US3016534A - Dual function antenna - Google Patents

Dual function antenna Download PDF

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Publication number
US3016534A
US3016534A US40377A US4037760A US3016534A US 3016534 A US3016534 A US 3016534A US 40377 A US40377 A US 40377A US 4037760 A US4037760 A US 4037760A US 3016534 A US3016534 A US 3016534A
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United States
Prior art keywords
antenna
plate
lens
dielectric
disc
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Expired - Lifetime
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US40377A
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English (en)
Inventor
Agostino Jack V D
Rothenberg Carl
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Unisys Corp
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Sperry Rand Corp
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Priority to NL266588D priority Critical patent/NL266588A/xx
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Priority to US40377A priority patent/US3016534A/en
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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/04—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/002—Antennas or antenna systems providing at least two radiating patterns providing at least two patterns of different beamwidth; Variable beamwidth antennas
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/12—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems
    • H01Q3/14—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device

Definitions

  • This invention relates to a dual function antenna, and more particularly to an antenna structure adapted for ush mounting on an aircraft and which is capable of simultaneously radiating and/or receiving microwave energy in both a rotatable directional antenna pattern and an omnidirectional antenna pattern.
  • an airborne communication system be capable of simultaneously radiating aud/or receiving energy in both an omnidirectional pattern and a directional pattern. Because of space and weight limitations in an aircraft, it is necessary to provide antenna means which can accomplish both of these functions with a minimum amount of equipment. It also is required that the antenna structure be adapted for mounting on the aircraft in such a way as to interfere as little as possible with the aerodynamics of the aircraft.
  • Another object of this invention is to provide a dual function antenna for mounting on an aircraft fuselage with a minimum of aerodynamic disturbance to said air craft.
  • a further object of this invention is to provide a small compact antenna arrangement for simultaneously radiating energy in both an omnidirectional radiation pattern and a directional radiation pattern.
  • Still another object of this invention is to provide a relatively simple compact antenna structure providing an omnidirectional antenna pattern and a directional antenna pattern rotatable throughout 360 of azimuth.
  • a structure comprising first and second centrally apertured conductive pla-tes. vertically spaced from each other. Disposed above and in contact with the uppermost plate is a circular dielectric disc which tapers uniformly in thickness from its center to its edge.
  • a coaxial transmission line extends through the center apertures of said two conductive plates, with the outer conductor of said line terminating on said uppermost plate and the center conductor of the coaxial line terminating within the dielectric disc.
  • the uppermost conductive plate and the dielectric disc comprise a dielectric-disc antenna which is excited by the center conductor of the coaxial line and operates as a surface wave antenna to radiate microwave energy in an omnidirectional radiation pattern.
  • the lowermost one of said conductive plates extends radially beyond the outer edge of the upper conductive pla-te, and the region between the plates, from the central axis of the plates to the periphery of the lowermost plate,
  • the entire antenna structure is rotatable about 'the central axis of the conductive plates to provide 360 of azimuth scanning of the directional beam.
  • FIG. l is a sectional view, partially broken away, illustrating one embodiment of the dual function antenna of this invention.
  • FIG. 2 is a top view lustratedin FIG. 1;
  • FIGS. 3, 4 and 5 are curves used to help explain certain features of the antennas of this invention.
  • FIG. .6 is an illustration of an alternative construction of the dual function antenna of this invention.
  • the du-al function antenna of this invention is comprised of integrally mounted omnidirectional antenna 10 and directional antenna 11.
  • Omnidirectional antenna 10 is comprised of a circular dielectric disc 12 having a uniformly decreasing taper from its center to its edge and is made of a low loss .material whose dielectric constant is greater than that of air.
  • vQmnidirectional antenna 10 further includes an annular conductive .plate 13 which functions as a ground plane .and .together with circular dielectric disc 12 operates as a surface wave type of antenna which isexcited by the extended center conductor 14 of coaxial transmission line section 25.
  • Omnidirectional antenna 10 radiates vertically polarized energy in an omnidirectional radiation pattern.
  • Directional antenna 11 is comprised of said centrally apertured conductive plate 13 and a second centrally apertured conductive plate 16 which is vertical'y displaced from plate 13 and extends radially beyond the edge of plate 13. Disposed between lthe two conductive plates 13 and 16 is an annular sheet of homogeneous low loss dielectric material 17 which provides a radially monotonically decreasing index of refraction between the plates, as will be explained in detail hereinbelow.
