In some applications, ultra-wide band antennas are needed to operate over a large field-of-view (FOV) in both azimuth and elevation directions. The typical bicone or monocone antenna does not provide a sufficient FOV particularly at higher elevations because the pattern is strongly influenced by a null at the apex (vertical direction).
In an illustrative embodiment, an ultra-wideband antenna is provided. The antenna includes, but is not limited to, a cone shaped ground element and a radiating element. The cone shaped ground element includes, but is not limited to, a first vertex region and an aperture formed through the first vertex region. The cone shaped ground element is configured to form an electrical ground. The radiating element includes, but is not limited to, a cone shaped radiator and a spherical shaped radiator. The cone shaped radiator includes, but is not limited to, a second vertex region that is electrically connectable to a feed element mounted through the aperture of the cone shaped ground element. The spherical shaped radiator is mounted to the cone shaped radiator opposite the second vertex region.
In another illustrative embodiment, an ultra-wideband antenna is provided. The antenna includes, but is not limited to, a cone shaped ground element, a radiating element, and a spacer. The cone shaped ground element includes, but is not limited to, a first vertex region and an aperture formed through the first vertex region. The cone shaped ground element is configured to form an electrical ground. The radiating element includes, but is not limited to, a cone shaped radiator and a spherical shaped radiator. The cone shaped radiator includes, but is not limited to, a second vertex region that is electrically connected to a feed element mounted through the aperture of the cone shaped ground element. The spherical shaped radiator is mounted to the cone shaped radiator opposite the second vertex region. The spacer is mounted to the cone shaped ground element and to the radiating element and configured to maintain a spacing between the cone shaped ground element and the radiating element.
In yet another illustrative embodiment, an ultra-wideband antenna is provided. The antenna includes, but is not limited to, a feed element, a cone shaped ground element, and a radiating element. The cone shaped ground element includes, but is not limited to, a first vertex region and an aperture formed through the first vertex region. The cone shaped ground element is configured to form an electrical ground. The radiating element includes, but is not limited to, a cone shaped radiator and a spherical shaped radiator. The cone shaped radiator includes, but is not limited to, a second vertex region that is electrically connected to the feed element mounted through the aperture of the cone shaped ground element. The spherical shaped radiator is mounted to the cone shaped radiator opposite the second vertex region.
Other principal features of the disclosed subject matter will become apparent to those skilled in the art upon review of the following drawings, the detailed description, and the appended claims.
Illustrative embodiments of the disclosed subject matter will hereafter be described referring to the accompanying drawings, wherein like numerals denote like elements.
With reference to
Cone shaped radiator 108 may include a vertex region 112 that is electrically connected to feed element 106. Spherical shaped radiator 110 is mounted to cone shaped radiator 108 opposite vertex region 112 along a transition region 114.
Cone shaped radiator 108 and spherical shaped radiator 110 may be formed of any conducting material suitable for forming a radiator of antenna 100. For example, cone shaped radiator 108 and spherical shaped radiator 110 may be formed of a metallic material such as copper, brass, etc. as understood by a person of skill in the art. Cone shaped radiator 108 and spherical shaped radiator 110 may be formed of the same or different materials.
Cone shaped ground element 104 may include a vertex region 116 and an aperture 404 (shown with reference to
Feed element 106 is mounted through aperture 404 of cone shaped ground element 104. Feed element 106 may include a receptacle 700 (shown with reference to
With reference to
With reference to
Spherical shaped radiator 110 has a spherical shape from transition region 114 to a top 304. In the illustrative embodiment, top 304 has a flat shape though this merely facilitates fabrication of radiating element 102. Top 304 may have a flat shape with a top diameter 306 of approximately 0.3 inches (0.33 inches in illustrative fabricated antenna). Spherical shaped radiator 110 may have a sphere diameter 308 of approximately four inches (4.178 inches in illustrative fabricated antenna). Spherical shaped radiator 110 may have a radius of curvature 310 of less than two inches, for example, radius of curvature 310 was 1.924 inches in an illustrative fabricated antenna.
