Many commercial and military technologies require the use of multiple transmission line types, such as coaxial cables, stripline, microstrip, waveguides, and optical fibers. These transmission lines offer different advantages and disadvantages, so it is desirable to transition between two different transmission line technologies within a module or system. Many of these transmission lines transitions tend to only operate efficiently over a narrow frequency band, which greatly reduces the amount of signal spectrum that can flow through them.
In particular, coaxial and waveguide transmission lines are used in a number of electrical modules and systems. A classic example is a waveguide fed antenna (such as a horn) with the waveguide having a signal input from a coaxial cable. This transition consists of the inner conductor of the coaxial line being probed into the waveguide and launching its signal into the waveguide. This transition and other coaxial to waveguide transmission line transitions are used in many applications. Commercially sold or academically documented coaxial-to-waveguide transitions are efficient (low-loss), but very frequency band limited. A need exists for a coaxial to waveguide transmission line transition that operates over a wider frequency band than currently-available transitions and maintains a high level of efficiency.
Reference in the specification to “one embodiment” or to “an embodiment” means that a particular element, feature, structure, or characteristic described in connection with the embodiments is included in at least one embodiment. The appearances of the phrases “in one embodiment”, “in some embodiments”, and “in other embodiments” in various places in the specification are not necessarily all referring to the same embodiment or the same set of embodiments.
Some embodiments may be described using the expression “coupled” and “connected” along with their derivatives. For example, some embodiments may be described using the term “coupled” to indicate that two or more elements are in direct physical or electrical contact. The term “coupled,” however, may also mean that two or more elements are not in direct contact with each other, but yet still co-operate or interact with each other. The embodiments are not limited in this context.
As used herein, the terms “comprises,” “comprising,” “includes,” “including,” “has,” “having” or any other variation thereof, are intended to cover a non-exclusive inclusion. For example, a process, method, article, or apparatus that comprises a list of elements is not necessarily limited to only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Further, unless expressly stated to the contrary, “or” refers to an inclusive or and not to an exclusive or.
Additionally, use of the “a” or “an” are employed to describe elements and components of the embodiments herein. This is done merely for convenience and to give a general sense of the invention. This detailed description should be read to include one or at least one and the singular also includes the plural unless it is obviously meant otherwise.
Further, the terms “around, “about” or “approximately” shall generally mean within 20 percent, preferably within 10 percent, and more preferably within 5 percent of a given value or range. Numerical quantities given herein are approximate, meaning that the term “around”, “about” or “approximately” can be inferred if not expressly stated.
The embodiments disclosed herein involve a means to transition between a waveguide transmission line and coaxial transmission line, or vice versa, using a wideband, efficient transition. The disclosed transition allows for extended frequency operation for high power combination of low power amplifiers using a radial combination method.
Transition 20 includes a first rigid portion 30 comprising an inverted hollow cone, a second rigid portion 40 comprising a hollow tube, and a third rigid portion 50 comprising a hollow cone. First rigid portion 30 has a first end 32 and a second end 34. First rigid portion 30 tapers inward at a first angle from first end 32 towards second end 34. Second rigid portion 40 has a first end 42 and a second end 44. First end 42 is at least partially disposed within second end 34 of first rigid portion 30. As an example, first end 42 is disposed 1 mm within second end 34, but other depths may be suitable depending upon the application and requirements. Third rigid portion 50 has a first end 52 and a second end 54. First end 52 is at least partially disposed within second end 44 of second rigid portion 40. Third rigid portion 50 tapers outward at a second angle from first end 52 towards second end 54.
In some embodiments, the second angle is less than the first angle. As an example, the second angle is about 90 degrees and the first angle is about 148 degrees. In some embodiments, the second angle is equal to the first angle. In some embodiments, the second angle is more than the first angle. In some embodiments, the first angle and the second angle are determined according to the equation
where Zc is the impedance, μ is permeability of a medium, ∈ is permittivity of the medium, such as air, θ1 is the first angle, and θ2 is the second angle.
The dimensions of the components of transition 20 may vary depending upon the particular application and system requirements. The following dimensions are provided as an illustrative example for a particular configuration. It should be recognized that even with the particular configuration, such dimensions may vary slightly from the numbers given without departing from the intended operation. Accordingly, first rigid portion 30, second rigid portion 40, and third rigid portion 50 may have a combined height of about 11 mm, such that the distance a is 11 mm, the distance b of first end 42 of second rigid portion 40 to the top surface of bottom plate 70 is 7.9 mm, the distance c of second end 44 of second rigid portion 40 to the bottom surface of top plate 60 is 5.25 mm, and the distance d of first end 42 of second rigid portion 40 to the top surface of top plate 60 is 4.7 mm.