  • the bottommcst conductive plate 16 has an aperture 18 naar its periphery through which energy is coupled into directional antenna 11.
  • a tapered-depth wave guide feed 21, which operates as an end tire waveguide antenna. is positioned in aperture 1 8 and couples microwave energy from waveguide 19 into directional antenna 11.
  • the reverse-bend portion 20 of waveguide 19 is filled with a dielectric material 22 to match the propagating characteristics of waveguide feed 21 to that of the lens of directional antenna l1.
  • .Directional antenna 11 is of the general type which has become known as -a Luneberg lens antenna originally suggested by R. K. Luneberg in Mathematical Theory of Optics, Brown University, 1944, pages 208-213, but modified in the manner suggested by J. E. Eaton in NRL Report 4110, An Extension of the Luneberg Type Lenses, February 16, 1953.
  • electromagnetic energy is directed Aacross the lens from a radiator near the periphery and emerges as a collimated beam diametrically opposite the point of entrance of the energy.
  • The' directional antena of this invention may be conof the func-tion antenna ilsidered as being comprised of two radially-adjacent lens regions 23 and 24.
  • Region 23 will be referred to herein as the parallel plate region and is comprised of the parallel conductive plates 13 and 16 between which is disposed dielectric material 17 whose thickness varies in the manner to be described hereinbelow in order to provide the radially decreasing eliective index of refraction.
  • the second region 24 will be refzrred to herein as the surface wave region and is comprised of the outer portion of dielectric disc 17 and the portion of conductive annular plate 16 which extends radially beyond the periphery of the uppermost plate 13. This latter portion of the lens functions as a surface wave antenna which performs as an Eaton-Luneberg type lens in the horizontal plane, while operating as an end-tire antenna in the vertical plane.
  • the dielectric material in both regions 23 and 24, that is, dielectric disc 17, is made from a single disc of homogeneous dielectric material whose cross-sectional contour is shaped in the respective regions 23 and 24 in a manner to be described hereinbelow.
  • Coaxial line section 25 which serves as a feed for surface wave omnidirectional antenna 10, extends through the central apertures of parallel plates 13 and 16 with the outer conductor 15 of said coaxial line terminating on the upper conductive plate 13 and the inner conductor 14 terminating within dielectric disc 12.
  • Coaxial line 25 is secured in position by means of nut 26 which engages a threaded portion 27 of outer conductor 15.
  • Nut 26 is hous;d within a recessed portion of bottom conductive plate 16 and is turned to engage the upper surface of said recessed portion.
  • Conductive plate 16 is comprised of a relatively thick disc of aluminum, and structurally serves as a base plate for supporting the antenna structure.
  • waveguide section 19 is coupled through ange joint 28 to a wave guide section 29 which in turn is coupled to the outermost coaxial line section of a dual concentric coaxial line section 30.
  • the outermost coaxial line section is comprised of outer conductor 31 and conductor l5.
  • the innermost coaxial line section which excites omnidirectional antenna 10, is comprised of inner conductor 14 and outer conductor 15.
  • This dual concentric coaxial line section is joined to a dual waveguide feed 32 by means of a dual coaxial line rotating joint 33.
  • the input wa eguide feed is comprised of two waveguideto-coaxial line transitions of the type illustrated on page 357 of Microwave Transmission Circuits, by Ragan, McGraw-Hill Book Company, Inc., 1948.
  • a source of microwave energy E is coupled to input waveguide 34, and by means of cross bar transition 35, said energy is coupl;d to the innermost one of the concentric coaxial lines 25.
  • a second source of microwave energy Ed is couped through a second input waveguide 36 to the outermost concentric coaxial line, which is coupled by waveguide sections 29 and 19 to directional antenna 11.
  • Rotating joint 33 and the dual coaxial line-towaveguide transition section 32 are both components which are well known in the art.
  • the entire antenna structure may be rotated about a vertical axis concentric with the longitudinal axis of center conductor 14.
  • the antenna structure is rotated about said vertical axis by means of a motor 40 and pinion gear 41 which engages internally threaded gear 42.
  • Internal gear 42 is secured to base plate 16, and is rotatably coupled to annular mounting ange 43 by means of ball bearing 44.
  • pinion gear 41 drives internal gear 32 and causes the entire antenna structure and associated transition line feeds to rotate, by means of rotating joint 33, about the vertical axis.
