CA1145843A - Coaxial phased array antenna - Google Patents
Coaxial phased array antennaInfo
- Publication number
- CA1145843A CA1145843A CA000337713A CA337713A CA1145843A CA 1145843 A CA1145843 A CA 1145843A CA 000337713 A CA000337713 A CA 000337713A CA 337713 A CA337713 A CA 337713A CA 1145843 A CA1145843 A CA 1145843A
- Authority
- CA
- Canada
- Prior art keywords
- radiation
- antenna
- cavity
- balun
- monopole
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
- H01Q19/108—Combination of a dipole with a plane reflecting surface
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/24—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
- H01Q21/26—Turnstile or like antennas comprising arrangements of three or more elongated elements disposed radially and symmetrically in a horizontal plane about a common centre
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0006—Particular feeding systems
- H01Q21/0075—Stripline fed arrays
Abstract
Abstract of the Disclosure Disclosed is a coaxial antenna array for communicating circularly polarized electromagnetic radiation. A pair of open ended antenna cavities is coaxially constructed and operates by excitation of linear radiation elements arranged within each of the cavities. A pair of crossed-dipole radiation devices are centered within the inner cavity and operated by means of a phase-shifting network circuit to transmit as well as receive circularly polarized radiation. Four monopole radiation devices are symmetrically arranged to operate in the outer cavity in phase quadrature by means of the phase-shifting network circuit to also both transmit and receive circularly polarized electromagnetic radiation. Combined operation of the two antenna cavities with a 180° phase differential between the fields related to the two antenna cavities provides a broad beam, relatively wide frequency bandwidth communication capability. Particular embodiments disclosed feature a generally square cavity array as well as a circular cavity array.
Description
The invention described herein was made in the performance of work under a NASA contract and is subject to the provisions of Section 305 o~ the National Aeronautics and Space Act of 1~58, Public Law 85-568 (72 Stat. 435 U.S.C. 2457).
Specification The present invention relates to antennas for transmitting and/or receiving circularly polarized electromagnetic radiation by means of linear radiation excitation elements arranged in coaxially arrayed cavities. Antennas constructed in accordance with the present invention are particularly suitable for flush mounting in high-altitude aircraft or spacecraft, where communicatii'on by means of circularly polarized radiation is often utilized to minimize signal degradation due to polarization effects at boundaries between atmospheric layers.
In contrast to previously known flush mounting antennas of comparable dimensions, the antenna assembly of the present invention exhibits a broader frequency bandwidth in both the transmitting and receiving modes.
In addition, the present antenna assembly -is characterized by a wider effective radiation pattern than prior flush mounting antennas, thereby reducing the number of antenna assemblies that are needed to insure reliable communication with an aircraft or spacecraft regardless of its physical orientation. Due to its coaxial layout, ~oreover, the present antenna assembly may be constructed compactly and operated in a limited aperture installation.
~1'15~3~3 In accordance with one aspect of this invention there is provided an antenna assembly for communicating electromagnetic radiation comprising: a) first antenna cavity means; b) second antenna cavity means, generally circumscribing said first antenna cavity means and su~- -stantially axially coextensive therewith, said first and second cavity means possessing a common central, longi-tudinal axis; c) first and second dipole radiation means, positioned in crossed-dipole configuration within said first antenna cavity means; and d) first, second, third, and fourth monopole radiation means positioned symmetri-cally relative to said second antenna cavity means for excitation therein.
In accordance with another aspect of this invention there is provided an antenna assembly for communicating electromagnetic radiation comprising a coaxial array of two open-ended cavities with double dipole radiation elements positioned for excitation within the inner cavity of the array, and four monopole radihtion elements symmetrically 20 positioned for excitation within the outer cavity of the array, said radiation elements coupled through feed means to a network in phased array to transmit or receive cir-cularly polarized radiation.
The manner of making and using an antenna assembly in accordance with the present invention, and the various alternative embodiments thereof, will be fully apprehend-ed from the following specification and from the appended drawings, in which:
-2a-58~3 Fig. 1 is a perspective view of a coaxial phased array antenna assembly according to the present invention;
Fig. 2 is a plan view of the antenna assembly shown in Fig. l;
Fig. 3 is a cross sectional view taken along line 3-3 of Figr 2;
Fig. 4 is an enlarged cross sectional view of a dipole radiation device taken along line 4-4 in Fig. 2, and showing details of the balun structure, Fig. 5 is a plan view of an embodiment of the present invention featuring circular cavities;
Fig. 6 is a schematic diagram of a network circuit which may be utilized to operate the present antenna assembly;
Fig. 7 is a graphical representation of a radiation pattern which may be generated by use of the crossed-dipole section of the antenna assembly alone; and Fig. 8 is a graphical representation of a radiation pattern which may be generated by use of the multiple monopole section of the antenna assembly alone; and Fig. 9 is a graphical representation of a radiation pattern that may be generated by illuminating both the monopole and dipole antenna sections according to the present invention.
An antenna assembly according to the present invention is shown generally at lO in Figs. 1 and 2. A pair of walls 12 and 14 cooperate with a base 16 (Fig. 3) to define inner and outer cavities A and B, respectively. The inner cavity A is limited by the interior surface of the inner wall 12 and the top surface of the cavity base 16. The outer cavity B is limited by the interior surface of the outer wall 14, the ¦¦exterior surface of the inner wall 12, and the top surface of ~¦the cavity base 16.
1145~3~3 It may best be appreciated from Fig. 2 that the inner cavity A is square in horizontal cross section, and the outer cavity B forms a square with a central square portion, established by the exterior surface of the interior wall 12, removed. It will be appreciated that the inner and outer walls are mutually coaxial, and the two cavities A and B are also mutually coaxial. Further, the two cavities A and B have a common center as well as mutually parallel corresponding sides. As Figs. 1 and 3 show, the cavities A and B are also gene~ally axially coextensive, with their respective bottoms at the same axial location, defined by the top surface of the same base 16. The height of the outer wall 14 is slightly greater than that of the inner wall 12, for a purpose discussed hereinafter.
A pair of dipole electromagnetic radiation devices shown generally at 18 and 20 are arranged within the inner cavity A in a crossed-dipole configuration~ Monopole radiation devices 22, 24, 26 and 28 are located at the four corners of the interior wall 12.
The configurations and structures of the radiation devices may be especially appreciated by reference to Figs. 3 and 4.
In particular, dipole device 20 is shown in Fig. 4 to be supported on the base 16 by a balun 30 including a balanced post 30a and an unbalanced post 30b. The balanced post 30a is a coaxial structure containing, as a central core, a transmission line 32 which extends from below the base 16, up through the balun post 30a and over to the top of the unbalanced portion 30b to which the transmission line is mechanically and electrically anchored. Both balun portions 30a and 30b are made of conducting material such as metal. However, within the I
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~1458~3 balanced post 30a the transmission line 32 is electrically insulated from the conducting outer portion of the balun by a dielectric material 34.
As seen in Figs. 3 and 4, the dielectric material 34 contained in the balanced segments of the baluns of all the radiation devices varies in thic~ness between a relatively wide section in the upper portion of the balun segment to a relatively narrow section in the lower portion of the balun segment. The transition between the two sections of different thickness in a particular balun is marked by a shoulder such as 30c in the balanced balun segment 30a.
The dielectric material 34 serves as a transmission line transformer for the corresponding radiation device. It is known to vary the length of the wider section of the dielectric 34 to vary the impedance of the transmission line and radiation device combination to match the network feeding the transmission line.
