The present invention relates to electromagnetic radomes and, more specifically, to wideband radomes for use at radio frequencies (RF) as well as microwave and millimeter-wave frequencies.
A radome is a structural enclosure that protects an antenna. Radomes are typically constructed of material that minimally attenuates the electromagnetic (EM) signal transmitted or received by the antenna. In other words, the radome is transparent to radar or radio waves. Radomes also protect the antenna surfaces from weather and conceal antenna electronic equipment from public view. Radomes can be constructed in several shapes (spherical, geodesic, planar, etc.) depending upon the particular application using various construction materials (fiberglass, PTFE-coated fabric, etc.). When provided on found on fixed-wing aircraft with forward-looking radar, radomes may be provided as nose cone sections of the fuselage.
A simple radome structure may be a uniform slab of material of thickness nλ/2 (where n is an integer) and λ=λvac/√(∈R).
Such radomes perform well at a single frequency, but are narrowband unless ∈R≈1 and fragile at millimeter-wave frequencies if n=1. Wideband performance typically requires a multilayer structure in which the dielectric constant and thickness of each layer are chosen to optimize performance. Examples of multilayer radome structures include, but are not limited to, A-sandwich structures where a low dielectric layer is sandwiched between two high dielectric layers and B-sandwich structures where a high dielectric layer is sandwiched between two low-dielectric layers.
According to one embodiment of the present invention, a monolithic, wideband, millimeter-wave radome is provided. The radome includes a solid layer formed of a single material and a single lattice layer formed of the single material and disposed on an exterior surface of the solid layer. The lattice layer includes void regions formed from selective omission of the single material during latticelayer buildup.
According to another embodiment, a monolithic, wideband, millimeter-wave radome is provided and includes multiple solid layers formed of a single material and multiple lattice layers formed of the single material and disposed on respective exterior surfaces of corresponding ones of the multiple solid layers. Each of the multiple lattice layers includes void regions formed from selective omission of the single material during lattice layer buildups.
According to another embodiment, a monolithic, wideband, millimeter-wave radome fabrication method is provided. The method includes laying down a single material in a layer-by-layer and side-to-side pattern to form a solid layer and laying down the single material in a layer-by-layer and side-to-side pattern to form a lattice layer on an exterior surface of the solid layer. The laying down of the single material to form the lattice layer includes selectively omitting the single material during buildup of the lattice layer to develop void regions therein.
Additional features and advantages are realized through the techniques of the present invention. Other embodiments and aspects of the invention are described in detail herein and are considered a part of the claimed invention. For a better understanding of the invention with the advantages and the features, refer to the description and to the drawings.
The subject matter which is regarded as the invention is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the invention are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
Conventional radome fabrication approaches become difficult to apply at millimeter-wave frequencies because tolerance requirements become increasingly difficult to meet as the effective wavelength of the electromagnetic (EM) radiation passing through radomes decreases. Additive manufacturing, however, with its ability to build three-dimensional structures at low cost via precise sequential deposition of material, offers a solution and opens a realm of new possibilities in radome design.
For example, with reference to
While the radome 1 performs well and demonstrates the potential of additive manufacturing for radome applications, its mechanical strength can be increased. One way to increase the mechanical strength is by increasing the thickness of the radome 1 material at either the cylindrical sidewall 2 or the semi-spherical section 3. Doing so will allow for insertion loss to remain small near the center of the design band as long as the thickness of the radome 1 is an integral number of half-wavelengths but it is to be understood that a consequence of increased radome 1 thickness is decreased bandwidth. Thus, an alternate option for increasing a strength characteristic of a given radome without sacrificing bandwidth or electrical performance relies on the formation of a multilayer radome structure.
Thus, with reference to
The single lattice layer 12 has a relatively low dielectric constant and is formed of the single material. The single lattice layer 12 is disposed on an uppermost surface 110 of the first single and solid layer 11 such that a lowermost surface 120 of the single lattice layer 12 is non-adhesively bonded to the uppermost surface 110. The second single and solid layer 13 has a relatively high dielectric constant and is formed of the single material. The second single and solid layer 13 is disposed on an uppermost surface 121 of the single lattice layer 12 such that a lowermost surface 130 of the second single and solid layer 13 is non-adhesively bonded to the uppermost surface 121.
As used herein, the term “non-adhesively bonded” refers to any bonding between a layer of the single material and another layer of the single material that is generated by FDM or another suitable additive manufacturing process.