Further, the height e of a tapered inset 62 within top plate 60 is 1 mm, the diameter of first end 32 of first rigid portion 30 may be about 12 mm, the diameter of second end 34 of first rigid portion 30 may be about 6.1 mm, the diameter f of first end 42 and second end 44 of second rigid portion 40 may be about 3.5 mm, the diameter of first end 52 of third rigid portion 50 may be about 3.5 mm, and the diameter g of second end 54 of third rigid portion 50 may be about 6.1 mm. These dimensions may be used for wideband operation in the Ku-Band, but the general design as discussed above is applicable at various dimensions for operation in any useable frequency band.
In some embodiments, system 60 further includes a waveguide comprising a top plate 60 and a bottom plate 70. In some embodiments, top plate 60 is separated from bottom plate 70 by a distance of about 10 mm. It should be recognized by a person having ordinary skill in the art that the distance between top plate 60 and bottom plate 70 may vary depending upon the particular application or system requirements.
In some embodiments, transition 20 is a stand-alone unit that is incorporated into system 10. In other embodiments, one or more portions of transition 20 are formed as part of another component within system 10. For example, in the stand-alone embodiments, the first end 32 of first rigid portion 30 is in contact with top plate 60. In the other embodiments, first rigid portion 30 is built within the top plate as is shown in
Top plate 60 has an opening 64 therein configured to receive a pin 84 of a coaxial connector 80 therethrough. Connector 80 is comprised of a metal pin 84 surrounded by a dielectric (Teflon) bead 82 to hold pin 84 in place. As an example, pin 84 may have a diameter of 0.91 mm and the coax dielectric bead 82 may have a diameter of 2.94 mm. In some embodiments, top plate 60, first rigid portion 30, second rigid portion 40, and third rigid portion 50 are sized such that when pin 84 of coaxial cable 80 passes through opening 64, pin 84 becomes electrically connected to third rigid portion 50. As shown in
The design of transition 20 is advantageous in that it increases the frequency bandwidth of commonly used coaxial to waveguide transition by about 28% when compared to a state of the art single top conical taper. Further, it increases the bandwidth of the transition by about 42% when compared to a state of the art single bottom conical taper.
As shown, the electric field lines emanating from coaxial conductor 212 within coaxial cable 210 are essentially parallel with waveguide 220. As the electric field lines transition into the region defined by inner wall 234, the electric field lines begin to expand out to fill the region, curving significantly beginning where conductor 212 meets second rigid portion 240, but still contained by inner wall 234. Upon reaching third rigid portion 250, the electric field lines are no longer contained by inner wall 234 and transition outwardly into waveguide 220 between top plate 222 and bottom plate 224. The electric field lines curve upward and outward from third rigid portion 250 until the electric field lines eventually become substantially vertical within waveguide 220, as shown.
The conical tapers of the transition, i.e. first rigid portion 230 and third rigid portion 230, allow the transition from the coaxial conductor 210 to waveguide 220 to be performed efficiently at a wide range of frequencies. This occurs because the spacing between the conductors is not one set length, but rather contains the optimal spacing for many different frequencies between the tapered portions.
The transition disclosed above may be suitable for many applications and in various devices. One embodiment of the type of device that may utilize the transition is the radial combiner shown in
As shown best in
One embodiment of the coaxial to waveguide wideband transition disclosed herein was tested in radial combiner 300 as shown in
The ideal loss for a 4-1 combiner/divider from the N-type threaded input to the rectangular waveguide output arms is 75% loss due to the 1:4 power splitting (6 dB loss). It can be seen from lines 410 and 420 that the transition incorporates nearly zero additional loss over a 2:1 bandwidth (10-20 GHz), which is remarkably wideband. Further, the bandwidth of the two transitions represented by lines 430 and 440 operate over a much narrower frequency range (every 10 units on the y-axis is a factor of 10× loss), indicating the advantages of the embodiments of the transition disclosed herein versus the compared transitions represented by lines 430 and 440.
Many modifications and variations of the Wideband Waveguide to Coaxial Transition are possible in light of the above description. Within the scope of the appended claims, the embodiments of the systems described herein may be practiced otherwise than as specifically described. The scope of the claims is not limited to the implementations and the embodiments disclosed herein, but extends to other implementations and embodiments as may be contemplated by those having ordinary skill in the art.
This application claims the benefit of U.S. Provisional Patent Application Ser. No. 62/309,392 filed Mar. 16, 2016, entitled “Ultra-Wideband Radial Combiner”, the content of which is fully incorporated by reference herein.
The Wideband Waveguide to Coaxial Transition is assigned to the United States Government and is available for licensing for commercial purposes. Licensing and technical inquiries may be directed to the Office of Research and Technical Applications, Space and Naval Warfare Systems Center, Pacific, Code 72120, San Diego, Calif., 92152; voice (619) 553-5118; email ssc_pac_T2@navy.mil; reference Navy Case Number 103526.
Number | Date | Country | |
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62309392 | Mar 2016 | US |