Additive manufacturing (AM) is a low-cost, high-accuracy manufacturing technique suitable for building complex antenna apertures. However, a major challenge of this technique is integrating a transition from an antenna element to a coaxial connector. This challenge is caused by a number of factors. For example, the structure of an additively manufactured device may be brittle and not as rugged as a machined metal antenna array structure. Thus, such device may not be able to accommodate conventional connectors designed for the machined metal antenna array structure. Moreover, the additively manufactured device is typically plated with a thin metal finish that may be easily damaged and cannot withstand soldering. These factors significantly complicate the integration of a connector to the additively manufactured device.
A conventional method of connector integration for an antenna aperture made by AM includes using conductive epoxy and zip ties to connect a radio frequency (RF) cable to an element of that aperture where solder cannot be used. Another method uses integrated printed circuit boards (PCBs) to integrate whole feed networks while providing a more suitable surface on which to solder a connector. However, these methods suffer from poor and/or unstable connections, high cost or high complexity.
Connectors are also a significant cost-driver in the development of antenna apertures. Yet, in most cases, connector integration is a permanent process that does not allow connectors and/or their associated components to be removed and/or reused.
Methods, systems and apparatuses are described herein that provide a novel, interlocking, snap-fit connection between an antenna aperture and a ground plane layer that contains coaxial connectors. The snap-fit design provides a simple and solderless transition from the connectors to the elements of the antenna aperture. This design facilitates easy assembly and disassembly, thereby allowing parts to be removed, reinstalled and/or reused.
In one embodiment, a modular solderless connector integration system for a conformal array is described. The system includes an opening formed on a ground plane; a flexible hook formed on the array, the array having a same geometrical shape as the ground plane layer, the hook being configured to be deflected to allow it to mate with the opening; and a transition assembly configured to transition an element of the array to a connector.
Optionally, the hook is configured to be deflected for insertion through the opening and be undeflected to securely attach the array to the ground plane layer.
Optionally, the hook enables of the array to be detached from the ground plane layer.
Optionally, the transition assembly comprises a conductive tube and a conductive element encased in a dielectric material.
Optionally, the transition assembly is integrated in at least one of the array or the ground plane layer.
Optionally, the connector is integrated in the ground plane layer.
Optionally, the conformal phased array is at least one of a planar phased array, a circular phased array, or a cylindrical phased array.
In another embodiment, a method of modular solderless connector integration for a conformal phased array is described. The method includes providing an opening on a ground plane layer; forming a flexible hook on the array, the array having a same geometrical shape as the ground plane layer, the hook being configured to be deflected to allow it to mate with the opening; and forming a transition assembly configured to transition an element of the array to a connector.
Optionally, the method includes integrating the transition assembly with the element, the transition assembly comprising a conductive tube and a conductive element encased in a dielectric material.
Optionally, the method includes integrating the connector with the ground plane layer.
Optionally, the method includes attaching the array to the ground plane layer via the hook.
Optionally, the method includes detaching the array from the ground plane layer via the hook.
Further features and advantages of the invention, as well as the structure and operation of various embodiments are described in detail below with reference to the accompanying drawings.
References in the specification to “one embodiment,” “an embodiment,” “an example embodiment,” etc., indicate that the embodiment described may include a particular feature, structure, or characteristic, but every embodiment may not necessarily include the particular feature, structure, or characteristic. Moreover, such phrases are not necessarily referring to the same embodiment. Further, when a feature, structure, or characteristic is described in connection with an embodiment, it is submitted that it is within the knowledge of one skilled in the art to effect such feature, structure, or characteristic in connection with other embodiments whether or not explicitly described.
In describing and claiming the disclosed embodiments, the following terminology will be used in accordance with the definition set forth below.
As used herein, the singular forms “a,” “an,” “the,” and “said” do not preclude plural referents, unless the content clearly dictates otherwise.
As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.
As used herein, the term “about” or “approximately” when used in conjunction with a stated numerical value or range denotes somewhat more or somewhat less than the stated value or range, to within a range of ±10% of that stated.
