US2682610A - Selective mode transducer - Google Patents

Selective mode transducer Download PDF

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US2682610A
US2682610A US260137A US26013751A US2682610A US 2682610 A US2682610 A US 2682610A US 260137 A US260137 A US 260137A US 26013751 A US26013751 A US 26013751A US 2682610 A US2682610 A US 2682610A
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guide
wave
iris
mode
plane
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Archie P King
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AT&T Corp
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Bell Telephone Laboratories Inc
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01PWAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00Auxiliary devices
    • H01P1/16Auxiliary devices for mode selection, e.g. mode suppression or mode promotion; for mode conversion
    • H01P1/161Auxiliary devices for mode selection, e.g. mode suppression or mode promotion; for mode conversion sustaining two independent orthogonal modes, e.g. orthomode transducer

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  • FIG. 1 A first figure.
  • This invention relates to duplex antenna systems for high frequency electromagnetic wave energy and, more particularly, to selective mode transducers employed in said systems whereby a single antenna means may be simultaneously excited in a first mode of high frequency wave energy propagation for transmission and in a second mode of high frequency wave energy propagation for reception.
  • Duplex antenna systems in which a single antenna is employed for transmitting and receiving a high frequency signal are well known. In some of these systems means must be provided for disabling the receiving apparatus during the period of transmission, thus obtaining alternate, rather than simultaneous, reception and transmission. In other of these systems reception and transmission are accomplished simultaneously in different frequency bands which greatly burdens the broad band requirements of the antenna.
  • a horn antenna system which-is of the particu lar type to be disclosed and which is capable of separate excitation by electromagnetic energy in each of two orthogonal polarizations or modes, is connected by a circular wave-guide section designed to suppress undesired higher order modes to a selective mode transducer, in accordance with the invention, the latter being adapted to launch one of said orthogonal modes in said circular guide for transmitting and to select the other of said modes from said circular guide for receiving.
  • the last-mentioned object of the invention is realized in a specific embodiment to be disclosed by coupling to the one mode by a shunt connected iris, the plane of the iris being parallel to the electric vector of said one mode and perpendicular to the electric vector of the other mode.
  • a diametrical septum lying in a plane parallel to the electric vector of the one mode and a plurality of reactive studs extending per-.
  • the other mode passes unaffected along the circular guide without reactive effect even though alone the iris would be expected to appear as an inductive reactance to this mode, and the septum and the studs would each be expected to present reactances to this mode.
  • Fig. 1 shows in pictorial representation a duplex antenna system in accordance with the invention.
  • Fig. 2 is a perspective cut-away view of the selective mode transducer, in accordance with the invention, as employed in the antenna system of Fig. 1.
  • Fig. 1 illustrates the components comprising one station of a duplex antenna system in accordance with the invention.
  • the antenna of this system may be of the type disclosed in United States Patent 2,416,675, granted March 4, 1947, to A. C. Beck and H. T. Friis.
  • this antenna comprises a vertical horn portion, having a front Wall 3, back wall a and side walls 5 and B in the form of an inverted square pyramidal structure having a mouth aperture 8 atthe top end and a virtual apex at the other.
  • a parabolic deflector l is attached to the back edge 9 of the horn mouth aperture 8 and to the extended wall portions or shields l0 and ll of walls 6 and 5, respectively.
  • Deflector 1 is positioned so as to face both aperture 8 and the opening l2 which is formed in the plane of the front wall 3 by the front edges of shields l0 and H, of deflector 7, and of wall 3. At the lower portion of the antenna and slightly above the position of the virtual apex, walls 3, 4, 5 and 56 converge in a square throat aperture 22.
  • transition section 13 tapers gradually from the square cross-section of the throat aperture to the circular cross-section of a connecting wave guide M which has a diameter similar to the cross-sectional dimension of the square aperture 22.
  • This antenna may be excited by a horizontally polarized signal wave, as indicated on Fig. 1, by a TEM Wave and also by a vertically polarized signal wave represented on the drawing by a TEM wave.
  • a horizontally polarized signal wave as indicated on Fig. 1
  • a TEM Wave and also by a vertically polarized signal wave represented on the drawing by a TEM wave.
  • These two polarized waves appear in the horn portion of the antenna of Fig. l as cross-polarized waves, the TEM induced wave having an electric vector of polarization extending between walls and 6 and the TEM induced wave between walls 3 and 4.
  • Either wave may be employed for receiving or transmitting or both may be employed for either receiving or transmitting, but for convenience in explanation, it will be assumed that the TEM wave is employed for transmission and the TEM for reception.
  • cross-polarized waves are transformed and coupled into a corresponding pair of orthogonal wave polarizations in guide US by transition section l3, each wave of the orthogonal pair having a plane of polarization respectively the same as the plane of one wave in the horn portion.
  • the plane of polarization of an electromagnetic Wave as defined herein according to conventional use is that plane extending in the direction of the electric vector and in the direction of wave energy propagation.
  • Each of the orthogonal waves in guide M are similarly transformed and coupled by means of a conical tapered section I5 to crosspolarized dominant TEn mode waves in guide I6.
  • tuning screws H are provided in, for example, four rows, which may be identical, spaced 90 degrees around the periphery of tapered section 15. Diametrically opposite rows of tuning screws 5? can be aligned with the electric field of each of the orthogonal modes.
  • Guide I6 is joined by wave guides l9 and El, each of rectangular transverse cross-section, at spaced positions along the length of guide 18.
  • are mutually perpendicular and are so oriented with respect to the horn portion of the antenna that the transverse plane of guide i9 is parallel to the polarization plane of energy induced by the TEM wave in the horn portion and the plane of guide 21 is parallel to the polarization plane of energy induced by the TEM wave in the horn portion.
