US3833908A - Back-fire loop antenna - Google Patents
Back-fire loop antenna Download PDFInfo
- Publication number
- US3833908A US3833908A US00382388A US38238873A US3833908A US 3833908 A US3833908 A US 3833908A US 00382388 A US00382388 A US 00382388A US 38238873 A US38238873 A US 38238873A US 3833908 A US3833908 A US 3833908A
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- United States
- Prior art keywords
- loop
- reflector
- antenna
- backfire
- reflectors
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- Expired - Lifetime
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- 239000011810 insulating material Substances 0.000 claims description 3
- 230000005855 radiation Effects 0.000 description 16
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 239000004020 conductor Substances 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005684 electric field Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229940020445 flector Drugs 0.000 description 1
- 239000000463 material Substances 0.000 description 1
Images
Classifications
-
- 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
- H01Q19/18—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 having two or more spaced reflecting surfaces
- H01Q19/185—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 having two or more spaced reflecting surfaces wherein the surfaces are plane
Definitions
- the invention relates to a back-fire antenna which employs a loop.
- Back-fire antennas have been proposed by Ehrenspeck in US. Pat. Nos. 3,438,043 and 3,508,278.
- the Ehrenspeck antennas offer greatly increased gain of an end-fire antenna without adding to its length and the multiple reflection of electromagnetic waves between two plane reflectors of different size, with the energy being bound to the longitudinal antenna axis by a slow wave structure.
- Such antennas have been described as short back-fire antennas and they are directional antennas of a cavity type and a slow-wave end-fire type and are unsuitable for use as indoor antennas in the U.I-I.F.
- An object of the present invention is to provide a.
- an object of the invention is to provide an improved antenna suitable for use indoors.
- the invention consists in the provision of a back-fire loop antenna.
- This comprises only: a driving element in the form of a conductive loop of at least one turn; a first 2 plane conductive reflector parallel to the plane of .the loop spaced apart therefrom on the axis thereof; a second plane conductive reflector parallel to the plane of theory of multiple images which I have developed and which is described hereinafter.
- each-reflector may be mounted on a common axial shaft which is of insulating material or from which they are, insulated.
- each reflector is adjustably mounted on the shaft so that its position with respect to the loop may be altered.
- the spacing of the reflectors will depend upon the radiation resistance required for the particular application. However, it should normally be within one wavelength 0 the radiation to' be received or transmitted.
- each reflector is constituted by a conduc tive mesh.
- the circumference of the loop is approximately equal to one wavelength of the radiation to be received or transmitted.
- the loop may be of any closed shape but is conveniently circular, square 'or rectangular.
- Each reflector may be of any shape.
- the first reflector has a minimum linear dimension which is greater than one wavelength of the radiation to be re ceived or transmitted.
- the second reflector has a minimum linear dimension which is greater than one quarter of the wavelength of radiation to be received or transmitted.
- FIGS. 1, 2 and 3 show in side elevation three examples of a loop configuration which may be used in an antenna in accordance with the invention
- FIGS. 4 and 5 show respectively in side elevation and end elevation respectively an antenna in accordance with the invention
- FIG. 6 is a diagram of multiple images formed with an antenna according to the invention.
- FIGS. 7 and 8 are sketches for the explanation of the theory of multiple images.
- the loop is of copper tubing formed into a rectangle of sides d1 and d2.
- 2(d1 d2) is approximately equal to )t.
- FIGS. 4 and 5 there is shown a loop antenna in accordance with the invention in which a loop 1 as in FIG. -l'is mounted on aninsulating shaft together with a first reflector 3. Loop 1 is supported by an insulating strut la which is fastened to shaft 2. Re-
- flector 3 is formed'of a mesh of copper wire into circular form.
- the diameter D1 of the circle is arranged to be greater than )t.
- the reflector 3 is mounted to be adju'stable on shaft 2 so that the spacing between loop 1 and reflector 3 can be changed to the optimum value.