The single lattice layer 12 includes solid regions 121 and void regions 122 that are interspersed among the solid regions 121. The void regions 122 are formed from selective omission of the single material during buildup processes of the single lattice layer 12 such that the single lattice layer 12 has an effective dielectric constant ∈eff approximated by:
∈eff=f∈R+(1−f)∈void,
where ∈R is a dielectric constant of the first and second single and solid layers 11 and 13, ∈void is a dielectric constant of the void regions and f is a volume fill fraction of the single material in the single lattice layer 12.
The monolithic, wideband, millimeter-wave radome 10 of
That is, if the single material has the dielectric constant ∈R and the void regions have the dielectric constant ∈void (typically ∈void=1 for air-filled voids), the desired dielectric constant for the lattice ∈eff can be approximated by a weighted average of the two dielectric constants;
where f is the volume fill fraction of the single material within the single lattice layer 12. Therefore, in an exemplary case, if ∈R=3, ∈void=1 and ∈lattice=1.25 is desired, the volume fill fraction of the single material within the single lattice layer 12 is 0.125. In other words, the single lattice layer 12 has the desired effective dielectric constant ∈lattice of 1.25 by the selective omission of 87.5% of the single material during the buildup of the single lattice layer 12.
With reference to
The rectangular-lattice structure of the single lattice layer 12 may be constructed using the formation of square beams that are about 25 mils on a side (rectangular and annular beams may also be used). The square beams include vertically oriented beams 30 and horizontally oriented beams 31 that cooperatively form the solid regions 121. The vertically oriented beams 20 may be arranged on their respective sides in a non-abutting front-to-back array. The horizontally oriented beams 31 are supported along the vertical lengths of the vertically oriented beams 30 at vertical distances from one another. As such, the spaces between adjacent vertically oriented beams 30 and proximal horizontally oriented beams 31 define the void regions 122.
By way of clarity,
Of course, it is to be understood that many lattice geometries are possible for the single lattice layer 12 besides the rectangular lattice illustrated in
As shown in
With such construction, if a diameter of the first and second cylindrical beams 40 and 41 is D and the beam-to-beam separation in each sub-layer of first and second cylindrical beams 40 and 41 is S, the volume fill factor of the “woodpile” lattice structure is:
Thus, if the single material used to form the “woodpile” lattice structure is Ultem™ 9085 or another similar low-loss dielectric for which ΣR=2.49 and tan δ=0.006, an effective lattice dielectric constant of ∈lattice=1.5 requires a fill factor of approximately 33% (f=0.33). Therefore, if the diameter of the first and second cylindrical beams 40 and 41 is 20 mils, the required beam-to-beam separation is S=47 mils. Exemplary thicknesses for the first and second single and solid layers 11 and 13 of 48 and 94 mils, respectively, may then be chosen to minimize insertion losses across a 71-86 GHz operating band. The calculated insertion loss for the radome 10 in the embodiment of
As shown in
While the radome 10 described above is provided as an A-sandwich type of structure it is to be understood that other embodiments exist. In particular, it is to be understood that the radome 10 described above can be formed with a B-sandwich type of structure and/or with a flat or complex geometry such as the geometry of the radome 1 of
For example, with reference to
As another example, with reference to
As yet another example, with reference to
While a material, such as Ultem 9085 can be used for a low- to moderate-speed nose-mounted radome or for a window/radome for a sensor or telemetry/communication antenna on a different part of the missile body where the mechanical/thermal environment is more benign, other materials may be used for a nose-mounted supersonic missile radome. Furthermore, this technology can be extended to lower frequencies for use with a single wideband sensor or as a common window for use with multiple sensors having a wide range of operating frequencies. For example, there may be wideband performance potential of this technology for frequencies below W-band (e.g., for frequencies between 100 MHz and 40 GHz) where a rectangular lattice structure of the single lattice layer 12 include 40 mil by 40 mil beams with a lattice period of 120 mils to realize a low-dielectric lattice with ∈lattice=1.5. Insertion loss for this structure may be less than 1 dB from very low frequencies to 40 GHz over a wide range of incident angles.
Any one or more of the radomes described above may be provided for use as an affordable millimeter-wave radome for low-speed aircraft (e.g., UAVs). Such radomes would have low reflection and transmission losses over a wide bandwidth and adequate mechanical strength for the expected flight regimes of the low-speed aircraft.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one more other features, integers, steps, operations, element components, and/or groups thereof.
The corresponding structures, materials, acts and equivalents of all means or step plus function elements in the claims below are intended to include any structure, material or act for performing the function in combination with other claimed elements as claimed. The description of the present invention has been presented for purposes of illustration and description, but is not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the invention. The embodiments were chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
While embodiments have been described, it will be understood that those skilled in the art, both now and in the future, may make various improvements and enhancements which fall within the scope of the claims which follow. These claims should be construed to maintain the proper protection for the invention first described.