  • TEm wave energy from a transmitter is is coupled by guide 19 to a dominant mode in guide It, which mode will be designated the TEu mode and which is associated with the transmitting TEM wave.
  • the TE"11 mode in guide I6 which is orthogonal to the TEn mode therein and is associated with the receiving TEM wave, is coupled from guide l6 by guide 2! as TE"10 wave energy and applied to a receiver 20. Further details of this mode transducer, the nature of the coupling provided by it between the particular modes of wave energy just designated, and the structural details of the transducer will be considered in detail hereinafter with specific reference to Fig. 2.
  • the lower end of guide I5 is terminated in a dissipative element comprising four tapered resistive cards or vanes 32 mounted longitudinally at degree intervals around the periphery of a circular wave-guide section 31.
  • These resistive cards may be of the type disclosed in my copending application Serial No. 135,759, filed December 29, 1949, now United States Patent 2,656,- 513, granted October 20, 1953, or in the continuation in part thereof Serial No. 222,006, filed April 20, 1951.
  • This dissipative combination is provided to absorb any energy reaching guide 31 and to prevent possible resonance effects due to reflection from the end wall 33 of guide 31.
  • a fine mesh screen may be employed at the end of guide 31 in place of the solid wall 38.
  • Fig. 2 shows in detail an enlarged cut-away view of circular wave guide 16 and its associated rectangular guides I9 and 2
  • these guides together constitute a selective mode transducer by which the TE 'ic mode in guide [9 from transmitter I8 is launched as a TE11 mode in guide 16, which in due course excites the transmitting TEM wave.
  • the received TEM waves excite a TE11 wave in guide I6 which is orthogonally polarized with respect to the TE-'11 wave therein.
  • This TEi"11 wave must travel past the junction of guide l9 and its associated components to be described, unaffected thereby, and pass to the lower portion of guide It to be selected by guide 2! and applied as a TE"1o wave to receiver 20.
  • guide I is joined to circular guide IS in a shunt or I-I-plane junction for the TE'11 mode, i. e., the narrow transverse dimension of guide I9 is parallel to the electric vector of polarization of the TE'11 wave in guide It and the longitudinal axis of guide I9 is perpendicular to said vector.
  • guide l9 will couple only to a polarization in guide i 6 which is parallel with the polarization of the dominant TE'm mode in guide 19.
  • a microwave iris 23 is employed in conjunction with a diametrical septum 24 at the junction.
  • Iris 23 may consist of an aperture in the wall of guide Hi, which aperture has cross-sectional dimensions less than the cross-sectional dimensions of guide [9. The factors determining these relative dimensions and the exact values recommended for a specific embodiment will be given hereinafter.
  • Septum 24 comprises a vane of highly conductive material diametrically disposed in guide it in a plane parallel to the plane of the iris and, therefore, in the plane of polarization of the TE11 waves. Since it divides guide 16 into two portions, each beyond cut-off for the 'I'E'u Wave, septum 24 therefore serves as a completely reflecting piston for this wave energy.
  • Septum 24 should extend along the axis of guide l6 for a suflicient length, for example in the order of one-half Wavelength of the energy therein, to prevent leakage of the TE'11 power beyond it. Inasmuch as the plane of septum 24 is perpendicular to the polarity of the TE"11 wave, it has only slight effect thereon as will be shown hereinafter.
  • a microwave iris such as iris 23
  • Certain of the characteristics of a microwave iris, such as iris 23, are well known in the art, including the fact that an iris behaves as a tuned circuit having specific values of inductance and capacitance which depend at a particular fre-.
  • iris 23 may therefore be made resonant at a given frequency for a range of aperture sizes.
  • the dimensions of iris 23 are not chosen to render it resonant at the frequency of the TEu wave, but rather these dimensions are chosen to tune iris 23 substantially on the capacitive side of resonance.
  • Septum 2 behaves as an inductive element for the TEn wave, placed in shunt with iris 23. The value of inductance introduced by septum 25 depends upon the position of the leading edge 25 thereof with respect to iris 23.
  • the position of edge 25 overlaps iris 23 to such an extent that the inductance of septum 24 tunes the shunt combination thereof with iris 23, slightly past resonance for the frequency of the TE'11 wave, the combination remaining very slightly inductive for the reasons to be shown hereinafter. If this minute residual inductive reactance is compensated in the manner to be shown, all of the 'I'E'1o energy in guide 59 is efficiently converted to the TEn wave energy in guide l8 and reflection due to impedance discontinuity is very small. This combination is, of course, bilateral in transmission so that energy may be propagated in either direction through the junction.
  • Fig. 2 has been restricted to the transmission of the TE waves between guides l9 and I6.
  • the TE11 mode polarized at right angles to the TE'n mode.
  • the TE"11 mode must be carried past the junction of guide It without having components thereof diverted into guide i9 and without having components reflected by any impedance discontinuity at the junction. Since the only electrical field components which can be induced by the TE"11 wave in guide It would be polarized across the wide dimension thereof and since the narrow dimension of guide 99 is not sufficient to support this polarization, no components of the TE11 wave will be diverted into guide iii.
  • Reactive studs 26 may comprise three tuning screws extending perpendicular to septum 2 within guide H5 in the region of the septum and may be spaced along guide i6 substantially one-eighth wavelength apart. Since screws 26 lie in the plane of polarization of the Til-"11 wave, they have an appreciable reactive effect thereon and may be tuned to introduce a capacitive reactance equal to the net inductive reactance of iris 23 and septum 2 5. In other words, iris 23, septum 2i and studs 26 together constitute a circuit tuned to resonance at the frequency of the TE"11 wave so that no impedance discontinuity is presented to this wave during its passage down guide 55 to the junction of guide 2
  • which joins guide ft in a shunt plane junction displaced degrees from the junction of guide I9, is therefore in the proper position to receive and support energy from the TE"11 wave of guide iii.
