A right-angle waveguide probe antenna with a bandwidth greater than 15% of the center frequency of the operating band, as defined by a return loss over the frequency range better than or equal to −20 dBV. This invention is most relevant to a right-angle coaxial to an air-filled rectangular waveguide transition. The probe antenna is comprised of a flared section followed by a rectangular section resulting in an irregular convex pentagon shape with two right angles at the base which resembles an A-frame on top of a rectangle. The resultant “A-frame probe” can be connected to a coaxial feed cable and extended into a waveguide through an aperture. The A-frame probe operates as a TE10 mode waveguide radiator, and is sized and positioned such that the impedance of the probe antenna is closely matched to the impedance of the waveguide across a wider frequency band.

CROSS-REFERENCE TO RELATED APPLICATIONS

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THE NAMES OF THE PARTIES TO A JOINT RESEARCH AGREEMENT

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BACKGROUND OF THE INVENTION

Field of the Invention

The present invention relates generally to coaxial to waveguide adapters, and more specifically, to a right-angle coaxial to waveguide probe antenna for transmitting and receiving the dominant TE mode.

Background of the Invention

Rectangular waveguides excited by a right-angle coaxial to waveguide probe antenna conventionally provide a narrow bandwidth of operation, typically less than 15% when defined by a return loss over the frequency range better than. or equal to −20 dBV. The frequency and/or frequency range of operation is determined by the frequencies at which the impedance of the probe antenna is matched to the impedance of the waveguide [R. Collin, Field Theory of Guided Waves. McGraw-Hill, 1960, pp. 258-271], provided the frequency and/or frequencies are above the cutoff frequency of the waveguide.

A common feature among conventional right-angle coaxial to waveguide probe antennas is a narrow band of frequencies at which the probe antenna impedance is matched, or closely matched, to the impedance of the waveguide. However, in some applications, a larger bandwidth is more desirable. The solution to this problem is not trivial and has, until now, remained elusive. Thus, there exists a need for a wideband coaxial to waveguide probe antenna.

Background Art

U.S. Pat. No. 4,463,324, patented Jul. 31, 1984 by inventor John C. Rolfs, reveals a miniature coaxial transmission line to waveguide transition that utilizes a metallic cylindrical sleeve affixed to the end of the projecting center conductor. The cited existing art provides a method of matching the antenna probe impedance to operate at a particular frequency but does not provide a method to increase the bandwidth beyond the conventional bandwidth of operation. The limitation of existing art is that the bandwidth is fixed and cannot be increased beyond the conventional bandwidth of operation.

BRIEF SUMMARY OF THE INVENTION

The following is intended to be a brief summary of the invention and is not intended to limit the scope of the invention.

With the stated background of the invention in mind, it is an object of this invention to provide a right-angle waveguide probe antenna. with a bandwidth greater than 15% of the center frequency of the operating band, defined by a return loss over the frequency range better than or equal to −20 dBV.

This invention is most relevant to a right-angle coaxial to an air-filled rectangular waveguide transition.

The object of this invention is attained generally by designing the shape of the probe antenna such that it is capable of matching, or closely matching, the impedance of the probe antenna to the impedance of the waveguide across a wide band of frequencies.

The embodiment of this invention is characterized by a conducting structure, typically copper, and is formed such that the probe antenna increases in width along the cross-sectional dimension of the waveguide from the diameter of the coaxial feed center conductor to a width greater than the diameter of the coaxial center conductor but less than the width of the waveguide. The exact width of the widest part of the probe antenna will be determined by the desired increase in bandwidth. The flared section will then be followed by a rectangular section to reach the depth necessary to match the impedance of the probe antenna to the impedance of the waveguide across the desired frequency band, resulting in a pentagon shape resembling an A-frame on top of a rectangle. The thickness of the probe antenna will remain equal to the diameter of the coaxial center conductor in the longitudinal dimension of the waveguide. Finally, the probe will be positioned such that the distance to the back wall of the waveguide is set to match the impedance of the probe antenna to the impedance of the waveguide across the desired frequency band. This invention overcomes the narrow bandwidth limitation of existing art by careful inclusion of a flared section and maintaining a uniform thickness in the longitudinal dimension of the waveguide, resulting in a wide bandwidth operation as previously defined.