The surface of spherical shaped radiator 110 curves away from top 304 with radius of curvature 310 from a center of curvature 311. Center of curvature 311 is located a distance from a rotational axis of symmetry 312 equal to top diameter 306 divided by two. The surface of spherical shaped radiator 110 continues to curve until it reaches an angle below a plane defined at sphere diameter 308. The angle may be approximately equal to cone half-angle 302 of cone shaped radiator 108. At transition region 114, a diameter of a circle through spherical shaped radiator 110 in a plane perpendicular to rotational symmetry axis 312 is approximately equal to diameter 300 of cone shaped radiator 108. Radiating element 102 may have a height 314 between vertex region 112 of cone shaped radiator 108 and top 304 of spherical shaped radiator 110. In an illustrative embodiment, height 314 is approximately five inches (4.769 inches in illustrative fabricated antenna).
With reference to
With reference to
With reference to
Cone shaped ground element 104 further may include a plurality of apertures 604 formed in, but not through, surface 400. Adjacent apertures of the plurality of apertures 604 may be separated by a spacing angle 406 (shown with reference to
With reference to
Second antenna 200 may be designed to match a standard 50-Ohm coaxial cable to match the “intrinsic impedance of free space”, which is ˜377 Ohms. This match may be selected based on an angle 708 between cone shaped radiator 108 and cone shaped ground element 104. For illustration, angle 708 is ˜67 degrees though angle 708 can be varied and still achieve acceptable results as understood by a person of skill in the art. A receiver may be electrically coupled to feed element 106 to receive a receive signal from second antenna 200 or to send a transmit signal to second antenna 200 for radiation by second antenna 200 as understood by a person of skill in the art.
With reference to
In alternative embodiments, cone shaped ground element 104 could have a shape similar to radiating element 102 or have rounded edges (i.e. chamfered edges).
As used in this disclosure, the term “mount” includes join, unite, connect, couple, associate, insert, hang, hold, affix, attach, fasten, bind, paste, secure, bolt, screw, rivet, pin, nail, clasp, clamp, cement, fuse, solder, weld, glue, form over, slide together, layer, and other like terms. The phrases “mounted on” and “mounted to” include any interior or exterior portion of the element referenced. These phrases also encompass direct mounting (in which the referenced elements are in direct contact) and indirect mounting (in which the referenced elements are not in direct contact, but are mounted together via intermediate elements). Elements referenced as mounted to each other herein may further be integrally formed together, for example, using a molding process as understood by a person of skill in the art. As a result, elements described herein as being mounted to each other need not be discrete structural elements. The elements may be mounted permanently, removable, or releasable.
The dimensions provided herein are illustrative as one skilled in the art could deviate from these dimensions and obtain similar results. The word “illustrative” is used herein to mean serving as an illustrative, instance, or illustration. Any aspect or design described herein as “illustrative” is not necessarily to be construed as preferred or advantageous over other aspects or designs. Further, for the purposes of this disclosure and unless otherwise specified, “a” or “an” means “one or more”. Still further, the use of “and” or “or” is intended to include “and/or” unless specifically indicated otherwise.
It will be understood that many additional changes in the details, materials, steps and arrangement of parts, which have been herein described and illustrated to explain the nature of the invention, may be made by those skilled in the art within the principle and scope of the invention as expressed in the appended claims. The foregoing description of illustrative embodiments of the disclosed subject matter has been presented for purposes of illustration and of description. It is not intended to be exhaustive or to limit the disclosed subject matter to the precise form disclosed, and modifications and variations are possible in light of the above teachings or may be acquired from practice of the disclosed subject matter. The embodiments were chosen and described in order to explain the principles of the disclosed subject matter and as practical applications of the disclosed subject matter to enable one skilled in the art to utilize the disclosed subject matter in various embodiments and with various modifications as suited to the particular use contemplated. It is intended that the scope of the disclosed subject matter be defined by the claims appended hereto and their equivalents.
The United States Government has ownership rights in this invention. Licensing inquiries may be directed to Office of Research and Technical Applications, Space and Naval Warfare Systems Center, Pacific, Code 72120, San Diego, Calif., 92152; telephone (619)553-5118; email: ssc_pac_t2@navy.mil. Reference Navy Case No. 101794.
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Simpson et al., Comparing Pulse Radiation from the Unloaded Ice Cream Cone and Resistively Loaded Cone, 2011 IEEE International Symposium on Antennas and Propagation (APSURS), Jul. 3, 2011, pp. 3309-3312. |