  • a septum 21 is associated with the junction iris of guide 2
  • tuning studs 28 are provided which are adjusted in the manner of studs 26 above.
  • the TE junction and the TE junction each constitute a tuned circuit comprising an iris, a septum and a set of tuning studs, separately tuned to resonance for each mode of a pair of cross-polarized or orthogonal wave modes, one of which is to be branched and the other of which is to be passed unaffected.
  • the septum produces a large effect upon the mode to be branched and a small effect upon the mode to be passed
  • the studs produce a larg effect upon the mode to be passed and a small effect upon the mode to be branched, both adjustments are readily made in practice.
  • the following related dimensions have been found to produce satisfactory results. At other frequencie proportionally related dimensions should produce equally desirable results.
  • the iris may be 1.502 X 0.875 inch in rectangular cross-section and the septum may be 2.8 inches in length and may extend 0.439 inch acrcss the iris aperture.
  • reactance introducing elements may be located in the rectangular wave guides 9 and 2
  • an antenna adapted to support electromagnetic wave energy cross-polarized in a first plane and in a second plane, a section of circular wave guide connected to said antenna to receive said Wave energy polarized in said two planes, a pair of branch shielded transmission lines, each of said branch lines being coupled to said circular guide by a microwave iris, the plane of each iris being parallel to a respective one of said polarization planes, one iris of said pair having dimensions such that a reactance of a first sign is introduced to wave energy in said first plane and thereby a reactance of a second sign to wave energy in said second plane, a diametrical septum of conductive material lying in said first plane and positioned in said circular guide to overlap said one iris, the amount of said overlap introducing a reactance of said second sign to wave energy in said first plane, and a plurality of reactive studs extending within said circular guide perpendicular to said first plane, said studs introducing a reactance of said first sign to wave energy in said second plane.
  • a selective mode transducer for electromagnetic wave energy comprising a section of circular wave guide, a rectangular wave guide, said rectangular wave guide being coupled to said circular guide by a microwave iris, said iris having dimensions such that the reactance thereof is of a first sign to wave energy polarized in a first plane parallel to the plane of said iris and thereby of a second sign to wave energy polarized perpendicular to said first plane, a diametrical septum of conductive material interposed in said circular guide and lying in said first plane, said septum positioned longitudinally along said circular guide with respect to said iris to introduce a reactance of said second sign to wave energy in said first plane, and a plurality of reactive studs extending within said circular guide adjacent said iris and perpendicular to said first plane, said studs introducing a reactance of said first sign to wave energy in said second plane.
  • a selective mode transducer for high frequency electrical transmission systems comprising a main shielded transmission line having a circular transverse cross-section, a pair of branch shielded transmission lines of rectangular transverse cross-section, each of said lines adapted to support the dominant modes of wave energy propagation therein, each of said branch lines being connected to said main line with the lengitudinal axis of each perpendicular to the longitudinal axis of said main line, said branch lines axes lying in mutually perpendicular longitudinal planes and lying in different transverse planes of said main line, a diametrical septum in said main line between said different planes and lying in a plane perpendicular to one of said branch lines axes, and a plurality of reactive studs extending perpendicular to said septum within said main line in the region of said septum.
  • an antenna adapted to sup port electromagnetic wave energy in cross-polarizations
  • a section of circular wave guide con nected to said antenna to receive said wave energy in a pair of orthogonal polarizations in said guide
  • a pair of rectangular wave guides joining said circular guide at diiferent longitudinal positions along said circular guide, the transverse cross-section of each of said rectangular guides being parallel to the polarization of one of said pair of polarizations
  • a vane of conductive material extending across the diameter of said circular guide at a position substantially between said rectangular guides and in a plane parallel to the transverse cross-section of one of said rectangular guides, and reactive means in said circular wave guide at the junction of said circular wave guide with the one of said rectangular wave guides which is closest to said antenna.
  • an antenna adapted to sup-- port electromagnetic wave energy in cross-polarized planes, a main section of shielded transmission line connected to said antenna to receive said wave energy, a pair of branch shielded transmission lines, each of said branch lines being coupled to said main line by a microwave iris, the plane of each iris being aligned parallel to one of said cross-polarized planes, a vane of conductive material associated with each iris and extending across said main line in a plane paral lel to the plane of the iris with which it is associated, and reactive means in said circular wave guide at the junction of said main transmission line with one of said branch transmission lines.

Description

June 29, 1954 A. P. KING SELECTIVE MODE TRANSDUCER Filed Dec. 6, 1951 FIG. 2
FIG.
R M m R INI/ENTOR A. F. m/va 234 Q AT ORNEV Patented June 29, 1954 UNITED STATES ()FFICE SELECTIVE MODE TRANSDUCER Application December 6, 1951, Serial No. 260,137
5 Claims.
This invention relates to duplex antenna systems for high frequency electromagnetic wave energy and, more particularly, to selective mode transducers employed in said systems whereby a single antenna means may be simultaneously excited in a first mode of high frequency wave energy propagation for transmission and in a second mode of high frequency wave energy propagation for reception.
Duplex antenna systems in which a single antenna is employed for transmitting and receiving a high frequency signal are well known. In some of these systems means must be provided for disabling the receiving apparatus during the period of transmission, thus obtaining alternate, rather than simultaneous, reception and transmission. In other of these systems reception and transmission are accomplished simultaneously in different frequency bands which greatly burdens the broad band requirements of the antenna.