Further, it is known to vary the dimensions of an antenna cavity and associated radiation devices to vary the center of the wavelength band of radiation able to be communicated by such an antenna assembly. In particular, with a structure such as cavity A and radiation devices 18 and 20, the height of the radiation devices is chosen to be approximately one quarter of the wavelength of the center of the excitation band. The same relationship between radiation device height and radiation excitation frequency applies to the exterior cavity B and associated radiation devices 22 through 28.
- The dipole radiation device 2~ is equipped with a pair of radiation elements 36 and 38, each radiation element supported by separate balun segment 30a and 30b, respectively. The radiation elements 36 and 38 are oriented along a common direction but extend in opposite senses.
I - 1145~3~3 m e other dipole radiation device at 18 is constructed similarly to dipole radiation device 20, with a two-post balun 40 (Figs. 3 and 4) and transmission line 42. Also, the posts of the balun 40 are each fitted with a radiation element 44 and 46, respectively. The radiation elements 44 and 46 are likewise orien~ed to extend in opposite senses along a common direction.
! As clearly visible in Figs. 1 and 2, the dipole radiation devices at 18 and 20 are positioned and oriented within the inner cavity A such that the four balun posts in question are arranged in a sauare centered on the center of the cavity A, and such that balun posts of the same radiation device are located at opposite corners of the balun post square. The two transmission lines 32 and 42 cross at approximately the center of the cavity A without making mutual electrical contact. The direction along which the radiation elements 36 and 38 are oriented is orthognal to the direction along which the radiation elements 44 and 46 are oriented. These directions lie in mutually orthogonal planes which include the common central longitudinal axis of both cavities A and B.
Each of the monopole radiation devices 22-28 is constructed in a manner similar to that of each of the dipole radiation devices 18 and 20. The similarities and the differences in construction between the two types of radiation devices may best be appreciated by reference to Figs. 2 and 3. Thus, for example, monopole radiation device 22 includes a balun 48 with balanced and unbalanced balun segments 48a and 48b, respectively.
The balanced balun segment 48a includes a transmission line 50 passing therethrough and crossing over to connect with the top of the unbalanced balun post 48b. The transmission line 50 ~¦is insulated from the conducting material of the balanced post ¦ 48a by dielectric material 52 serving as the transmission line transformer, and which varies in thickness with the transition between different thicknesses marked by a shoulder 48c.
11 ~1458~3 The two balun posts 48a and 48b of the monopole radiation device 22 straddle the inner wall 12 at one corner thereof.
Similarly, each of the other monopole radiation devices 2~-28 include a balun constructed of two posts which also straddle the inner wall 12, one such monopole device located at each corner of the ~all 12. The monopole radiation device at 22 includes only one radiation element 54, supported by the balun post exterior of the inner wall 12. Similarly, each o~ the other . three monopole radiation devices 24, 26 and 28 possesses only one radiation element 56, 58, and 60, respectively, all monopole radiation elements being positioned within the outer cavity B.
All of the radiation elements 54-60 of the monopole radiation devices are oriented to extend generally away from the inner cavity A. Thus, as may be appreciated from Figs. 1 and 2, two monopole radiation devices 22 and 26 are positioned mutually diametrically opposed across the interior cavity A with their respective radiation elements 54 and 58 lying generally along the direction of orientation of the dipole radiation elements 36 and 38, and extending in opposite senses away from the common central longitudinal axis of the two cavities A and B. Similarly, the other two monopole radiation devices at 24 and 28 are positioned mutually diametrically opposed across the interior cavity A with their respective radiation elements 56 and 60 extending away from the interior cavity in opposite senses along the same direction as the direction of orientation of the dipole radiation elements 44 and 46.
In the case of three of the monopole radiation devices 24-28, the transmission lines are carried by the balun posts located within the inner wall 12, while the transmission line of the fourth monopole radiation device at 22 is carried by the balun post located in the exterior cavity B. This latter 458~3 monopole radiation device at 22 is also located adjacent the radiation element 38 supported by the unbalanced balun post of the dipole radiation device at 20.
The relationship between the positioning of the balanced and unbalanced segments of the diametrically positioned monopole radiation devices at 22 and 26 establishes a 180 phase relationship between the excitation of the corresponding radiation elements 54 and 58. Then, with the network circuit shown and described hereinafter, circularly polarized electromagnetic radia~ion may be both received and transmitted by the monopole antenna array in the outer cavity B.
Similarly, the crossed-dipole arrangement of the dipole radiation devices at 18 and 20 within the inner cavity A enables circularly polarized electromagnetic radiation to be both received and transmitted by the dipole antenna ararngement of the inner cavity.
A network for operating the antenna assembly to both receive and transmit electromagnetic signals is shown schematically in Fig. 3 at 62. A dielectric lamina, such as a film strip, 64 may typically be used as a base or substrate for the network components. The network circuit may be constructed by depositing copper or other conducting material on one or both sides of the base 64, and attaching additional circuit components thereto. As one alternative, the network circuit may be constructed by beginning with a laminar sandwich of a conducting plane and a dielectric substrate, and possibly a second conducting plane on the opposite side of the substrate, and selectively etching material from the one or more conducting planes to leave a circuit on the substrate as required.
These and other strip line circuit construction techniques are well known, and will not be further discussed herein.
I
11~58~3 The various transmission lines, such as 50, extend down from the balanced balun segments through appropriate holes in the cavity base 16 and to the area of the network circuit as shown. At the network base 64, the transmission lines are joined to the network circuit at connections, or traces, 66.
The network circuit may be enclosed in additional dielectric material 68 which isolates the network circuit from a surrounding housing made of electrically conducting material 70. The conducting housing 70 serves as a ground plane for the transmission network. Appropriate passageways are provided, ~uch as 70a, for passing the transmission lines from the radiation devices through the ground plane housing 70 to the network circuit The dielectric material 14 within the balanced balun posts may continue downwardly through the cavity base 15 and the passage-ways 70a to insure that the transmission lines are insulated from these two conducting objects.
The continuations of the transmission lines directly to the network circuit 62 act as feed lines between the network circuit and the radiation devices. While the present arrange-ment indicated in Fig. 3 has the advantage of a compact construction, the network circuit itself may be provided at a location remote from the antenna assembly proper. ~n such case, more extensive lines must connect the network circuit to the radiation devices. Also, the transmission line transformers withi the balanced balun posts, exhibited by the wide and narrow segments of the dielectric material 34, must be provided so as to insure a proper impedance match along the network circuit-feed line-transmission line hookup.
A typical network circuit that may be utilized in operating the antenna assembly of the present invention for transmitting or receiving circularly polarized electromagnetic radiation is sh~wn schematically in ~ig. 6. The signal to 11458~3 be transmitted by the antenna assembly is introduced to the network circuit at the input 72 to a coupler 74. The coupler 74 is essentially an inductive device which passes the input signal to an output 74a and excites the same frequency signal, with a 180 phase shift, in a parallel branch output at 74b.
The opposite end of the parallel branch is an isolation port 74c, which terminates the induced signal to the ground plane through an impedance matching device. The coupler 74, as well as the remaining ci~cuit devices to be described, is a conventiona device well known in the strip line circuitry field, and will not be discussed in further detail herein.
The output signals at 74a and 74b from the coupler 74 are fed to combination signal splitters and phase shifters 76 and 78, respectively. Each of these elements 76 and 78 is a 3 DB 90 phase shifting hybrid power divider. Thus, for example, the hybrid power divider 76 feeds the input signal from 74a to two output terminals 76a and 76b, at equal power levels, but 90 out of phase. Inductive coupling is used between the input circuit, which terminates at an isolation port 76c, and the output circuit with output terminals 76a and 76b. Thus, two output signals are produced by the signal splitter at terminals 76a and 76b, which output signals are essentially identical in all respect, with the exception that the two output signals are mutually 90 out of phase. Similarly, the signal splitter 78 provides two essentially identical ouput signals at terminals 78a and 78b, which signals are also 90~ out of phase.
