US3056130A - Cavity loaded slot antenna - Google Patents

Cavity loaded slot antenna Download PDF

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Publication number
US3056130A
US3056130A US83085159A US3056130A US 3056130 A US3056130 A US 3056130A US 83085159 A US83085159 A US 83085159A US 3056130 A US3056130 A US 3056130A
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Prior art keywords
cavity
slot
aerial
provided
resonant
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Expired - Lifetime
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Charman Frederick John Henry
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EMI Ltd
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EMI Ltd
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    • HELECTRICITY
    • H01BASIC ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q13/00Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/10Resonant slot antennas
    • H01Q13/18Resonant slot antennas the slot being backed by, or formed in boundary wall of, a resonant cavity ; Open cavity antennas

Description

Sept. 25, 1962 F. J. H. CHARMAN CAVITY LOADED SLOT ANTENNA Filed July 31, 1959 FIG. 4. FIG. fimverztor United States Patent Dfiice 3,056,130 Patented Sept. 25, 1962 3,056,130 CAVITY LOADED SLOT ANTENNA Frederick John Henry Charman, l ightwater, Surrey, England, assignor to Electric & Musical Industries Lunited, Hayes, England, a company of Great Britain Filed July 31, 1959,GSer.tl;o. t80,g51 6 1958 laims riorit a lication rea r1 am ug. C p b ciiims. (Cl. 343-467) This invention relates to aerials.

The problem is sometimes encountered of providlng an aerial on a vehicle or mast structure where the space available for the aerial is small and the aerial must not extend outside the surfaces of the vehicle. The natural approach to the solution of such a problem is to employ a slot aerial but even for such an aerial there may be insufficient internal space to provide the quarter-wave resonant cavity necessary to obstruct radiation into the interior of the vehicle.

The object of the present invention is to reduce the difficulty indicated and at the same time to provide an aerial with 'broad band characteristics.

According to the present invention there is provided a slot aerial comprising a slot formed in the wall of a resonant cavity, the cavity having a dimension smaller than required for resonance at a desired frequency and capacitive loading means being provided in the cavity to tune the cavity to resonance at said desired frequency. The capacitive loading is preferably provided by means of a longitudinal baffle and it reduces the effective phase velocity for energy in the cavity, so that tuning of the cavity to resonance in the desired frequency band can be achieved by choosing the capacitive loading required to give the appropriate phase velocity.

I11 order that the invention may be clearly understood and readily carried into effect, the invention will be described with reference to the accompanying drawings, in which:

FIGURE 1 is a cross sectional view of a slot aerial according to the invention,

FIGURE 2 is a fragmentary plan view of the aerial,

FIGURE 3 is the equivalent circuit of the aerial shown in FIGURES l and 2, and

FIGURES 4 and 5 illustrate diagrammatically slot aerials according to the invention mounted on a mast structure.

The aerial shown in FIGURES 1 and 2 of the drawing is formed by means of a cavity in a part of the outer casing 1 of a vehicle. The cavity in this example is about four inches wide, one inch deep and eighteen inches long. The cavity behaves as a waveguide and is formed as a folded cavity by virtue of a baffle 2, so that the cavity is tuned to resonance in a desired frequency band. The baflie 2 comprises a plate 2A extending longitudinally from one end of the cavity to the other and extending laterally from one side approximately half Way to the other side. It comprises furthermore a web 2B extending from the plate 2A nearly to the bottom of the cavity where the web 2B is provided with a flange 2C spaced from the bottom of the cavity by di-electrical material 2D. In some cases the di-electric material 2D may be dispensed with. By virtue of the baffle 2, the cavity has the form of a cavity folded about a longitudinal axis and the baffle provides capacitive loading sufl'icient to bring the cavity to resonance at a desired frequency in the working band, the length of the cavity (the vertical dimension of FIGURE 2) being only a fraction of that which would be required for quarter wave resonance at that frequency with the phase velocity which would prevail in the absence of the capacitive loading. The cavity is represented in the drawing as conforming to a rectangular prism, but it may in fact be curved to conform to the surface of the vehicle on which it is provided. For example it may be curved about an axis normal to the plane of the web 2A, the part 1 being for example of ring formation. The slot which forms the radiating element of the aerial is bounded by the edge 1A of the cavity and by the edge 1B of the baffle and it extends the full length of the cavity to give the maximum conductance load on the cavity. The shunt resistance of a half-wave slot radiating into half-space is 1,000 ohms. The slot shown, nearly 3M4 long, provides a load of about 500 ohms and some capacitive load which is taken into account in resonating the cavity. However the working characteristic impedance of the cavity is lower than this value, and the bandwidth of the aerial would be too restricted for many applications. In order to increase the bandwidth, a linear conductor or rod 3 is disposed within the slot, its position being adjusted so that it taps into the electric field across the slot and provides a transformer with turns ratio V /V as indicated. The linear conductor 3 behaves as a transmission line in series with the feed which is provided by a coaxial line 7, and the length of the conductor 3 is adjusted to provide inductive reactance. Series capacitance is added at the feed point of the arrangement, for example by conductive films 5 and 6 the former of which is deposited on the under surface of a di-electric window 4 which closes the slot and is connected to the inner conductor of the aerial feed line 7, and the latter of which is embedded in the di-electric window 4 and connected to the conductor 3. The equivalent circuit of the aerial is shown in FIGURE 3 and as can be seen it represents a half section constant-k band pass filter comprising a series resonant circuit 8, a parallel resonant circuit 9 and an admittance 10. The capacity 11 of the series resonant circuit is introduced mainly by the conductive films 5 and 6 and the inductance 12 is provided mainly by the conductor 3. The parallel resonant circuit 9 is provided mainly by the cavity and the series and parallel resonant circuits are in effect coupled by tapping the senes resonant circuit to an intermediate point in the capacitive arm of the parallel resonant circuit, the tapping pomt being determined by the position of the conductor 3 in the slot. The admittance 10 is provided by the slot, the reactive component of this admittance being, .as aforesaid, taken into account in tuning the cavity.