It is an obj ect of the present invention to simultaneously receive and transmit high frequency I electrical wave energy in a given frequency band with a single antenna by diiierent modes of wave energy propagation.
In the specific illustrative embodiment of the invention to be hereinafter described in detail, a horn antenna system which-is of the particu lar type to be disclosed and which is capable of separate excitation by electromagnetic energy in each of two orthogonal polarizations or modes, is connected by a circular wave-guide section designed to suppress undesired higher order modes to a selective mode transducer, in accordance with the invention, the latter being adapted to launch one of said orthogonal modes in said circular guide for transmitting and to select the other of said modes from said circular guide for receiving.
It is a particular object of the invention to minimize interference and cross-talk between signals transmitted in said orthogonal modes.
It is a specific object of the invention to couple to and from the wave energy in one orthogonal mode in a circular wave guide without introducing impedance irregularities or other disturbing effects to wave energy in the other orthogonal mode in said guide.
The last-mentioned object of the invention is realized in a specific embodiment to be disclosed by coupling to the one mode by a shunt connected iris, the plane of the iris being parallel to the electric vector of said one mode and perpendicular to the electric vector of the other mode. A diametrical septum lying in a plane parallel to the electric vector of the one mode and a plurality of reactive studs extending per-.
pendicular to the septum are associated with the iris in the manner to be described. As will be shown the effect of the iris in combination with the septum, which alone would appear as an inductive reactance to the one mode, and the studs, which alone would appear asa capacitive reactance to the one mode, is todivert without impedance discontinuity the energy in the one mode through the iris. 0n the other hand, due to the novel arrangement of these three components, the other mode passes unaffected along the circular guide without reactive effect even though alone the iris would be expected to appear as an inductive reactance to this mode, and the septum and the studs would each be expected to present reactances to this mode.
These and other objects, the nature of the present invention, and its various features and advantages, Will appear more fully upon consideration of the various specific illustrative embodiments, shown in the accompanying drawings and in the following detailed description of these embodiments.
In the drawings:
Fig. 1 shows in pictorial representation a duplex antenna system in accordance with the invention; and
Fig. 2 is a perspective cut-away view of the selective mode transducer, in accordance with the invention, as employed in the antenna system of Fig. 1.
In more detail, Fig. 1 illustrates the components comprising one station of a duplex antenna system in accordance with the invention. The antenna of this system may be of the type disclosed in United States Patent 2,416,675, granted March 4, 1947, to A. C. Beck and H. T. Friis. As shown on Fig. 1, this antenna comprises a vertical horn portion, having a front Wall 3, back wall a and side walls 5 and B in the form of an inverted square pyramidal structure having a mouth aperture 8 atthe top end and a virtual apex at the other. A parabolic deflector l is attached to the back edge 9 of the horn mouth aperture 8 and to the extended wall portions or shields l0 and ll of walls 6 and 5, respectively. Deflector 1 is positioned so as to face both aperture 8 and the opening l2 which is formed in the plane of the front wall 3 by the front edges of shields l0 and H, of deflector 7, and of wall 3. At the lower portion of the antenna and slightly above the position of the virtual apex, walls 3, 4, 5 and 56 converge in a square throat aperture 22. A
transition section 13 tapers gradually from the square cross-section of the throat aperture to the circular cross-section of a connecting wave guide M which has a diameter similar to the cross-sectional dimension of the square aperture 22.
This antenna may be excited by a horizontally polarized signal wave, as indicated on Fig. 1, by a TEM Wave and also by a vertically polarized signal wave represented on the drawing by a TEM wave. These two polarized waves appear in the horn portion of the antenna of Fig. l as cross-polarized waves, the TEM induced wave having an electric vector of polarization extending between walls and 6 and the TEM induced wave between walls 3 and 4. Either wave may be employed for receiving or transmitting or both may be employed for either receiving or transmitting, but for convenience in explanation, it will be assumed that the TEM wave is employed for transmission and the TEM for reception. These cross-polarized waves are transformed and coupled into a corresponding pair of orthogonal wave polarizations in guide US by transition section l3, each wave of the orthogonal pair having a plane of polarization respectively the same as the plane of one wave in the horn portion. It is understood that the plane of polarization of an electromagnetic Wave as defined herein according to conventional use, is that plane extending in the direction of the electric vector and in the direction of wave energy propagation. Each of the orthogonal waves in guide M are similarly transformed and coupled by means of a conical tapered section I5 to crosspolarized dominant TEn mode waves in guide I6.
The diameter of tapered section is reduced from that of guide 14, to which it is coupled at one end, to the dimension of guide #9 at the other, the latter dimension being chosen so that only the several polarizations of the dominant mode in guide I6 can be propagated in order to avoid undesirable spurious mode generation. In order to minimize loss in tapered section l5 due to the impedance mismatch produced thereby, tuning screws H are provided in, for example, four rows, which may be identical, spaced 90 degrees around the periphery of tapered section 15. Diametrically opposite rows of tuning screws 5? can be aligned with the electric field of each of the orthogonal modes.
Guide I6 is joined by wave guides l9 and El, each of rectangular transverse cross-section, at spaced positions along the length of guide 18. The cross-sectional dimensions of guides it and are chosen so that only the TE m dominant mode in each may be supported. The transverse cross-sectional planes of guides 19 and 2| are mutually perpendicular and are so oriented with respect to the horn portion of the antenna that the transverse plane of guide i9 is parallel to the polarization plane of energy induced by the TEM wave in the horn portion and the plane of guide 21 is parallel to the polarization plane of energy induced by the TEM wave in the horn portion. Thus TEm wave energy from a transmitter is is coupled by guide 19 to a dominant mode in guide It, which mode will be designated the TEu mode and which is associated with the transmitting TEM wave. Likewise, the TE"11 mode in guide I6, which is orthogonal to the TEn mode therein and is associated with the receiving TEM wave, is coupled from guide l6 by guide 2! as TE"10 wave energy and applied to a receiver 20. Further details of this mode transducer, the nature of the coupling provided by it between the particular modes of wave energy just designated, and the structural details of the transducer will be considered in detail hereinafter with specific reference to Fig. 2.