The two output signals from the signal splitter 78 are fed to separate 3 DB power dividers 80 and 82. Each of these two elements 80 and 82 functions to split its input signal to provide two output signals v~ich are essentially identical in 1~ -10-58~3 all respects, and mutually in phase as well. Thus, output ~ignals are provided at the power divider terminals 80a and 80b which are mutually in phase, and output signals are provided at the power divider terminals 82a and 82b which are also mutually in phase. However, there is a 90 phase differential between the signals from terminals 80a and 80b compared to the signals from terminals 82a and 82b due to the phase shift effected by the hybrid pouer divider 78.
The output signals from the hybrid signal splitter 76 are fed to the two dipole radiation devices 18 and 20, respectively, represented symbolically in Fig. 6 as elements 1 and 2. The output signals from the power divider 80 are similarly fed to the diametrically opposed monopole radiation devices 28 and 24, represented symbolically as elements 3 and 4, respectively.
Also, the output signals from the power divider 82 are fed to the remaining diametrically opposed monopole radiation devices 26 and 22, represented symbolically by elements 5 and 6, respectively. The dipole radiation devices within the inner cavity A thus receive their signals 90 out of phase. The resulting signal transmitted by the inner cavity portion of the antenna assembly is circularly polarized. It will be appreciated that the sense of rotation of the circularly polarized electro-magnetic radiation thus transmitted by the inner cavity portion of the antenna assembly is determined by the sense of the phase shift provided by the hybrid signal splitter 76. Therefore, by reversing the feed connections between the dipole radiation devices 18 and 20 relative to the signal splitter 76, the sense of rotation of the circularly polarized electromagnetic radiation transmitted by the inner cavity portion of the antenna assembly may be reversed.
458~3 As noted hereinbefore, the two monopole radiation devices 24 and 28 receive their two signals in phase, but 90 out of phase relative to the reception of the two signals by the remaining two monopole radiation devices 22 and 26. However, the feed to the monopole radiation device 22 is effected through the balun post which supports the radiation element 54, as opposed to the feeding of the other three monopole radiation devices occuring through the balun posts located within the .
inner cavity A. This difference in feed to the two diametrically opposed monopole radiation devices 22 and 26, which otherwise receive their input signals from the power divider 82 in phase, effects a 180 phase shift in the signals actually transmitted by the two radiation elements 54 and 58. Thus, by a combination of the phase shifting effected in the network circuitry as illustrated in Fig. 6 and the construction and positioning of the various monopole radiation devices 22 through 28, the sig~al provided by element 58 is 90 .
out of phase with the signals provided by elements 56 and 609 which are mutually in phase and 90~ out of phase with the signal provided by element 54. Also, there is a 180~ phase differential between the signals provided by elements 58 and 54. Thus, the total signal transmitted by the outer cavity portion of the antenna assembly is also circularly polarized. Furthermore, the sense of rotation of the circularly polarized signal thus transmitted by the outer portion of the antenna assembly may be reversed by simply reversing the output terminal connections of the hybrid signal splitter 78.
Excitation by the dipole radiation elements within the inner cavity A results in the transmission of a circularly ~)olarized signal. Similarly, excitation of the monopole ~1458~3 radiation elements in the outer cavity B of the antenna assembly results in the transmission of a circularly polarized signal as well. Due to the phase shift effected by the coupler 74, the dipole radiation elements illuminate the inner cavity 180 out of phase with the illumination of the outer cavity B effected by the monopole radiation elements. With the coaxial arrangement of the two antenna portions, the two individual signals then combine to a single signa~ of circularly polarized electro-magnetic radiation, whose rotational sense may be reversed by simply reversing the feed line connections of the two hybrid signal splitters 76 and 78 as noted hereinbefore.
The general radiation pattern characteristic of the inner cavity A illuminated by the crossed-dipole radiation elements is illustrated in Fig. 7 for a plane perpendicular to the aperture of the cavity A. Similarly, the general pattern of radiation characteristic of the outer cavity B as illuminated by the four monopole radiation devices operated in phase quadrature is illustrated in Fig. 8 for a plane normal to the aperture of the outer cavity B. The combined antenna assembly with the inner and outer cavities illuminated 180~ out of phase as discussed hereinbefore generates a radiation pattern as given by Fig. 9 for a plane normal to the apertures of both cavities A and B. It will be appreciated, by a compari~on of Figs. 7-9, that the coaxial array of antenna cavities illuminated by linear radiation elements excited according to the phas~
relationships described hereinbefore provides a radiation pattern of greater effective beam width than that of either of the antenna cavities operated alone. Further, the frequency bandwidth produced in the transmitted signals by the coaxial antenna ~array of the present invention is broader than that obtainable by either of the two antenna cavity portions operating alone.
1~58~3 The coaxial array antenna assembly of the present invention is also operable to receive circularly polarized electromagnetic radiation. In such case, the antenna assembly operates as a receiving antenna, with the incoming signals entering the cavities A and B and exciting both the dipole and monopole radiation elements. The received signals are then fed along the transmission lines of the six radiation devices through the feed connectors to the network circuitry previously described. The network circuit of the type illustrated in Fig. 6 operates to combine the individual signals induced in the various radiation devices. Then, the signal splitters 76-82 combine paired signals input thereto at the respective terminals previously identified as output terminals. Finally, the coupler 74 combines the two signals received by the inner and outer cavity antenna portions into a single signal presented at 72. The signal thus received by the antenna array and processed by the network circuit of Fig. 6 is provided for further processing by conventional receiver or other equipment.
For the purpose of flush mounting the antenna assembly in a spacecraft or other vehicle, the outer cavity wall 14 may be extended slightly above the height of the inner cavity wall 12, and provided with an externally extended flange 14a as shown in Figs. 1-3. The flange 14a may serve to facilitate the installation of the antenna array with an outer covering 84 as illustrated by dashed lines in Fig. 2. The greater height of the outer wall 14a above the base 16 compared to the height of the inner wall 12 raises the covering 84 above the top of the inner wall 12 and the balun posts of the radiation elements to accomodatl , the extension of the transmission lines above the balun posts.
1 ,, 1~ 11458~3 The covering 84 may include various environmental pro-tection elements~ such as a heat shield, but it must be at least partially transparent to electromagnetic radiation in the frequency range of communication by the antenna assembly.
The present invention may also be constructed in the form ¦ of coaxial circular antenna cavities as illustrated in Fig. 5 ¦ wherein certain elements which may be essentially identical in structure and/or function to those previously described are identified by numerals differing in value by 100 from the numerals used to identify the corresponding elements.
An inner antenna cavity C is limited by an inner circular wall 112 and the top surface of a cavity base 116. An outer antenna cavity D is defined by the inner surface of an outer circular wall 114, the outer surface of the inner wall 112, and the top surface of the cavity base 116. The outer wall 114 is fitted with a top outwardly extending flange 114a for purposes of mounting and/or covering the antenna array as discussed hereinbefore in relation to the square antenna array embodiment.
A crossed-dipole configuration, including dipole radiation devices 118 and 120 is centered within the inner cavity C. The dipole radiation device 118 includes radiation elements 144 and 146 extending in opposite senses along one diameter of the inner cavity circular cross section; the other dipole radiation device 120 includes radiation elements 136 and 138 extending in oppo~ite senses along a second diameter of the inner cavity C cross section which second diameter is perpendicular to the first diameter. , The radiation elements of the dipole devices 118 and 12~
are of the same type as those of the dipole devices 18 and 20 ~of the previously discussed embodiment. Thus, all such dipole radiation elements of both embodiments are in the general form of planar, radially extending flags lying in planes which include the longitudinal axis of the corresponding inner cavity.