A principal advantage of the present invention is that it reduces the volume required for the cavity and it allows the use of a slot which is considerably longer than half-wave length, thus allowing for heavy radiation loading and increased bandwidth.

In some cases a small variable capacitance, not shown, may be provided between the flange 2C and the bottom of the cavity for the purpose of practical adjustment of the resonant frequency. Moreover more than one aerial such as shown in the drawing may be provided on a single vehicle. For example two such aerials may be provided opposite each other and formed around the circumference of a cylinder, being for example built into a ring which is part of the structure of the vehicle.

The invention is not confined to the provision of aerials on vehicles but may be applied to aerials used for U.H.F. and V.H.F. broadcasting. In such applications, the invention is particularly advantageous where it is desired to provide aerials on masts of relatively small diameter, the slots being vertical when horizontal polarization is required and being circumferential when vertical polarization is required. FIGURES 4 and 5 illustrate the provision of two aerials 13 and 14 in accordance with the invention on opposite sides of the mast, the mast being represented in horizontal section and the slots being vertical for horizontal polarization. The aerials are each constructed substantially as illustrated in FIGURES l and 2. In the example shown in FIGURE 4 the two aerials 13 and 14 are arranged to radiate in phase whereas in the example shown in FIGURE 5 the two aerials 13 and 14 are arranged to radiate in antiphase, the antiphase radiation being achieved simply by turning one aerial upsidedown with reference to the other. In both cases feeder lines 15 and 16 of equal lengths are provided from a common feed point 17 to the two aerials.

What I claim is:

1. A slot aerial comprising a resonant cavity having two substantially parallel oblong walls, a slot formed in one of said oblong walls, said slot extending longitudinally along the oblong wall and being disposed nearer to one of the long edges of said wall than the other, the cavity being provided with a bafiie connected to and projecting from said first mentioned oblong wall towards the parallel wall and being formed with a flange parallel to but insulated from said parallel wall, said bafile extending longitudinally from one end of the cavity to the other and being such as to have the elfect of folding the cavity about a longitudinal axis, and said flange providing capacitive loading means to tune the cavity to resonance at a desired frequency, the cavity having a dimension which in the absence of said loading is smaller than required for resonance at said desired frequency.

2. A slot aerial according to claim 1 comprising means for supplying energy to said slot, said means including a capacitive reactance connecting in series with a conductor disposed in the slot, said conductor being substantially parallel to the longitudinal edge of the slot and being dimensioned and positioned to provide inductance which forms with said capacitive reactance a series resonant circuit coupled to the cavity to increase the bandwidth of the aerial.

3. An aerial array comprising a plurality of slot aerials each according to claim 1, one aerial being turned upside-down with respect to another so as to radiate in anti-phase with respect to said other aerial.

4. A slot aerial according to claim 1, said loading means comprising a longitudinal bafile extending parallel to the slot and between the slot and said other edge, and said baflie being conductively attached to said oblong wall, and means being provided for injecting energy to be radiated into the cavity at the slot.

5 A slot aerial comprising a slot formed in the wall of a resonant cavity, the cavity having a dimension smaller than required for resonance at a desired frequency and being provided with capacitive loading means to tune the cavity to resonance at said desired frequency and comprising means having capacitive reactance connected to a conductor disposed in the slot for applying energy to the slot, said conductor being dimensioned and positioned to provide inductance which forms with said capacitive reactance a series resonant circuit coupled to the cavity to increase the band width of the aerial.

