today's commercially-available market. One opportunity is to eliminate the need for low dielectric foam as a mechanically structural, “RF-transparent” material. Use of 3-dimensional periodic lattice structures of appropriate unit cell size, based on required RF performance, to define volume fraction of bulk material-to-air ratio in order to achieve low overall dielectric constant and loss while maintaining required structural integrity and mechanical support is one benefit of the present disclosure. In one embodiment, tuning geometric parameters could achieve RF properties along a continuous spectrum from bulk material to very near air.
Additive manufacturing methods are numerous and include, but are not limited to vat photopolymerization methods, material extrusion methods, material jetting methods, binder jetting methods, power bed fusion methods, direct energy deposition methods, sheet lamination, and the like. It is understood that the method of additive manufacturing chosen is based, in part, on the bulk material and other properties needed for a particular RF application.
Referring to
Referring to
Referring to
Referring to
What takes a technician about eight hours to produce using current techniques will only requires about a five minute assembly step according to the principles of the present disclosure, as the radome 120 and the skin 110 can be manufactured using additive manufacturing as a single part with no required tooling. Depending on several aspects including, but not limited to, the lattice structure chosen, the bulk material used, any dopants present, and the like, a low-K radome can be manufactured in a very short time, all while having superior application-specific properties (e.g., Low-K, absorbing, etc.). Further, the entire radome can be manufactured in a single piece despite the complexity of the shape needed for the particular application. Once the radome is manufactured the RF antenna array is simply inserted into the radome using standard fastening or bonding techniques.
Referring to
Referring to
Referring to
In certain embodiments, the bulk material used may introduce some absorption of RF signals, but not scattering. In certain cases, the loss for the RF component is tunable based on the selection of bulk material. In some cases, the loss for the RF component is tunable based on the lattice structure chosen. In some embodiments, the component will be designed using materials with particular dielectric constants, unit cells, lattice structures, volume fractions, and the like.
In some cases, low loss, low dielectric structures for use in RF, radome and impedance matching applications will lend themselves to the use of gradients. In some cases, a high dielectric value near the antenna might taper off to a dielectric similar to air at the extent of the radome. In these cases, the gradient could be manufactured to significantly reduce loss and backscattering as compared to discrete interfaces between different regions in a traditional method.
While various embodiments of the present invention have been described in detail, it is apparent that various modifications and alterations of those embodiments will occur to and be readily apparent to those skilled in the art. However, it is to be expressly understood that such modifications and alterations are within the scope and spirit of the present invention, as set forth in the appended claims. Further, the invention(s) described herein is capable of other embodiments and of being practiced or of being carried out in various other related ways. In addition, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including,” “comprising,” or “having,” and variations thereof herein, is meant to encompass the items listed thereafter and equivalents thereof as well as additional items while only the terms “consisting of and “consisting only of are to be construed in a limitative sense.
The foregoing description of the embodiments of the present disclosure has been presented for the purposes of illustration and description. It is not intended to be exhaustive or to limit the present disclosure to the precise form disclosed. Many modifications and variations are possible in light of this disclosure. It is intended that the scope of the present disclosure be limited not by this detailed description, but rather by the claims appended hereto.
A number of implementations have been described. Nevertheless, it will be understood that various modifications may be made without departing from the scope of the disclosure. Although operations are depicted in the drawings in a particular order, this should not be understood as requiring that such operations be performed in the particular order shown or in sequential order, or that all illustrated operations be performed, to achieve desirable results.
While the principles of the disclosure have been described herein, it is to be understood by those skilled in the art that this description is made only by way of example and not as a limitation as to the scope of the disclosure. Other embodiments are contemplated within the scope of the present disclosure in addition to the exemplary embodiments shown and described herein. Modifications and substitutions by one of ordinary skill in the art are considered to be within the scope of the present disclosure.
This disclosure was made with United States Government support under Contract No. 6533773795 awarded by the Department of the Navy. The United States Government has certain rights in this disclosure.