As in the case of the square antenna array embodimen~, the circular antenna array includes four monopole radiation devices for excitation in the outer cavity D. Radiation devices 122 and 126 are positioned mutually diametrically opposed along the direction of orientation of the dipole device 120. Similarly, monopole radiation devices 124 and 128 are positioned mutually diametrially opposed along the direction of orientation of the dipole device 118.
Analagously to.the square embodiment, the balun posts-of the monopole radiation devices of the circular array straddle the inner circular wall 112. Further, three of the nopole devices 124, 126, and 128 are fed by transmission lines passing through balanced balun posts located within the inner wall 112, while the fourth monopole device is structured with its balanced balun post located in the outer cavity D. This particular monopole device 122 is.also positioned with its unbalanced balun post adjacent the radiation element 138 supported by an unbalanced balun post of the dipole radiation device 120.
The various transmission lines in each case also cross from the balanced posts to the unbalanced balun posts for each radiation device.
The monopole radiation devices 122-128 of the circular embodiment include radiation elements 154, 156, 158 and 160, respectively, in the general form of planar flags of a.pie-cut type shape, lying in a common plane perpendicular to the common longitudinal axis of the two cavities C and D, and positioned in the vicinity of the top of the various balun posts. Further, each of the flag elements 154-160 is positioned symmetrically about the diameters of the cavities C and D along which the radiation device of which the flag is a part is positioned.
11458~3 The performance of the antenna array with generally circular cavities is generally the same as that previously des-cribed in connection with the square antenna array assembly.
Thus, the individual cavities C and D, being illuminated separately, may be expected to provide radiation patterns as illustrated in Figs. 7 and 8, respectively, while the com~ined signal radiation pattern obtained by operating both cavities C
and D together resembles that illustrated in Fig. 9. Thus, the broadened radiation beam width as well as extended frequency bandwidth may be achieved by constructing the coaxial antenna array of the present invention in either a generaily square or circular pattern. Further, the network circuitry shown in Fig. 6, and the general construction of the network and feed connections illustrated in Fi8. 3 and described in connection therewith may be employed with the circular type antenna array of the present invention for both transmitting and receiving circularly polarized electromagnetic radiation. Then, for example, radiation devices 118, 120, 122, 124, 1~6 and 128 may be represented in Fig. 6 as elements 1, 2, 6, 4, 5, and 3, respectively.
In a particularly advantageous application, four individual coaxial-antenna assemblies according to the present invention may be spaced apart 90 about the roll plane of a spacecraft to utilize the 1n~ steradian coverage of the radiation pattern exhibited by one such antenna assembly, as illustrated in Fig. 8.
The foregoing disclosure and description of the invention is illustrative and explanatory thereof, and various changes in the details of the illustrated apparatus may be made within the ~cope of the appended claims without departing from the spirit of the invention.
Specification The present invention relates to antennas for transmitting and/or receiving circularly polarized electromagnetic radiation by means of linear radiation excitation elements arranged in coaxially arrayed cavities. Antennas constructed in accordance with the present invention are particularly suitable for flush mounting in high-altitude aircraft or spacecraft, where communicatii'on by means of circularly polarized radiation is often utilized to minimize signal degradation due to polarization effects at boundaries between atmospheric layers.
In contrast to previously known flush mounting antennas of comparable dimensions, the antenna assembly of the present invention exhibits a broader frequency bandwidth in both the transmitting and receiving modes.
In addition, the present antenna assembly -is characterized by a wider effective radiation pattern than prior flush mounting antennas, thereby reducing the number of antenna assemblies that are needed to insure reliable communication with an aircraft or spacecraft regardless of its physical orientation. Due to its coaxial layout, ~oreover, the present antenna assembly may be constructed compactly and operated in a limited aperture installation.
~1'15~3~3 In accordance with one aspect of this invention there is provided an antenna assembly for communicating electromagnetic radiation comprising: a) first antenna cavity means; b) second antenna cavity means, generally circumscribing said first antenna cavity means and su~- -stantially axially coextensive therewith, said first and second cavity means possessing a common central, longi-tudinal axis; c) first and second dipole radiation means, positioned in crossed-dipole configuration within said first antenna cavity means; and d) first, second, third, and fourth monopole radiation means positioned symmetri-cally relative to said second antenna cavity means for excitation therein.
In accordance with another aspect of this invention there is provided an antenna assembly for communicating electromagnetic radiation comprising a coaxial array of two open-ended cavities with double dipole radiation elements positioned for excitation within the inner cavity of the array, and four monopole radihtion elements symmetrically 20 positioned for excitation within the outer cavity of the array, said radiation elements coupled through feed means to a network in phased array to transmit or receive cir-cularly polarized radiation.
The manner of making and using an antenna assembly in accordance with the present invention, and the various alternative embodiments thereof, will be fully apprehend-ed from the following specification and from the appended drawings, in which:
-2a-58~3 Fig. 1 is a perspective view of a coaxial phased array antenna assembly according to the present invention;
Fig. 2 is a plan view of the antenna assembly shown in Fig. l;
Fig. 3 is a cross sectional view taken along line 3-3 of Figr 2;
Fig. 4 is an enlarged cross sectional view of a dipole radiation device taken along line 4-4 in Fig. 2, and showing details of the balun structure, Fig. 5 is a plan view of an embodiment of the present invention featuring circular cavities;
Fig. 6 is a schematic diagram of a network circuit which may be utilized to operate the present antenna assembly;
Fig. 7 is a graphical representation of a radiation pattern which may be generated by use of the crossed-dipole section of the antenna assembly alone; and Fig. 8 is a graphical representation of a radiation pattern which may be generated by use of the multiple monopole section of the antenna assembly alone; and Fig. 9 is a graphical representation of a radiation pattern that may be generated by illuminating both the monopole and dipole antenna sections according to the present invention.
An antenna assembly according to the present invention is shown generally at lO in Figs. 1 and 2. A pair of walls 12 and 14 cooperate with a base 16 (Fig. 3) to define inner and outer cavities A and B, respectively. The inner cavity A is limited by the interior surface of the inner wall 12 and the top surface of the cavity base 16. The outer cavity B is limited by the interior surface of the outer wall 14, the ¦¦exterior surface of the inner wall 12, and the top surface of ~¦the cavity base 16.
1145~3~3 It may best be appreciated from Fig. 2 that the inner cavity A is square in horizontal cross section, and the outer cavity B forms a square with a central square portion, established by the exterior surface of the interior wall 12, removed. It will be appreciated that the inner and outer walls are mutually coaxial, and the two cavities A and B are also mutually coaxial. Further, the two cavities A and B have a common center as well as mutually parallel corresponding sides. As Figs. 1 and 3 show, the cavities A and B are also gene~ally axially coextensive, with their respective bottoms at the same axial location, defined by the top surface of the same base 16. The height of the outer wall 14 is slightly greater than that of the inner wall 12, for a purpose discussed hereinafter.
A pair of dipole electromagnetic radiation devices shown generally at 18 and 20 are arranged within the inner cavity A in a crossed-dipole configuration~ Monopole radiation devices 22, 24, 26 and 28 are located at the four corners of the interior wall 12.
The configurations and structures of the radiation devices may be especially appreciated by reference to Figs. 3 and 4.