6. A slot aerial according to claim 5, wherein said capacitive loading means comprises a longitudinal baffle.

7. A slot aerial according to claim 5 wherein the slot extends substantially the Whole length of the cavity.

8. A slot aerial according to claim 6, wherein said baffle extends longitudinally from one end of the cavity to the other and is such as to have the effect of folding the cavity about a longitudinal axis.

9. An aerial array comprising a plurality of slot aerials each according to claim 8, one aerial being turned upsidedown with respect to another so as to radiate in antiphase with respect to said other aerial.

References Cited in the file of this patent UNITED STATES PATENTS 2,414,266 Lindenblad Jan. 14, 1947 2,642,529 Frankel June 16, 1953 2,684,444 Fales July 20, 1954 2,942,263 Baldwin June 21, 1960

US3056130A 1958-08-06 1959-07-31 Cavity loaded slot antenna Expired - Lifetime US3056130A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2513758A GB929871A (en) 1958-08-06 1958-08-06 Improvements relating to aerials

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US3056130A true US3056130A (en) 1962-09-25

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DE (1) DE1095330B (en)
GB (1) GB929871A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3312976A (en) * 1965-07-19 1967-04-04 Trak Microwave Corp Dual frequency cavity backed slot antenna
US4005429A (en) * 1975-10-08 1977-01-25 The United States Of America As Represented By The Secretary Of The Army Camouflaged VHF antenna
US4023179A (en) * 1975-10-08 1977-05-10 The United States Of America As Represented By The Secretary Of The Army Camouflage VHF antenna
US4451830A (en) * 1980-12-17 1984-05-29 The Commonwealth Of Australia VHF Omni-range navigation system antenna
US5126751A (en) * 1989-06-09 1992-06-30 Raytheon Company Flush mount antenna
US5365244A (en) * 1993-01-29 1994-11-15 Westinghouse Electric Corporation Wideband notch radiator
US5596337A (en) * 1994-02-28 1997-01-21 Hazeltine Corporation Slot array antennas
EP1280233A1 (en) * 2000-04-13 2003-01-29 Mitsubishi Denki Kabushiki Kaisha Antenna element and portable communication terminal

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1364941A (en) * 1972-01-05 1974-08-29 Secr Defence Aerials
US4047179A (en) * 1976-05-03 1977-09-06 Raytheon Company IFF antenna arrangement

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2414266A (en) * 1942-06-27 1947-01-14 Rca Corp Antenna
US2642529A (en) * 1949-07-29 1953-06-16 Int Standard Electric Corp Broadband loop antenna
US2684444A (en) * 1950-08-15 1954-07-20 Bendix Aviat Corp Pocket antenna
US2942263A (en) * 1957-02-25 1960-06-21 Gen Dynamics Corp Antennas

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2414266A (en) * 1942-06-27 1947-01-14 Rca Corp Antenna
US2642529A (en) * 1949-07-29 1953-06-16 Int Standard Electric Corp Broadband loop antenna
US2684444A (en) * 1950-08-15 1954-07-20 Bendix Aviat Corp Pocket antenna
US2942263A (en) * 1957-02-25 1960-06-21 Gen Dynamics Corp Antennas

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3312976A (en) * 1965-07-19 1967-04-04 Trak Microwave Corp Dual frequency cavity backed slot antenna
US4005429A (en) * 1975-10-08 1977-01-25 The United States Of America As Represented By The Secretary Of The Army Camouflaged VHF antenna
US4023179A (en) * 1975-10-08 1977-05-10 The United States Of America As Represented By The Secretary Of The Army Camouflage VHF antenna
US4451830A (en) * 1980-12-17 1984-05-29 The Commonwealth Of Australia VHF Omni-range navigation system antenna
US5126751A (en) * 1989-06-09 1992-06-30 Raytheon Company Flush mount antenna
US5365244A (en) * 1993-01-29 1994-11-15 Westinghouse Electric Corporation Wideband notch radiator
US5596337A (en) * 1994-02-28 1997-01-21 Hazeltine Corporation Slot array antennas
EP1280233A1 (en) * 2000-04-13 2003-01-29 Mitsubishi Denki Kabushiki Kaisha Antenna element and portable communication terminal
EP1280233A4 (en) * 2000-04-13 2004-12-22 Mitsubishi Electric Corp Antenna element and portable communication terminal

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Publication number Publication date Type
GB929871A (en) 1963-06-26 application
DE1095330B (en) 1960-12-22 application

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