  • FIG. 1 The manner in which the antenna structure is secured to the aircraft frame is illustrated on the right side of FIG. 1.
  • Mounting ange 43 is secured by nut 45 to the end of a cylindrical can 46, and a radially extending flange 47 secured thereto is fixed by means of screws 48 to a bracket 49 which is secured to the aircraft frame.
  • the antenna structure is mounted so that the top of conductive plate 16 is substantially hush with the skin 50 of the aircraft.
  • p0 is the normalized radius of the feed circle
  • p is the normalized distance from the center of the lens to a point within the lens
  • 1 is the effective index of refraction
  • the leed horn 21, FIG. 1 should be close to the outer periphery of the lens.
  • a value of p0 equal to .8 was chosen as a value which would provide high aperture eticiency and also would satisfy the mechanical requirement that the waveguide feed be entirely contained within the radius of the aperture circle. This latter feature reduces the size of the structure, and allows compactness of both the antenna structure and the microwave plumbing.
  • the surface wave portion 24 of directional antenna 11 provides means for obtaining a desired directivity in the vertical plane of the radiated pattern, while at the same time provides the varying elective index of refraction medium for satisfying the Equations 1 and 2 above to provide the Luneberg lens type of focusing in the azimuth plane.
  • the necessary radial variation in the effective index of refraction in region 24 is obtained by varying the height of the dielectric material over the ground plate (conductive plate 16), and is determined according to the following equation.
  • FIGURE 3 is a plot of Equation 3 for polystyrene dielectric material whose dielectric constant 11 is 2.54, and wherein p0 is equal to .8.
  • the required varying effective index of refraction in the parallel plate region 23 of directional antenna 11 is obtained by varying the thickness of dielectric material 17 between parallel plates 13 and 16.
  • the determination ofthe contour of this tapered dielectric region may be made by referring to pages 391-393 of Waveguide Handbook by Marcuvitz, McGraw-Hil1 Book Company, 1951, wherein the author describes the propagation characteristic in a rectangular waveguide having slabs of dielectric material whose faces are perpendicular to the electric field.
  • the desired thickness of dielectric member 17 may be determined for providing the desired varying effective index of refraction.
  • the thickness of dielectric disc 17 varies in the parallel plate region 23 and in the surface wave region 24 in order to obtain the desired radial variation in the effective index of refraction.
  • Other means may be employed to achieve this result. That is, concentric rings of dielectric nifaterialshaving differing dielectric con tlyie employed to achieve this purpose.
  • the lens structure may be constructed from compressed dielectric foam, wherein the degree of cornpression determines the index of refraction, such as described in "The Luneberg Lens of Continuous Varying Dielectric Constant, by Corkum et al., October 1954, Air Force Cambridge Research Center, Publication AFCRC -TR-54-l03.
  • the elevational radiation patterns for omnidirectional antenna and directional antenna 11 are functions of the rad of the respective antennas and may be approximately determined according to the following relationship which expresses the half-power beam width of the elevational patterns:
  • Elevation half-power beam Width wherein l is equal to the radius of the omnidirectional antenna and is equal to the difference between the radii of the two parallel plates 13 and 16 for the directional antenna 11, and A0 is the free space wavelength of the energy.
  • coaxial line 25 extends between the centers of conductive plates 13 and 16 any deleterious eect which it might have on the focussing action of directional antenna 11 is substantially eliminated by providing a tuned post about said coaxial line 25.
  • the tuned post is of the type disclosed in U.S. Patent 2,528,367, and is comprised of short conductive annular cylinders 51 and 52 extending respectively from upper and lower conductive plates 13 and 16.
  • a dielectric material 53 is disposed between and within said cylinders. Cylinders S1 and 52 comprise capacitive means and the dielectric 53 comprises -inductive means therebetween. The dimensions of the respective capacitive and inductive means for optimum performance of directional antenna 11 are best determined experimentally.
  • the primary illumination function Sow) of the waveguide feed horn 21 is modified in the directional antenna -lens by the variable index of refraction medium.
  • the 'aperture illumination function S0(f) of lthe directional dens antenna may be determined by considering that the energy ow through the lens is along a ray path (solid line) FIG. 5, and considering a cone of rays (dotted lines), the total energy through any cross sectional area perpendicular to the cone axis is constant. With this assumed condition, the power flow through the incremental angle dill at the focus can be expressed as S0 (1l/)da where S0 (4f) is the power level of the primary waveguide feed -as a function of 1,0. If S0 (-r) is the power level at the aperture, the power ow through the cone at this point is S0 ('r) dy.