In particular, dipole device 20 is shown in Fig. 4 to be supported on the base 16 by a balun 30 including a balanced post 30a and an unbalanced post 30b. The balanced post 30a is a coaxial structure containing, as a central core, a transmission line 32 which extends from below the base 16, up through the balun post 30a and over to the top of the unbalanced portion 30b to which the transmission line is mechanically and electrically anchored. Both balun portions 30a and 30b are made of conducting material such as metal. However, within the I
.
~1458~3 balanced post 30a the transmission line 32 is electrically insulated from the conducting outer portion of the balun by a dielectric material 34.
As seen in Figs. 3 and 4, the dielectric material 34 contained in the balanced segments of the baluns of all the radiation devices varies in thic~ness between a relatively wide section in the upper portion of the balun segment to a relatively narrow section in the lower portion of the balun segment. The transition between the two sections of different thickness in a particular balun is marked by a shoulder such as 30c in the balanced balun segment 30a.
The dielectric material 34 serves as a transmission line transformer for the corresponding radiation device. It is known to vary the length of the wider section of the dielectric 34 to vary the impedance of the transmission line and radiation device combination to match the network feeding the transmission line.
Further, it is known to vary the dimensions of an antenna cavity and associated radiation devices to vary the center of the wavelength band of radiation able to be communicated by such an antenna assembly. In particular, with a structure such as cavity A and radiation devices 18 and 20, the height of the radiation devices is chosen to be approximately one quarter of the wavelength of the center of the excitation band. The same relationship between radiation device height and radiation excitation frequency applies to the exterior cavity B and associated radiation devices 22 through 28.
- The dipole radiation device 2~ is equipped with a pair of radiation elements 36 and 38, each radiation element supported by separate balun segment 30a and 30b, respectively. The radiation elements 36 and 38 are oriented along a common direction but extend in opposite senses.
I - 1145~3~3 m e other dipole radiation device at 18 is constructed similarly to dipole radiation device 20, with a two-post balun 40 (Figs. 3 and 4) and transmission line 42. Also, the posts of the balun 40 are each fitted with a radiation element 44 and 46, respectively. The radiation elements 44 and 46 are likewise orien~ed to extend in opposite senses along a common direction.
! As clearly visible in Figs. 1 and 2, the dipole radiation devices at 18 and 20 are positioned and oriented within the inner cavity A such that the four balun posts in question are arranged in a sauare centered on the center of the cavity A, and such that balun posts of the same radiation device are located at opposite corners of the balun post square. The two transmission lines 32 and 42 cross at approximately the center of the cavity A without making mutual electrical contact. The direction along which the radiation elements 36 and 38 are oriented is orthognal to the direction along which the radiation elements 44 and 46 are oriented. These directions lie in mutually orthogonal planes which include the common central longitudinal axis of both cavities A and B.
Each of the monopole radiation devices 22-28 is constructed in a manner similar to that of each of the dipole radiation devices 18 and 20. The similarities and the differences in construction between the two types of radiation devices may best be appreciated by reference to Figs. 2 and 3. Thus, for example, monopole radiation device 22 includes a balun 48 with balanced and unbalanced balun segments 48a and 48b, respectively.
The balanced balun segment 48a includes a transmission line 50 passing therethrough and crossing over to connect with the top of the unbalanced balun post 48b. The transmission line 50 ~¦is insulated from the conducting material of the balanced post ¦ 48a by dielectric material 52 serving as the transmission line transformer, and which varies in thickness with the transition between different thicknesses marked by a shoulder 48c.
11 ~1458~3 The two balun posts 48a and 48b of the monopole radiation device 22 straddle the inner wall 12 at one corner thereof.
Similarly, each of the other monopole radiation devices 2~-28 include a balun constructed of two posts which also straddle the inner wall 12, one such monopole device located at each corner of the ~all 12. The monopole radiation device at 22 includes only one radiation element 54, supported by the balun post exterior of the inner wall 12. Similarly, each o~ the other . three monopole radiation devices 24, 26 and 28 possesses only one radiation element 56, 58, and 60, respectively, all monopole radiation elements being positioned within the outer cavity B.
All of the radiation elements 54-60 of the monopole radiation devices are oriented to extend generally away from the inner cavity A. Thus, as may be appreciated from Figs. 1 and 2, two monopole radiation devices 22 and 26 are positioned mutually diametrically opposed across the interior cavity A with their respective radiation elements 54 and 58 lying generally along the direction of orientation of the dipole radiation elements 36 and 38, and extending in opposite senses away from the common central longitudinal axis of the two cavities A and B. Similarly, the other two monopole radiation devices at 24 and 28 are positioned mutually diametrically opposed across the interior cavity A with their respective radiation elements 56 and 60 extending away from the interior cavity in opposite senses along the same direction as the direction of orientation of the dipole radiation elements 44 and 46.
In the case of three of the monopole radiation devices 24-28, the transmission lines are carried by the balun posts located within the inner wall 12, while the transmission line of the fourth monopole radiation device at 22 is carried by the balun post located in the exterior cavity B. This latter 458~3 monopole radiation device at 22 is also located adjacent the radiation element 38 supported by the unbalanced balun post of the dipole radiation device at 20.
The relationship between the positioning of the balanced and unbalanced segments of the diametrically positioned monopole radiation devices at 22 and 26 establishes a 180 phase relationship between the excitation of the corresponding radiation elements 54 and 58. Then, with the network circuit shown and described hereinafter, circularly polarized electromagnetic radia~ion may be both received and transmitted by the monopole antenna array in the outer cavity B.
Similarly, the crossed-dipole arrangement of the dipole radiation devices at 18 and 20 within the inner cavity A enables circularly polarized electromagnetic radiation to be both received and transmitted by the dipole antenna ararngement of the inner cavity.
A network for operating the antenna assembly to both receive and transmit electromagnetic signals is shown schematically in Fig. 3 at 62. A dielectric lamina, such as a film strip, 64 may typically be used as a base or substrate for the network components. The network circuit may be constructed by depositing copper or other conducting material on one or both sides of the base 64, and attaching additional circuit components thereto. As one alternative, the network circuit may be constructed by beginning with a laminar sandwich of a conducting plane and a dielectric substrate, and possibly a second conducting plane on the opposite side of the substrate, and selectively etching material from the one or more conducting planes to leave a circuit on the substrate as required.
These and other strip line circuit construction techniques are well known, and will not be further discussed herein.
I
11~58~3 The various transmission lines, such as 50, extend down from the balanced balun segments through appropriate holes in the cavity base 16 and to the area of the network circuit as shown. At the network base 64, the transmission lines are joined to the network circuit at connections, or traces, 66.
The network circuit may be enclosed in additional dielectric material 68 which isolates the network circuit from a surrounding housing made of electrically conducting material 70. The conducting housing 70 serves as a ground plane for the transmission network. Appropriate passageways are provided, ~uch as 70a, for passing the transmission lines from the radiation devices through the ground plane housing 70 to the network circuit The dielectric material 14 within the balanced balun posts may continue downwardly through the cavity base 15 and the passage-ways 70a to insure that the transmission lines are insulated from these two conducting objects.
The continuations of the transmission lines directly to the network circuit 62 act as feed lines between the network circuit and the radiation devices. While the present arrange-ment indicated in Fig. 3 has the advantage of a compact construction, the network circuit itself may be provided at a location remote from the antenna assembly proper. ~n such case, more extensive lines must connect the network circuit to the radiation devices. Also, the transmission line transformers withi the balanced balun posts, exhibited by the wide and narrow segments of the dielectric material 34, must be provided so as to insure a proper impedance match along the network circuit-feed line-transmission line hookup.