The lower end of guide I5 is terminated in a dissipative element comprising four tapered resistive cards or vanes 32 mounted longitudinally at degree intervals around the periphery of a circular wave-guide section 31. These resistive cards may be of the type disclosed in my copending application Serial No. 135,759, filed December 29, 1949, now United States Patent 2,656,- 513, granted October 20, 1953, or in the continuation in part thereof Serial No. 222,006, filed April 20, 1951. This dissipative combination is provided to absorb any energy reaching guide 31 and to prevent possible resonance effects due to reflection from the end wall 33 of guide 31. In order to avoid the trapping of water in guide 31 as a result of seepage from rain or condensation when the antenna system of Fig. 1 is employed in an unsheltered location, a fine mesh screen may be employed at the end of guide 31 in place of the solid wall 38.
Fig. 2 shows in detail an enlarged cut-away view of circular wave guide 16 and its associated rectangular guides I9 and 2|. As has been briefly noted, these guides together constitute a selective mode transducer by which the TE 'ic mode in guide [9 from transmitter I8 is launched as a TE11 mode in guide 16, which in due course excites the transmitting TEM wave. Similarly, the received TEM waves excite a TE11 wave in guide I6 which is orthogonally polarized with respect to the TE-'11 wave therein. This TEi"11 wave must travel past the junction of guide l9 and its associated components to be described, unaffected thereby, and pass to the lower portion of guide It to be selected by guide 2! and applied as a TE"1o wave to receiver 20.
Consider for the moment only the transmitted TE waves and the coupling provided for them between guides i9 and I6. Guide I!) is joined to circular guide IS in a shunt or I-I-plane junction for the TE'11 mode, i. e., the narrow transverse dimension of guide I9 is parallel to the electric vector of polarization of the TE'11 wave in guide It and the longitudinal axis of guide I9 is perpendicular to said vector. Thus, guide l9 will couple only to a polarization in guide i 6 which is parallel with the polarization of the dominant TE'm mode in guide 19.
In order to provide complete power transfer through this path a microwave iris 23 is employed in conjunction with a diametrical septum 24 at the junction. Iris 23 may consist of an aperture in the wall of guide Hi, which aperture has cross-sectional dimensions less than the cross-sectional dimensions of guide [9. The factors determining these relative dimensions and the exact values recommended for a specific embodiment will be given hereinafter. Septum 24 comprises a vane of highly conductive material diametrically disposed in guide it in a plane parallel to the plane of the iris and, therefore, in the plane of polarization of the TE11 waves. Since it divides guide 16 into two portions, each beyond cut-off for the 'I'E'u Wave, septum 24 therefore serves as a completely reflecting piston for this wave energy. Septum 24 should extend along the axis of guide l6 for a suflicient length, for example in the order of one-half Wavelength of the energy therein, to prevent leakage of the TE'11 power beyond it. Inasmuch as the plane of septum 24 is perpendicular to the polarity of the TE"11 wave, it has only slight effect thereon as will be shown hereinafter.
Certain of the characteristics of a microwave iris, such as iris 23, are well known in the art, including the fact that an iris behaves as a tuned circuit having specific values of inductance and capacitance which depend at a particular fre-.
quency upon the physical dimension of the iris aperture. An iris may therefore be made resonant at a given frequency for a range of aperture sizes. In accordance with the present invention, however, the dimensions of iris 23 are not chosen to render it resonant at the frequency of the TEu wave, but rather these dimensions are chosen to tune iris 23 substantially on the capacitive side of resonance. Septum 2 3, on the other hand, behaves as an inductive element for the TEn wave, placed in shunt with iris 23. The value of inductance introduced by septum 25 depends upon the position of the leading edge 25 thereof with respect to iris 23. In accordance with the present invention, the position of edge 25 overlaps iris 23 to such an extent that the inductance of septum 24 tunes the shunt combination thereof with iris 23, slightly past resonance for the frequency of the TE'11 wave, the combination remaining very slightly inductive for the reasons to be shown hereinafter. If this minute residual inductive reactance is compensated in the manner to be shown, all of the 'I'E'1o energy in guide 59 is efficiently converted to the TEn wave energy in guide l8 and reflection due to impedance discontinuity is very small. This combination is, of course, bilateral in transmission so that energy may be propagated in either direction through the junction.
Thus far the discussion of Fig. 2 has been restricted to the transmission of the TE waves between guides l9 and I6. Consider now the transmission of the TE11 mode, polarized at right angles to the TE'n mode. In order to minimize interference and cross-talk between signals carried by these two modes, the TE"11 mode must be carried past the junction of guide It without having components thereof diverted into guide i9 and without having components reflected by any impedance discontinuity at the junction. Since the only electrical field components which can be induced by the TE"11 wave in guide It would be polarized across the wide dimension thereof and since the narrow dimension of guide 99 is not sufficient to support this polarization, no components of the TE11 wave will be diverted into guide iii. However, an appreciable inductive reactance would be introduced to this wave by iris 23, which reactance would produce large and undesirable reflection-s. Since the plane of septum 24 lies along equipotential points in the field of the 'IE"11 wave,septum 2% would have substantially no effect thereon except for a possible small reflection from edge 25. This reflection may be minimized by making the thickness of septum 24 a minimum. In accordance with the invention, however, both the inductive reactance of iris 23 and the reactance of septum 24 to the TE"11 wave are tuned out by reactive studs 26. Reactive studs 26 may comprise three tuning screws extending perpendicular to septum 2 within guide H5 in the region of the septum and may be spaced along guide i6 substantially one-eighth wavelength apart. Since screws 26 lie in the plane of polarization of the Til-"11 wave, they have an appreciable reactive effect thereon and may be tuned to introduce a capacitive reactance equal to the net inductive reactance of iris 23 and septum 2 5. In other words, iris 23, septum 2i and studs 26 together constitute a circuit tuned to resonance at the frequency of the TE"11 wave so that no impedance discontinuity is presented to this wave during its passage down guide 55 to the junction of guide 2|. Studs 25 have only small effect upon the TE'11 mode but will nevertheless introduce to it a slight capacitive reactance which, however, compensates the residual inductive reactance reserved above when iris 23 and septum 2% were tuned for the 'IE'n wave.