DETAILED DESCRIPTION OF THE INVENTION

Referring toFIG. 1, a wideband A-frame waveguide probe antenna1and2(hereinafter sometimes referred to simply as A-frame probe) is shown to include a waveguide section3having a pair of broad walls4aand4b, a pair of narrow walls5aand5b, and a short circuited end (or backshort)6. The A-frame probe extends into the waveguide section3, through an aperture7in one of the broad walls4a, and is attached to the center conductor8of a coaxial feed cable9.

The coaxial feed cable9is filled with a dielectric material between the inner and out conductors, while the waveguide section3is filled with air. The transition between the two materials occurs at the interior broad wall4awhich the aperture7is located. The A-frame probe1-2and coaxial feed inner conductor8are made of copper. The coaxial feed outer conductor and waveguide walls4a,4b,5a,5b. and6are made of aluminum.

The overall length of the A-frame probe is approximately 0.799 mm, as measured from the inside broad wall4aat the center point of the aperture7to the bottom of the rectangular section of the A-frame probe1.

The thickness of the A-frame probe is approximately 0.36 mm, which is equal to the diameter of this specific embodiment of the center conductor8of the coaxial feed cable9.

The height of the top triangular section of the A-frame probe2is approximately 0.31478 mm as measured from the point at which the probe width begins to flare approximately 0.1349 mm below the inside broad wall4aat the center point of the aperture7.

The height of the bottom rectangular section of the A-frame probe1is approximately 0.34976 mm as measured from the bottom of triangular flared section of the A-frame probe2.

The narrow width at the top of the triangular section of the A-frame probe2is approximately 0.36 mm, which is equal to the thickness of the A-frame probe1and the diameter of the center conductor8of the coaxial feed cable9.

The broad width of the rectangular section of the A-frame probe1is approximately 0.9924 mm.

The interior of the broad walls4aand4bof the waveguide section3are approximately 4.997 mm wide and the interior of the narrow walls5aand5bare approximately 1.249 mm high.

The center of the A-frame probe1and2is approximately 1.0818 mm away from the back wall (or backshort) of the waveguide section6and in the center of the broad wall4adimension.

The diameter of the aperture7is approximately 1.152 mm and the relative permittivity of the dielectric within the coaxial cable between the center and outer conductor is 2.08. The outer diameter of the dielectric within the coaxial cable (and coincident inner diameter of the coaxial cable outer conductor) is equal to the diameter of the aperture7. The characteristic impedance of the coaxial cable is therefore approximately 50 Ohms. The rectangular waveguide is air-filled, and thus has a relative permittivity of1. This specific embodiment of this invention has demonstrated a bandwidth of up to 46% for a symmetric center frequency across the band of operation of 68 GHz. The resulting 31.3 GHz bandwidth, thus, ranges from approximately 52.3 GHz to 83.6 GHz. In operation, the A-frame probe antenna operates as a TE10 mode waveguide radiator within or across the frequency band of operation.

The dimensions of the A-frame probe just mentioned were:

Having described a specific embodiment of this invention, it is now evident that other embodiments incorporating its concepts may be used. For example. the antenna element could be fed by an alternative feed network, such as a planar trace. Also, it will be apparent to those skilled in the art that various modifications and variations of the present invention's parameters can be made to achieve differing amounts of bandwidth without departing from the scope or spirit of the invention. Thus, this invention should not be restricted to its disclosed embodiment, but rather it is intended that the present invention covers such modifications and variations as come within the scope of the appended claims and their equivalents.