A typical network circuit that may be utilized in operating the antenna assembly of the present invention for transmitting or receiving circularly polarized electromagnetic radiation is sh~wn schematically in ~ig. 6. The signal to 11458~3 be transmitted by the antenna assembly is introduced to the network circuit at the input 72 to a coupler 74. The coupler 74 is essentially an inductive device which passes the input signal to an output 74a and excites the same frequency signal, with a 180 phase shift, in a parallel branch output at 74b.
The opposite end of the parallel branch is an isolation port 74c, which terminates the induced signal to the ground plane through an impedance matching device. The coupler 74, as well as the remaining ci~cuit devices to be described, is a conventiona device well known in the strip line circuitry field, and will not be discussed in further detail herein.
The output signals at 74a and 74b from the coupler 74 are fed to combination signal splitters and phase shifters 76 and 78, respectively. Each of these elements 76 and 78 is a 3 DB 90 phase shifting hybrid power divider. Thus, for example, the hybrid power divider 76 feeds the input signal from 74a to two output terminals 76a and 76b, at equal power levels, but 90 out of phase. Inductive coupling is used between the input circuit, which terminates at an isolation port 76c, and the output circuit with output terminals 76a and 76b. Thus, two output signals are produced by the signal splitter at terminals 76a and 76b, which output signals are essentially identical in all respect, with the exception that the two output signals are mutually 90 out of phase. Similarly, the signal splitter 78 provides two essentially identical ouput signals at terminals 78a and 78b, which signals are also 90~ out of phase.
The two output signals from the signal splitter 78 are fed to separate 3 DB power dividers 80 and 82. Each of these two elements 80 and 82 functions to split its input signal to provide two output signals v~ich are essentially identical in 1~ -10-58~3 all respects, and mutually in phase as well. Thus, output ~ignals are provided at the power divider terminals 80a and 80b which are mutually in phase, and output signals are provided at the power divider terminals 82a and 82b which are also mutually in phase. However, there is a 90 phase differential between the signals from terminals 80a and 80b compared to the signals from terminals 82a and 82b due to the phase shift effected by the hybrid pouer divider 78.
The output signals from the hybrid signal splitter 76 are fed to the two dipole radiation devices 18 and 20, respectively, represented symbolically in Fig. 6 as elements 1 and 2. The output signals from the power divider 80 are similarly fed to the diametrically opposed monopole radiation devices 28 and 24, represented symbolically as elements 3 and 4, respectively.
Also, the output signals from the power divider 82 are fed to the remaining diametrically opposed monopole radiation devices 26 and 22, represented symbolically by elements 5 and 6, respectively. The dipole radiation devices within the inner cavity A thus receive their signals 90 out of phase. The resulting signal transmitted by the inner cavity portion of the antenna assembly is circularly polarized. It will be appreciated that the sense of rotation of the circularly polarized electro-magnetic radiation thus transmitted by the inner cavity portion of the antenna assembly is determined by the sense of the phase shift provided by the hybrid signal splitter 76. Therefore, by reversing the feed connections between the dipole radiation devices 18 and 20 relative to the signal splitter 76, the sense of rotation of the circularly polarized electromagnetic radiation transmitted by the inner cavity portion of the antenna assembly may be reversed.
458~3 As noted hereinbefore, the two monopole radiation devices 24 and 28 receive their two signals in phase, but 90 out of phase relative to the reception of the two signals by the remaining two monopole radiation devices 22 and 26. However, the feed to the monopole radiation device 22 is effected through the balun post which supports the radiation element 54, as opposed to the feeding of the other three monopole radiation devices occuring through the balun posts located within the .
inner cavity A. This difference in feed to the two diametrically opposed monopole radiation devices 22 and 26, which otherwise receive their input signals from the power divider 82 in phase, effects a 180 phase shift in the signals actually transmitted by the two radiation elements 54 and 58. Thus, by a combination of the phase shifting effected in the network circuitry as illustrated in Fig. 6 and the construction and positioning of the various monopole radiation devices 22 through 28, the sig~al provided by element 58 is 90 .
out of phase with the signals provided by elements 56 and 609 which are mutually in phase and 90~ out of phase with the signal provided by element 54. Also, there is a 180~ phase differential between the signals provided by elements 58 and 54. Thus, the total signal transmitted by the outer cavity portion of the antenna assembly is also circularly polarized. Furthermore, the sense of rotation of the circularly polarized signal thus transmitted by the outer portion of the antenna assembly may be reversed by simply reversing the output terminal connections of the hybrid signal splitter 78.
Excitation by the dipole radiation elements within the inner cavity A results in the transmission of a circularly ~)olarized signal. Similarly, excitation of the monopole ~1458~3 radiation elements in the outer cavity B of the antenna assembly results in the transmission of a circularly polarized signal as well. Due to the phase shift effected by the coupler 74, the dipole radiation elements illuminate the inner cavity 180 out of phase with the illumination of the outer cavity B effected by the monopole radiation elements. With the coaxial arrangement of the two antenna portions, the two individual signals then combine to a single signa~ of circularly polarized electro-magnetic radiation, whose rotational sense may be reversed by simply reversing the feed line connections of the two hybrid signal splitters 76 and 78 as noted hereinbefore.
The general radiation pattern characteristic of the inner cavity A illuminated by the crossed-dipole radiation elements is illustrated in Fig. 7 for a plane perpendicular to the aperture of the cavity A. Similarly, the general pattern of radiation characteristic of the outer cavity B as illuminated by the four monopole radiation devices operated in phase quadrature is illustrated in Fig. 8 for a plane normal to the aperture of the outer cavity B. The combined antenna assembly with the inner and outer cavities illuminated 180~ out of phase as discussed hereinbefore generates a radiation pattern as given by Fig. 9 for a plane normal to the apertures of both cavities A and B. It will be appreciated, by a compari~on of Figs. 7-9, that the coaxial array of antenna cavities illuminated by linear radiation elements excited according to the phas~
relationships described hereinbefore provides a radiation pattern of greater effective beam width than that of either of the antenna cavities operated alone. Further, the frequency bandwidth produced in the transmitted signals by the coaxial antenna ~array of the present invention is broader than that obtainable by either of the two antenna cavity portions operating alone.
1~58~3 The coaxial array antenna assembly of the present invention is also operable to receive circularly polarized electromagnetic radiation. In such case, the antenna assembly operates as a receiving antenna, with the incoming signals entering the cavities A and B and exciting both the dipole and monopole radiation elements. The received signals are then fed along the transmission lines of the six radiation devices through the feed connectors to the network circuitry previously described. The network circuit of the type illustrated in Fig. 6 operates to combine the individual signals induced in the various radiation devices. Then, the signal splitters 76-82 combine paired signals input thereto at the respective terminals previously identified as output terminals. Finally, the coupler 74 combines the two signals received by the inner and outer cavity antenna portions into a single signal presented at 72. The signal thus received by the antenna array and processed by the network circuit of Fig. 6 is provided for further processing by conventional receiver or other equipment.
For the purpose of flush mounting the antenna assembly in a spacecraft or other vehicle, the outer cavity wall 14 may be extended slightly above the height of the inner cavity wall 12, and provided with an externally extended flange 14a as shown in Figs. 1-3. The flange 14a may serve to facilitate the installation of the antenna array with an outer covering 84 as illustrated by dashed lines in Fig. 2. The greater height of the outer wall 14a above the base 16 compared to the height of the inner wall 12 raises the covering 84 above the top of the inner wall 12 and the balun posts of the radiation elements to accomodatl , the extension of the transmission lines above the balun posts.
1 ,, 1~ 11458~3 The covering 84 may include various environmental pro-tection elements~ such as a heat shield, but it must be at least partially transparent to electromagnetic radiation in the frequency range of communication by the antenna assembly.