Rectangular guide 2|, which joins guide ft in a shunt plane junction displaced degrees from the junction of guide I9, is therefore in the proper position to receive and support energy from the TE"11 wave of guide iii. In accordance with the considerations set out above, a septum 21 is associated with the junction iris of guide 2|, identical in relationship thereto as was septum 24 to iris 23. Since'only one wave component is now present in guide Iii, it should be apparent that septum 21 may be positioned to tune the iris of guide 2! precisely to resonance and that tuning studs are not absolutely required. However, commercial considerations are facilitated by making the junction of guide 2| identical in all respects, other than the displacement of 90 degrees around the circumference of guide Hi, to that of guide it, and therefore tuning studs 28 are provided which are adjusted in the manner of studs 26 above.
In summary, therefore, it is seen that the TE junction and the TE junction each constitute a tuned circuit comprising an iris, a septum and a set of tuning studs, separately tuned to resonance for each mode of a pair of cross-polarized or orthogonal wave modes, one of which is to be branched and the other of which is to be passed unaffected. Inasmuch as the septum produces a large effect upon the mode to be branched and a small effect upon the mode to be passed, and conversely, the studs produce a larg effect upon the mode to be passed and a small effect upon the mode to be branched, both adjustments are readily made in practice.
In a specific embodiment designed for a midband frequency of 4040 megacycles, the following related dimensions have been found to produce satisfactory results. At other frequencie proportionally related dimensions should produce equally desirable results. Thus, if guide it a 2.09 inch inside diameter and guides iii and 25 each are constructed of 1.145 x 2.2% inch rectangular wave guide, the iris may be 1.502 X 0.875 inch in rectangular cross-section and the septum may be 2.8 inches in length and may extend 0.439 inch acrcss the iris aperture.
Should manufacturing tolerances make it difficult to maintain the exact dimensions of the iris or should it be diflicult to determine the exact initial dimensions thereof, it should be noted that reactance introducing elements may be located in the rectangular wave guides 9 and 2|, adjustment of which will vary the effective inductance and capacitance of the iris presented to wave components in guide 6 without actually requiring minute changes in the dimensions of the iris aperture.
In all cases, it is understood that the abovedescribed arrangement is simply illustrative of one of the many possible specific embodiments which can represent applications of the principles of the invention. Numerous and varied other arrangements can readily be devised in accordance with said principles by those skilled in the art without departing from the spirit and scope of the invention.
What is claimed is:
1. In combination, an antenna adapted to support electromagnetic wave energy cross-polarized in a first plane and in a second plane, a section of circular wave guide connected to said antenna to receive said Wave energy polarized in said two planes, a pair of branch shielded transmission lines, each of said branch lines being coupled to said circular guide by a microwave iris, the plane of each iris being parallel to a respective one of said polarization planes, one iris of said pair having dimensions such that a reactance of a first sign is introduced to wave energy in said first plane and thereby a reactance of a second sign to wave energy in said second plane, a diametrical septum of conductive material lying in said first plane and positioned in said circular guide to overlap said one iris, the amount of said overlap introducing a reactance of said second sign to wave energy in said first plane, and a plurality of reactive studs extending within said circular guide perpendicular to said first plane, said studs introducing a reactance of said first sign to wave energy in said second plane.
2. A selective mode transducer for electromagnetic wave energy comprising a section of circular wave guide, a rectangular wave guide, said rectangular wave guide being coupled to said circular guide by a microwave iris, said iris having dimensions such that the reactance thereof is of a first sign to wave energy polarized in a first plane parallel to the plane of said iris and thereby of a second sign to wave energy polarized perpendicular to said first plane, a diametrical septum of conductive material interposed in said circular guide and lying in said first plane, said septum positioned longitudinally along said circular guide with respect to said iris to introduce a reactance of said second sign to wave energy in said first plane, and a plurality of reactive studs extending within said circular guide adjacent said iris and perpendicular to said first plane, said studs introducing a reactance of said first sign to wave energy in said second plane.
3. A selective mode transducer for high frequency electrical transmission systems comprising a main shielded transmission line having a circular transverse cross-section, a pair of branch shielded transmission lines of rectangular transverse cross-section, each of said lines adapted to support the dominant modes of wave energy propagation therein, each of said branch lines being connected to said main line with the lengitudinal axis of each perpendicular to the longitudinal axis of said main line, said branch lines axes lying in mutually perpendicular longitudinal planes and lying in different transverse planes of said main line, a diametrical septum in said main line between said different planes and lying in a plane perpendicular to one of said branch lines axes, and a plurality of reactive studs extending perpendicular to said septum within said main line in the region of said septum.