  • the far lield radiation pattern in the plane of the antenna may be calculated once the amplitudedistribution function of the antenna radiating aperture is known.
  • the far field radiation pattern E (6) then may be calculated from the expression A detailed analysis of the far field mapping for the type of radiation under consideration is presented in section 6.6 of Microwave Antenna Theory and Design, by Silver, McGraw-Hill Book Co., 1949.
  • FIG. 6 An alternative construction of the dual function antenna of this invention is illustrated in FIG. 6, wherein the same numerals used in FIG. l are used to designate corresponding parts.
  • the antenna structure will present even less of an aerodynamic disturbance than the embodiment illustrated in FIGS. l and 2, inasmuch as the surface of dielectric disc 12 of omnidirectional antenna 10 is exactly ush with the skin of the aircraft along a diameter of the disc.
  • the tapered portion of dielectric disc 12 is on the bottom rather than the top as illustrated in FIG. l, and similarly the tapered portion of dielectric disc 17 in the surface wave region 24 of di rectional antenna 11 is on the bottom rather than the top.
  • Upper annular conductive plate 13 is slightly conical in shape in order to conform to the tapered dielectric disc 12.
  • the bottom annular conductive plate 16 curves upwardly in the surface wave region 24 to contact the skin of the aircraft at its periphery. Despite the slightly conical shape of upper annular conductive plate 13, region 23 still may be considered as a parallel plate region.
  • the operation of the dual function antenna constructed in accordance with FIG. 6 is substantially identical with the operation of the dual function antenna illustrated in FIG. l, except that both the omnidirectional and the directional radiation patterns in the plane orthogonal to the plane of the antenna will be inclined more away from said plane of the antenna.
  • a dual function antenna for independently radiating electromagnetic energy both in a directional radiation pattern and in an omnidirectional pattern comprising iirst and second spaced parallel conductive plates, the second one of said plates extending radially beyond the periphery of the first one of said plates and each of the plates having a central aperture, a first circular dielectric lens disposed between said plates and extending to the periphery of said second plate, a second circular dielectric leus disposed on the outer surface of said first plate coaxially with respect to said apertures, each of said lenses having a radially monotonically varying index of refraction, a coaxial transmission line extending transversely through said apertures with the outer conductor of said line terminating on said first plate and the inner conductor of said line extending through the aperture of said first plate and terminating within said lens, whereby said extended center conductor comprises a probe for launching waves into said first lens, and electromagnetic energy feed means positioned in an aperture in said second plate radially beyond the periphery of said first plate for
  • a dual function antenna for independently radiating electromagnetic energy both in an omnidirectional radiation pattern and in a directional radiation pattern comprising a pair of spaced, centrally apertured, substantially parallel circular conductive plates, a conically shaped disc of low loss dielectric material having a dielectric constant diiferent from air symmetrically disposed on the outer plane surface of the first one of said plates, a coaxial transmission line extending through the central aperture of the second one of said parallel plates, the outer conductor of said line terminating on said first plate and the center conductor of said line passing through the aperture of said first plate and terminating within said dielectric disc, a dielectric lens disposed between said parallel plates and having a radially decreasing effective index of refraction, and an electromagnetic energy feed disposed adjacent the periphery of the second plate for launching electromagnetic energy diametrically across the lens disposed between said plates.
  • a dual function antenna for independently radiating electromagnetic energy both in an omnidirectional radiation pattern and in a directional radiation pattern comprising a thin circular lens having a radially varying effective index of refraction, electromagnetic energy feed means disposed adjacent the periphery of said lens for launching electromagnetic energy diametrically across said lens, a centrally apertured conductive plate disposed on an outer face of said circular lens, a disc of dielectric material having a radially varying index of refraction symmetrically disposed on the face of said plate opposite said lens thereby forming a dielectric-disc antenna, and
  • a coaxial transmission line extending transversely through -the central portion of said lens with the outer conductor of said line terminating on said plate and the center conductor extending through the central aperture of said plate and terminating within said dielectric disc for launching surface waves in said dielectric-disc antenna.