The present invention may also be constructed in the form ¦ of coaxial circular antenna cavities as illustrated in Fig. 5 ¦ wherein certain elements which may be essentially identical in structure and/or function to those previously described are identified by numerals differing in value by 100 from the numerals used to identify the corresponding elements.
An inner antenna cavity C is limited by an inner circular wall 112 and the top surface of a cavity base 116. An outer antenna cavity D is defined by the inner surface of an outer circular wall 114, the outer surface of the inner wall 112, and the top surface of the cavity base 116. The outer wall 114 is fitted with a top outwardly extending flange 114a for purposes of mounting and/or covering the antenna array as discussed hereinbefore in relation to the square antenna array embodiment.
A crossed-dipole configuration, including dipole radiation devices 118 and 120 is centered within the inner cavity C. The dipole radiation device 118 includes radiation elements 144 and 146 extending in opposite senses along one diameter of the inner cavity circular cross section; the other dipole radiation device 120 includes radiation elements 136 and 138 extending in oppo~ite senses along a second diameter of the inner cavity C cross section which second diameter is perpendicular to the first diameter. , The radiation elements of the dipole devices 118 and 12~
are of the same type as those of the dipole devices 18 and 20 ~of the previously discussed embodiment. Thus, all such dipole radiation elements of both embodiments are in the general form of planar, radially extending flags lying in planes which include the longitudinal axis of the corresponding inner cavity.
As in the case of the square antenna array embodimen~, the circular antenna array includes four monopole radiation devices for excitation in the outer cavity D. Radiation devices 122 and 126 are positioned mutually diametrically opposed along the direction of orientation of the dipole device 120. Similarly, monopole radiation devices 124 and 128 are positioned mutually diametrially opposed along the direction of orientation of the dipole device 118.
Analagously to.the square embodiment, the balun posts-of the monopole radiation devices of the circular array straddle the inner circular wall 112. Further, three of the nopole devices 124, 126, and 128 are fed by transmission lines passing through balanced balun posts located within the inner wall 112, while the fourth monopole device is structured with its balanced balun post located in the outer cavity D. This particular monopole device 122 is.also positioned with its unbalanced balun post adjacent the radiation element 138 supported by an unbalanced balun post of the dipole radiation device 120.
The various transmission lines in each case also cross from the balanced posts to the unbalanced balun posts for each radiation device.
The monopole radiation devices 122-128 of the circular embodiment include radiation elements 154, 156, 158 and 160, respectively, in the general form of planar flags of a.pie-cut type shape, lying in a common plane perpendicular to the common longitudinal axis of the two cavities C and D, and positioned in the vicinity of the top of the various balun posts. Further, each of the flag elements 154-160 is positioned symmetrically about the diameters of the cavities C and D along which the radiation device of which the flag is a part is positioned.
11458~3 The performance of the antenna array with generally circular cavities is generally the same as that previously des-cribed in connection with the square antenna array assembly.
Thus, the individual cavities C and D, being illuminated separately, may be expected to provide radiation patterns as illustrated in Figs. 7 and 8, respectively, while the com~ined signal radiation pattern obtained by operating both cavities C
and D together resembles that illustrated in Fig. 9. Thus, the broadened radiation beam width as well as extended frequency bandwidth may be achieved by constructing the coaxial antenna array of the present invention in either a generaily square or circular pattern. Further, the network circuitry shown in Fig. 6, and the general construction of the network and feed connections illustrated in Fi8. 3 and described in connection therewith may be employed with the circular type antenna array of the present invention for both transmitting and receiving circularly polarized electromagnetic radiation. Then, for example, radiation devices 118, 120, 122, 124, 1~6 and 128 may be represented in Fig. 6 as elements 1, 2, 6, 4, 5, and 3, respectively.
In a particularly advantageous application, four individual coaxial-antenna assemblies according to the present invention may be spaced apart 90 about the roll plane of a spacecraft to utilize the 1n~ steradian coverage of the radiation pattern exhibited by one such antenna assembly, as illustrated in Fig. 8.
The foregoing disclosure and description of the invention is illustrative and explanatory thereof, and various changes in the details of the illustrated apparatus may be made within the ~cope of the appended claims without departing from the spirit of the invention.
Claims (13)
1. An antenna assembly for communicating electromagnetic radiation comprising:
a) first antenna cavity means;
b) second antenna cavity means, generally circumscribing said first antenna cavity means and substantially axially coextensive therewith, said first and second cavity means possessing a common central, longitudinal axis;
c) first and second dipole radiation means, positioned in crossed-dipole configuration within said first antenna cavity means; and d) first, second, third, and fourth monopole radiation means positioned symmetrically relative to said second antenna cavity means for excitation therein.
a) first antenna cavity means;
b) second antenna cavity means, generally circumscribing said first antenna cavity means and substantially axially coextensive therewith, said first and second cavity means possessing a common central, longitudinal axis;
c) first and second dipole radiation means, positioned in crossed-dipole configuration within said first antenna cavity means; and d) first, second, third, and fourth monopole radiation means positioned symmetrically relative to said second antenna cavity means for excitation therein.
2. An antenna assembly as defined in Claim 1 wherein:
a) said first antenna cavity means is defined by the interior surface of a first wall, generally circumscribing said first cavity means, and the surface of a base; and b) said second antenna cavity means is defined by the interior surface of a second wall, generally circumscribing said second cavity means, the exterior surface of said first wall, and the surface of a base.
a) said first antenna cavity means is defined by the interior surface of a first wall, generally circumscribing said first cavity means, and the surface of a base; and b) said second antenna cavity means is defined by the interior surface of a second wall, generally circumscribing said second cavity means, the exterior surface of said first wall, and the surface of a base.
3. An antenna assembly as defined in Claim 2 wherein:
a) each of said first and second dipole radiation means include balun means comprising, a balanced segment and an unbalanced segment, and radiation element means such that each balun segment supports a radiation element means, both radiation element means thus supported by a single balun means being oriented along a common direction and in opposite senses away from each other, the direction of orientation of the radiation element means of said first dipole radiation means being orthogonal to the direction of orientation of the radiation element means of said second dipole radiation means;
b) each of said first, second, third and fourth monopole radiation means includes balun means, each comprising a balanced segment and an unbalanced segment, and radiation element means such that only one balun segment of each said monopole radiation means supports a radiation element means;
c) the balun means of each said monopole radiation means is positioned such that, in each such case, the balun segment supporting a radiation element means is located within said second cavity means with said radiation element means supported thereby oriented along a direction generally away from said first antenna cavity means, and said other balun segment not supporting a radiation element means is located within said first antenna cavity means;
d) said first and third monopole radiation means are positioned mutually diametrically opposed across said first antenna cavity means along the direction of orientation of said radiation element means of said first dipole radiation means, said radiation element means of said first and second monopole radiation means extending in opposite senses generally along said direction; and e) said second and fourth monopole radiation means are positioned mutually diametrically opposed across said first antenna cavity means along said direction of orientation of said radiation element means of said second dipole radiation means, said radiation element means of said second and fourth monopole radiation means extending in opposite senses along said direction of orientation.
a) each of said first and second dipole radiation means include balun means comprising, a balanced segment and an unbalanced segment, and radiation element means such that each balun segment supports a radiation element means, both radiation element means thus supported by a single balun means being oriented along a common direction and in opposite senses away from each other, the direction of orientation of the radiation element means of said first dipole radiation means being orthogonal to the direction of orientation of the radiation element means of said second dipole radiation means;
b) each of said first, second, third and fourth monopole radiation means includes balun means, each comprising a balanced segment and an unbalanced segment, and radiation element means such that only one balun segment of each said monopole radiation means supports a radiation element means;
c) the balun means of each said monopole radiation means is positioned such that, in each such case, the balun segment supporting a radiation element means is located within said second cavity means with said radiation element means supported thereby oriented along a direction generally away from said first antenna cavity means, and said other balun segment not supporting a radiation element means is located within said first antenna cavity means;
d) said first and third monopole radiation means are positioned mutually diametrically opposed across said first antenna cavity means along the direction of orientation of said radiation element means of said first dipole radiation means, said radiation element means of said first and second monopole radiation means extending in opposite senses generally along said direction; and e) said second and fourth monopole radiation means are positioned mutually diametrically opposed across said first antenna cavity means along said direction of orientation of said radiation element means of said second dipole radiation means, said radiation element means of said second and fourth monopole radiation means extending in opposite senses along said direction of orientation.