- Shaft 2 is extended through loop 1 and carries at its end remote from reflector 3 a-further, smaller, reflector.
- Reflector 4 is also constituted by a mesh of copper wire as shown in FIG. 5. The mesh is cut to circular form and has a diameter D2 which is greater than AA.
- Reflector 4 is mounted to be adjustable on shaft 2 so that its spacing from loop 1 may be set to the optimum. The optimum spacing for reflectors 3 and 4 will depend upon the particular radiation resistance required for the antenna.
- the dimensions of the antenna have a tolerance of plus or minus 20 percent 1 about the optimum.
- the antenna is arranged so that the loop 1 is in a vertical plane which is directed towards the transmitter or receiver, as the case may be, from which or to which the radiation is transmitted. Both vertically and horizontally polarised radiation may be received.
- the loop may be made of more than one turn, it may be of any desired shape and may be constituted by a conductor which is, say, of tubular aluminium or steel or of solid conductive material.
- the shape of the reflectors need not be circular, but they may be square or rectangular, forexample.
- the reflectors need not be made of mesh and may be solid, perhaps perforated.
- the material of the reflectors may be any suitable conductive material such as aluminium or steel and need not be copper.
- the two planereflectors M andR are both infinite in extent in order to formulate theproblem in terms of multiple images produced by multiple reflections between the conducting reflectors.
- the plane reflectors can then be replaced theoretically by two infinite series of images with appropriate direction of current-flow, one to the right of reflector R and one to the left of reflector M.
- the two series of images A,, A A and A A A I are primarily interested in the radiation field on the right-hand side of the large plane reflector, we shall therefore only consider the contributions from the loop antenna itself together with the image to the left of the large reflector.
- the back-fire antenna is then shown in FIG. 2 for analysis. This, in fact, reduces to an array of identical elements A A A A A alternatively 2D 2D
- the electric field in the far field due to the N" radiating element can be written as spaced where r is the distance from the origin to the far field point.
- a is the complex current in the n" element and is sometimes called the feeding coefficient of the element.
- E(0, (b) is the element pattern.
- a backfire loop antenna consisting of a driving element in the form of a conductive loop of at least one turn having a circumference approximating one wavelength at the frequency of operation; a first plane conductive reflector parallel to the plane of the loop spaced apart therefrom on the axis thereof; a second plane conductive reflector parallel to the plane of the loop on the axis thereof and on the'side thereof remote from the first conductive reflector, the second reflector .being smaller than the first reflector; and support means for supporting-the loop and the first and second conductive reflectors intheir said relative positions.
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- Aerials With Secondary Devices (AREA)
Abstract
A back-fire loop antenna having a loop of one or more turns situated between a pair of reflectors parallel with the plane of the loop, one reflector being larger than the other, there being means for supporting the loop and the reflectors in the required positions.
Description
mam States Patent [191 Lots [4 1 Sept. 3, 1974 [54] BACKQFIRE LOOP ANTENNA 3,491,361 1/1970 Campbell 343/741 [76] Inventor: Shin-Chang Loh, 12 Cooper Road,
J ardines Look-out, Hong Kong Primary ExamznerEl1 Lieberman Flledi J y 25, 1973 Attorney, Agent, or FirmWenderoth, Lind & Ponack [21] Appl. No.: 382,388
Related US. Application Data [63] Continuation-impart of Ser. No. 138,700, April 29, [57] ABSTRACT 1971, abandoned.
52 us. c1. 343/741, 343/837 A back-fire p antenna having a loop of one or r [51] Int. Cl. 3 .Q H01q 19/10 mms Situated between a P of reflectors Parallel with [58] Field of Search 343/833, 834, 837, 741 plane of the loop, one reflector being larger n the other, there being means for supporting the loop 5 R f r n es Cited and the reflectors in the required positions.