  • said omnidirectional antenna for independently radiating electromagnetic energy in respective omnidirectional and directional radiation patterns
  • said omnidirectional antenna comprising a first thin circular lens having a radially monotonically decreasing effective index of refraction and a rst centrally apertured, circular conductive plate disposed on a face of said lens, a coaxial transmission line extending normally away from said plate with the inner conductor of said line extending through said plate and terminating within said lens for launching electromagnetic waves therein
  • said directional antenna comprising said first conductive plate and a second centrally apertured, circular conductive plate coaxial with and axially spaced from said first plate and extending radially beyond said first plate, said coaxial line passing through the central aperture of said second plate
  • said directional antenna further including a second circular lens disposed between said two plates and extending to the periphery of said scci ond plate, said second lens having a radially monotonically decreasing effective index of refraction, a feed aperture in said second plate at a radial distance beyond
  • An integrally constructed dual function antenna adapted for mounting on an aircraft exterior surface comprising first and second substantially parallel circular discs of dielectric material, a thin centrally apertured conductive plate having a radius substantially equal to that of said first disc separating said two discs, a coaxial transmission line extending through said second disc and terminating within said first disc for launching electromagnetic waves therein, a second centrally apertured conductive plate disposed on the surface of said second disc opposite said first disc and extending radially beyond the periphery of said first disc, a feed aperture in said second plate at a radial distance greater than the outer radius of said first plate, a waveguide feed coupled to said feed aperture for launching electromagnetic waves which propagate through said second disc and are radiated in a collimated beam on the side of said second disc diametrically opposite said feed aperture, first and second dual concentric coaxial transmission lines coupled respectively to the coaxial transmission line terminating within said first disc and to said waveguide feed, said concentric coaxial transmission lines being coaxial with the central axis of said discs and
  • a dual function antenna for independently radiating electromagnetic energy both in a directional and an omnidirectional radiation patterns comprising a directional antenna comprised of first and second centrally apertured, circular conductive plates disposed coaxially and axially spaced with respect to each other, a first circular lens having a radially monotonically decreasing effective index of refraction disposed between said plates and extending radially to the periphery of the first of said plates,
  • said directional antenna is comprised of a parallel plate region bounded by said plates and a surface wave region extending between the peripheries of said plates, a feed aperture in said rst plate in the surface wave region thereof, a waveguide feed coupled to said aperture yfor launching electromagnetic waves which propagate from said surface wave region through said parallel plate region and are radiated in a collimated beam from lthe surface wave region diametrically opposite said feed aperture, an omnidirectional antenna comprised of the 10 second one of said plates and a circular lens having a radially monotonically decreasing effective index of refraction disposed on the face of said second plate opposite said first lens, a coaxial transmission line extending through said directional antenna with -the outer conductor of said line terminating within said second lens for launching surface waves of electromagnetic energy which are radiated in an omnidirectional radiation pattern by said second lens.

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4531129A (en) * 1983-03-01 1985-07-23 Cubic Corporation Multiple-feed luneberg lens scanning antenna system
US4698638A (en) * 1985-12-26 1987-10-06 General Dynamics, Pomona Division Dual mode target seeking system
US4742358A (en) * 1986-10-01 1988-05-03 United Technologies Corporation Multifrequency rotatable scanning prisms
US6121936A (en) * 1998-10-13 2000-09-19 Mcdonnell Douglas Corporation Conformable, integrated antenna structure providing multiple radiating apertures
US20060171076A1 (en) * 2005-01-28 2006-08-03 Hitachi Global Storage Technologies Lead configuration for reduced capacitive interference in a magnetic read/write head
FR2940380A1 (fr) * 2008-12-19 2010-06-25 Thales Sa Dispositif tournant, notamment antenne tournante

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4531129A (en) * 1983-03-01 1985-07-23 Cubic Corporation Multiple-feed luneberg lens scanning antenna system
US4698638A (en) * 1985-12-26 1987-10-06 General Dynamics, Pomona Division Dual mode target seeking system
US4742358A (en) * 1986-10-01 1988-05-03 United Technologies Corporation Multifrequency rotatable scanning prisms
US6121936A (en) * 1998-10-13 2000-09-19 Mcdonnell Douglas Corporation Conformable, integrated antenna structure providing multiple radiating apertures
US20060171076A1 (en) * 2005-01-28 2006-08-03 Hitachi Global Storage Technologies Lead configuration for reduced capacitive interference in a magnetic read/write head
FR2940380A1 (fr) * 2008-12-19 2010-06-25 Thales Sa Dispositif tournant, notamment antenne tournante

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