The radiation pattern reconfigurability offered cylindrical arrays makes them an attractive aperture for applications including ubiquitous radar, weather radar, and 5G millimeter wave communications systems. However, as with any conformal structure, manufacturing of cylindrical arrays comes with challenges not seen in traditional linear or planar apertures.
In embodiments, a system and method for modular solderless connector integration is described. This technique provides a simple, solderless transition from connectors to antenna elements of a conformal phased array by using flexible, interlocking hooks to securely fasten the array to a ground plane in a snap-fit manner. This snap-fit technique facilitates an easy assembly and disassembly process, allowing parts to be removed, reinstalled and/or reused (e.g., with other apertures of the same lattice spacing) to reduce costs. In addition, electrical continuity and tight tolerances are maintained over potentially long, thin excitation ports (holes) in an array that is 3D-printed. This technique eliminates concerns over stripping and/or damaging electroplating.
Also shown in
Array 102 may include flexible hooks 106 and 108 formed as protrusions on the back of array 102. Hooks 106 and 108 are designed to correspond to opening 110 of ground plane 104. Array 102 and ground plane 104 may have the same geometrical shape to allow array 102 to be securely attached to ground plane 104 via hooks 106 and 108. Alternatively, array 102 and ground plane 104 may be composed of one or more sections that have congruent geometrical shapes to enable the one or more sections of array 102 to be securely attached to the corresponding one or more sections of ground plane 104 via hooks 106 and 108. For example, hooks 106 and 108 may be deflected to allow them to mate with corresponding opening 110 on ground plane 104. Thus, during the assembly process, hooks 106 and 108 may be deflected slightly to pass through opening 110, and then be undeflected to their original shape (shown as 112 in
Hooks 106 and 108 may be formed from any suitable material with enough flexibility to enable them to be snap-fit attachment features. Such material may include any material suitable for the manufacturing process (e.g., AM) and may be deflected. In an embodiment, array 102, including hooks 106 and 108 may be additively manufactured using powdered nylon and then electroplated with a metal (e.g., copper) to provide conductivity. Hooks 106 and 108 may take on any form, such as cantilever, torsional and annular. Hooks 106 and 108 may serve as alternatives to screws and provide ease of assembly and no loose parts as they are integrally formed on array 102. While four cantilevered hooks are shown in
A transition assembly 114 configured to transition an element of array 102, such as element 118 to a connector 134 is further shown in
In an embodiment, array 102 may be additively manufactured as a single structure. In another embodiment, array 102 may be manufactured in modular sections that may be assembled together to form the complete array. The snap-fit technique is not limited to devices made by the AM process, although the snap-fit technique may be more applicable and/or beneficial to certain manufacturing methods and array designs than others.
In step 604, a flexible hook is provided on the array, the array having a same geometrical shape as the ground plane layer, the hook being configured to be deflected to allow it to mate with the opening. For example and in reference to
In step 606, a transition assembly configured to transition an element of the array to a connector is formed. As described above, transition assembly 114 of
In step 608, the array is attached to the ground plane layer via the hook. For example, as shown in
In step 610, the array is detached from the ground plane layer via the hook. For example and in referenced to
The example embodiments described herein are provided for illustrative purposes and are not limiting. The examples described herein may be adapted to any type of targeted crawling system. Further structural and operational embodiments, including modifications/alterations, will become apparent to persons skilled in the relevant art(s) from the teachings herein.
While various embodiments of the disclosed subject matter have been described above, it should be understood that they have been presented by way of example only, and not limitation. Various modifications and variations are possible without departing from the spirit and scope of the embodiments as defined in the appended claims. Accordingly, the breadth and scope of the disclosed subject matter should not be limited by any of the above-described exemplary embodiments, but should be defined only in accordance with the following claims and their equivalents.
This Application claims the benefit of U.S. Provisional Application No. 62/845,008 filed on May 8, 2019, the entirety of which is incorporated herein by reference.
The United States Government has ownership rights in this invention. Licensing inquiries may be directed to Office of Technology Transfer, US Naval Research Laboratory, Code 1004, Washington, DC 20375, USA; +1.202.767.7230; techtran@nrl.navy.mil, referencing Navy Case #111111-US2.
Number | Date | Country | |
---|---|---|---|
62845008 | May 2019 | US |