4. An antenna assembly as defined in Claim 3 wherein three of said monopole radiation means are structured such that their balun means balanced segments are within said first antenna cavity means, and the other said monopole radiation element means is structured such that its balun means balanced segment is located within said second antenna cavity means.
5. An antenna assembly as defined in Claim 4 wherein said monopole radiation means with its balun means balanced segment located within said second antenna cavity means is positioned with its balun means unbalanced segment adjacent the radiation element means supported by a balun means unbalanced segment of one of said dipole radiation means.
6. An antenna assembly as defined in Claim 1 wherein:
a) the transverse cross section of said first antenna cavity means is generally square; and b) the transverse cross section of said second antenna cavity means is a plane figure generally square in exterior boundary and limited by a generally square interior boundary, said two boundaries being concentric and with mutually parallel corresponding sides.
a) the transverse cross section of said first antenna cavity means is generally square; and b) the transverse cross section of said second antenna cavity means is a plane figure generally square in exterior boundary and limited by a generally square interior boundary, said two boundaries being concentric and with mutually parallel corresponding sides.
7. An antenna as defined in Claim 6 wherein all said radiation element means are generally planar and oriented in planes containing the common longitudinal axis of said first and second cavity means.
8. An antenna assembly as defined in Claim 1 wherein:
a) the transverse cross section of said first antenna cavity means is generally circular; and b) the transverse cross section of said second antenna cavity means is a plane figure with exterior limit that is generally circular and interior limit that is generally circular, and concentric with said exterior limit.
a) the transverse cross section of said first antenna cavity means is generally circular; and b) the transverse cross section of said second antenna cavity means is a plane figure with exterior limit that is generally circular and interior limit that is generally circular, and concentric with said exterior limit.
9. An antenna assembly as defined in Claim 8 wherein:
a) said radiation element means of said dipole radiation means are generally planar and oriented in planes containing the common longitudinal axis of said first and second antenna cavity means; and b) said radiation element means of said monopole radiation means are generally planar and oriented in planes perpendicular to the common longitudinal axis of said first and second antenna cavity means.
a) said radiation element means of said dipole radiation means are generally planar and oriented in planes containing the common longitudinal axis of said first and second antenna cavity means; and b) said radiation element means of said monopole radiation means are generally planar and oriented in planes perpendicular to the common longitudinal axis of said first and second antenna cavity means.
10. An antenna assembly as defined in Claim 2 wherein said base whose surface partially defines said second antenna cavity means is an extension of said base whose surface partially defines said first antenna cavity means.
11. An antenna assembly for communicating electromagnetic radiation comprising a coaxial array of two open-ended cavities with double dipole radiation elements positioned for excitation within the inner cavity of the array, and four monopole radiation elements symmetrically positioned for excitation within the outer cavity of the array, said radiation elements coupled through feed means to a network in phased array to transmit or receive circularly polarized radiation.
12. An antenna assembly as defined in Claim 11 wherein the boundaries of the transverse cross sections of each of said inner and outer cavities are generally square, with the rotational orientation of all such squares relative to the common longitudinal axis of said inner and outer cavities being identical.
13. An antenna assembly as defined in Claim 11 wherein the boundaries of the transverse cross sections of said inner and outer cavities are generally circular and concentric.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US953,313 | 1978-10-17 | ||
| US05/953,313 US4218685A (en) | 1978-10-17 | 1978-10-17 | Coaxial phased array antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1145843A true CA1145843A (en) | 1983-05-03 |
Family
ID=25493814
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000337713A Expired CA1145843A (en) | 1978-10-17 | 1979-10-16 | Coaxial phased array antenna |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4218685A (en) |
| JP (1) | JPS5591208A (en) |
| CA (1) | CA1145843A (en) |
| DE (1) | DE2942061A1 (en) |
| FR (1) | FR2439483A1 (en) |
| GB (1) | GB2034125B (en) |
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| EP3573179B1 (en) * | 2018-05-24 | 2023-09-20 | Nokia Shanghai Bell Co., Ltd. | An antenna system |
| US11063357B2 (en) * | 2019-06-04 | 2021-07-13 | City University Of Hong Kong | Dual-band antenna for global positioning system |
| US11050151B2 (en) * | 2019-06-04 | 2021-06-29 | City University Of Hong Kong | Multi-band antenna |
| US11367948B2 (en) | 2019-09-09 | 2022-06-21 | Cubic Corporation | Multi-element antenna conformed to a conical surface |
| CN111181518A (en) * | 2019-12-28 | 2020-05-19 | 珠海市东恒电子有限公司 | Balanced unbalanced radio frequency conversion component manufacturing method |
| CN111180880B (en) * | 2020-02-10 | 2022-05-06 | 中国电波传播研究所（中国电子科技集团公司第二十二研究所） | Ultra-wideband circularly polarized antenna array |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3545001A (en) * | 1968-04-24 | 1970-12-01 | Bendix Corp | Antenna feed comprising dipole array with conductive ground plane |
| US3789416A (en) * | 1972-04-20 | 1974-01-29 | Itt | Shortened turnstile antenna |
| US3740754A (en) * | 1972-05-24 | 1973-06-19 | Gte Sylvania Inc | Broadband cup-dipole and cup-turnstile antennas |
| US3864687A (en) * | 1973-06-18 | 1975-02-04 | Cubic Corp | Coaxial horn antenna |
| US4042935A (en) * | 1974-08-01 | 1977-08-16 | Hughes Aircraft Company | Wideband multiplexing antenna feed employing cavity backed wing dipoles |
| GB1555307A (en) * | 1975-06-17 | 1979-11-07 | Marconi Co Ltd | Dipole radiotors |
| US4032921A (en) * | 1975-09-08 | 1977-06-28 | American Electronic Laboratories, Inc. | Broad-band spiral-slot antenna |
-
1978
- 1978-10-17 US US05/953,313 patent/US4218685A/en not_active Expired - Lifetime
-
1979
- 1979-10-16 JP JP13349679A patent/JPS5591208A/en active Pending
- 1979-10-16 CA CA000337713A patent/CA1145843A/en not_active Expired
- 1979-10-16 FR FR7925670A patent/FR2439483A1/en active Granted
- 1979-10-16 GB GB7935960A patent/GB2034125B/en not_active Expired
- 1979-10-17 DE DE19792942061 patent/DE2942061A1/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| DE2942061A1 (en) | 1980-05-08 |
| FR2439483A1 (en) | 1980-05-16 |
| JPS5591208A (en) | 1980-07-10 |
| GB2034125B (en) | 1982-12-01 |
| US4218685A (en) | 1980-08-19 |
| GB2034125A (en) | 1980-05-29 |
| FR2439483B1 (en) | 1983-07-22 |
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