4. In combination, an antenna adapted to sup port electromagnetic wave energy in cross-polarizations, a section of circular wave guide con nected to said antenna to receive said wave energy in a pair of orthogonal polarizations in said guide, a pair of rectangular wave guides joining said circular guide at diiferent longitudinal positions along said circular guide, the transverse cross-section of each of said rectangular guides being parallel to the polarization of one of said pair of polarizations, a vane of conductive material extending across the diameter of said circular guide at a position substantially between said rectangular guides and in a plane parallel to the transverse cross-section of one of said rectangular guides, and reactive means in said circular wave guide at the junction of said circular wave guide with the one of said rectangular wave guides which is closest to said antenna.
5. In combination, an antenna adapted to sup-- port electromagnetic wave energy in cross-polarized planes, a main section of shielded transmission line connected to said antenna to receive said wave energy, a pair of branch shielded transmission lines, each of said branch lines being coupled to said main line by a microwave iris, the plane of each iris being aligned parallel to one of said cross-polarized planes, a vane of conductive material associated with each iris and extending across said main line in a plane paral lel to the plane of the iris with which it is associated, and reactive means in said circular wave guide at the junction of said main transmission line with one of said branch transmission lines.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,362,561 Katzin Nov. 14, 194A 2,364,371 Katzin Dec. 5, 194.4: 2,441,598 Robertson May 18, 1948 2,458,579 Feldman Jan. 11, 1949 2,556,001 Robertson June 5, 1951 2,606,248 Dicke Aug. 5, 1952 2,607,849 Purcell et a1 Aug. 19, 1952
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Cited By (29)

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US2730677A (en) * 1952-08-26 1956-01-10 Csf Ultra-high frequency wave-mode transformers
US2782299A (en) * 1952-01-18 1957-02-19 Bendix Aviat Corp Anti-pulling duplexer
US2786981A (en) * 1954-05-18 1957-03-26 Gen Precision Lab Inc Broadband coaxial line to waveguide transition
US2933731A (en) * 1954-12-08 1960-04-19 Cossor Ltd A C Electromagnetic wave radiators
US2942266A (en) * 1957-07-16 1960-06-21 Bell Telephone Labor Inc Antenna with means for preventing re-radiation into feed guide
US2961618A (en) * 1957-06-12 1960-11-22 Bell Telephone Labor Inc Selective mode transducer
US2975420A (en) * 1954-10-04 1961-03-14 Telefunken Gmbh Directional antenna having cosine shaped aperture
US3004228A (en) * 1958-07-01 1961-10-10 Hughes Aircraft Co Orthogonal mode transducer
US3048804A (en) * 1959-07-27 1962-08-07 Gen Electric Wave guiding system and method
US3166725A (en) * 1962-06-04 1965-01-19 Glenn F Engen Broadband tuning transformer permitting independent matching at adjacent frequencies
US3284802A (en) * 1963-11-12 1966-11-08 Bell Telephone Labor Inc Folded horn-reflector antenna wherein primary reflector is nonreflective at portion where specular reflection to feed would otherwise occur
US3357022A (en) * 1963-12-05 1967-12-05 Bell Telephone Labor Inc Folded horn-reflector antenna structure
US3391350A (en) * 1967-08-09 1968-07-02 Army Usa Tunable slot coupling between oscillator and waveguide
US3421086A (en) * 1966-03-01 1969-01-07 Gen Electric Co Ltd Mode suppressing filters in aerial feeders
US3508277A (en) * 1966-05-27 1970-04-21 Int Standard Electric Corp Coaxial horns with cross-polarized feeds of different frequencies
US4558290A (en) * 1984-04-11 1985-12-10 The United States Of America As Represented By The Secretary Of The Air Force Compact broadband rectangular to coaxial waveguide junction
FR2569907A1 (en) * 1984-08-31 1986-03-07 Loire Electronique DEVICE FOR RECEIVING DOUBLE POLARIZED HYPERFREQUENCY SIGNALS
US4584588A (en) * 1982-11-12 1986-04-22 Kabelmetal Electro Gmbh Antenna with feed horn and polarization feed
US4628538A (en) * 1985-05-13 1986-12-09 Andrew Corporation Television transmission system using overmoded waveguide
US4797681A (en) * 1986-06-05 1989-01-10 Hughes Aircraft Company Dual-mode circular-polarization horn
US4816786A (en) * 1982-11-12 1989-03-28 Kabelmetal Electro Gmbh Polarizer
US5216433A (en) * 1991-11-15 1993-06-01 Hughes Aircraft Company Polarimetric antenna
US6087999A (en) * 1994-09-01 2000-07-11 E*Star, Inc. Reflector based dielectric lens antenna system
US6107897A (en) * 1998-01-08 2000-08-22 E*Star, Inc. Orthogonal mode junction (OMJ) for use in antenna system
US6160520A (en) * 1998-01-08 2000-12-12 E★Star, Inc. Distributed bifocal abbe-sine for wide-angle multi-beam and scanning antenna system
US6181293B1 (en) * 1998-01-08 2001-01-30 E*Star, Inc. Reflector based dielectric lens antenna system including bifocal lens
WO2006111702A1 (en) * 2005-04-21 2006-10-26 Invacom Ltd Circular and/of linear polarity format data receiving apparatus
US20080186110A1 (en) * 2004-09-08 2008-08-07 Invacom Ltd. Broadcast Signal Waveguide
RU2703605C1 (en) * 2019-03-22 2019-10-21 Публичное акционерное общество "Радиофизика" Waveguide polarization selector with reduced longitudinal size

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US2364371A (en) * 1940-08-31 1944-12-05 Rca Corp Double polarization feed for horn antennas
US2441598A (en) * 1944-06-16 1948-05-18 Bell Telephone Labor Inc Wave transmission
US2458579A (en) * 1945-04-26 1949-01-11 Bell Telephone Labor Inc Microwave modulator
US2556001A (en) * 1947-01-02 1951-06-05 Bell Telephone Labor Inc Microwave impedance matching reactor
US2606248A (en) * 1945-04-03 1952-08-05 Robert H Dicke Transmit receive device
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US2364371A (en) * 1940-08-31 1944-12-05 Rca Corp Double polarization feed for horn antennas
US2362561A (en) * 1940-12-12 1944-11-14 Rca Corp Horn radiator
US2607849A (en) * 1943-10-02 1952-08-19 Edward M Purcell Control of polarization in wave guides and wave guide systems
US2441598A (en) * 1944-06-16 1948-05-18 Bell Telephone Labor Inc Wave transmission
US2606248A (en) * 1945-04-03 1952-08-05 Robert H Dicke Transmit receive device
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Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782299A (en) * 1952-01-18 1957-02-19 Bendix Aviat Corp Anti-pulling duplexer
US2730677A (en) * 1952-08-26 1956-01-10 Csf Ultra-high frequency wave-mode transformers
US2786981A (en) * 1954-05-18 1957-03-26 Gen Precision Lab Inc Broadband coaxial line to waveguide transition
US2975420A (en) * 1954-10-04 1961-03-14 Telefunken Gmbh Directional antenna having cosine shaped aperture
US2933731A (en) * 1954-12-08 1960-04-19 Cossor Ltd A C Electromagnetic wave radiators
US2961618A (en) * 1957-06-12 1960-11-22 Bell Telephone Labor Inc Selective mode transducer
US2942266A (en) * 1957-07-16 1960-06-21 Bell Telephone Labor Inc Antenna with means for preventing re-radiation into feed guide
US3004228A (en) * 1958-07-01 1961-10-10 Hughes Aircraft Co Orthogonal mode transducer
US3048804A (en) * 1959-07-27 1962-08-07 Gen Electric Wave guiding system and method
US3166725A (en) * 1962-06-04 1965-01-19 Glenn F Engen Broadband tuning transformer permitting independent matching at adjacent frequencies
US3284802A (en) * 1963-11-12 1966-11-08 Bell Telephone Labor Inc Folded horn-reflector antenna wherein primary reflector is nonreflective at portion where specular reflection to feed would otherwise occur
US3357022A (en) * 1963-12-05 1967-12-05 Bell Telephone Labor Inc Folded horn-reflector antenna structure
US3421086A (en) * 1966-03-01 1969-01-07 Gen Electric Co Ltd Mode suppressing filters in aerial feeders
US3508277A (en) * 1966-05-27 1970-04-21 Int Standard Electric Corp Coaxial horns with cross-polarized feeds of different frequencies
US3391350A (en) * 1967-08-09 1968-07-02 Army Usa Tunable slot coupling between oscillator and waveguide
US4584588A (en) * 1982-11-12 1986-04-22 Kabelmetal Electro Gmbh Antenna with feed horn and polarization feed
US4816786A (en) * 1982-11-12 1989-03-28 Kabelmetal Electro Gmbh Polarizer
US4558290A (en) * 1984-04-11 1985-12-10 The United States Of America As Represented By The Secretary Of The Air Force Compact broadband rectangular to coaxial waveguide junction
FR2569907A1 (en) * 1984-08-31 1986-03-07 Loire Electronique DEVICE FOR RECEIVING DOUBLE POLARIZED HYPERFREQUENCY SIGNALS
US4695844A (en) * 1984-08-31 1987-09-22 Societe D'electronique De La Region Pays De Loire Device for receiving dual polarized microwave signals
EP0174250A1 (en) * 1984-08-31 1986-03-12 Societe Electronique De La Region Pays De Loire Device for receiving dual polarized microwave signals
US4628538A (en) * 1985-05-13 1986-12-09 Andrew Corporation Television transmission system using overmoded waveguide
US4797681A (en) * 1986-06-05 1989-01-10 Hughes Aircraft Company Dual-mode circular-polarization horn
US5216433A (en) * 1991-11-15 1993-06-01 Hughes Aircraft Company Polarimetric antenna
US6087999A (en) * 1994-09-01 2000-07-11 E*Star, Inc. Reflector based dielectric lens antenna system
US6198449B1 (en) 1994-09-01 2001-03-06 E*Star, Inc. Multiple beam antenna system for simultaneously receiving multiple satellite signals
US6181293B1 (en) * 1998-01-08 2001-01-30 E*Star, Inc. Reflector based dielectric lens antenna system including bifocal lens
US6160520A (en) * 1998-01-08 2000-12-12 E★Star, Inc. Distributed bifocal abbe-sine for wide-angle multi-beam and scanning antenna system
US6107897A (en) * 1998-01-08 2000-08-22 E*Star, Inc. Orthogonal mode junction (OMJ) for use in antenna system
US20080186110A1 (en) * 2004-09-08 2008-08-07 Invacom Ltd. Broadcast Signal Waveguide
US7804381B2 (en) * 2004-09-08 2010-09-28 Invacom Ltd. Broadcast signal waveguide
WO2006111702A1 (en) * 2005-04-21 2006-10-26 Invacom Ltd Circular and/of linear polarity format data receiving apparatus
US20080157902A1 (en) * 2005-04-21 2008-07-03 Invacom Ltd. Circular and/or Linear Polarity Format Data Receiving Apparatus
US8040206B2 (en) 2005-04-21 2011-10-18 Invacom Ltd. Circular and/or linear polarity format data receiving apparatus
RU2703605C1 (en) * 2019-03-22 2019-10-21 Публичное акционерное общество "Радиофизика" Waveguide polarization selector with reduced longitudinal size

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