UNITED STATES PATENTS I I 7 3,438,043 4/1969 Ehrensp ec'k .1 343/837 7 Claims, 10 Drawing Figin'es PATENTEDSEP 319M 3.833.908
SHEEI 10F 5 FIG]. I 6 2 PAIENTED 3' v suwsur s BACK-FIRE LOOP ANTENNA This application is a contin'uation-in-part of application Ser. No. 138,700 filed Apr. 29, 1971 and now abandoned.
The invention relates to a back-fire antenna which employs a loop.
Back-fire antennas have been proposed by Ehrenspeck in US. Pat. Nos. 3,438,043 and 3,508,278. The Ehrenspeck antennas offer greatly increased gain of an end-fire antenna without adding to its length and the multiple reflection of electromagnetic waves between two plane reflectors of different size, with the energy being bound to the longitudinal antenna axis by a slow wave structure. Such antennas have been described as short back-fire antennas and they are directional antennas of a cavity type and a slow-wave end-fire type and are unsuitable for use as indoor antennas in the U.I-I.F.
range. I
An object of the present invention is to provide a.
back-fire antenna operating on a different principle from the short back-fire antenna and suitable for use in the U.H.F. region for television purposes. In particular an object of the invention is to provide an improved antenna suitable for use indoors. g I
The invention consists in the provision of a back-fire loop antenna. This comprises only: a driving element in the form of a conductive loop of at least one turn; a first 2 plane conductive reflector parallel to the plane of .the loop spaced apart therefrom on the axis thereof; a second plane conductive reflector parallel to the plane of theory of multiple images which I have developed and which is described hereinafter.
' The loop and each-reflector may be mounted on a common axial shaft which is of insulating material or from which they are, insulated. Preferably each reflector is adjustably mounted on the shaft so that its position with respect to the loop may be altered. The spacing of the reflectors will depend upon the radiation resistance required for the particular application. However, it should normally be within one wavelength 0 the radiation to' be received or transmitted.
Preferably each reflector is constituted by a conduc tive mesh.
Preferably the circumference of the loop is approximately equal to one wavelength of the radiation to be received or transmitted. The loop may be of any closed shape but is conveniently circular, square 'or rectangular.
Each reflector may be of any shape. Preferably the first reflector has a minimum linear dimension which is greater than one wavelength of the radiation to be re ceived or transmitted. Preferably the second reflector has a minimum linear dimension which is greater than one quarter of the wavelength of radiation to be received or transmitted.
The invention will further be described with reference to the accompanying drawings, of which:
FIGS. 1, 2 and 3 show in side elevation three examples of a loop configuration which may be used in an antenna in accordance with the invention;
FIGS. 4 and 5 show respectively in side elevation and end elevation respectively an antenna in accordance with the invention;
FIG. 6 is a diagram of multiple images formed with an antenna according to the invention;
FIGS. 7 and 8 are sketches for the explanation of the theory of multiple images; and
FIGS. 9 and l0are diagrams of radiation patterns for back-fire loop antennas.
Referring to FIG. 3 the loop is of copper tubing formed into a rectangle of sides d1 and d2. In this case 2(d1 d2) is approximately equal to )t.
Referring now to FIGS. 4 and 5 there is shown a loop antenna in accordance with the invention in which a loop 1 as in FIG. -l'is mounted on aninsulating shaft together with a first reflector 3. Loop 1 is supported by an insulating strut la which is fastened to shaft 2. Re-
For acceptable performance the dimensions of the antenna have a tolerance of plus or minus 20 percent 1 about the optimum. In use, the antenna is arranged so that the loop 1 is in a vertical plane which is directed towards the transmitter or receiver, as the case may be, from which or to which the radiation is transmitted. Both vertically and horizontally polarised radiation may be received.
The invention is not restricted to the details of the foregoing example described with reference to the accompanying drawings. For example, the loop may be made of more than one turn, it may be of any desired shape and may be constituted by a conductor which is, say, of tubular aluminium or steel or of solid conductive material. The shape of the reflectors need not be circular, but they may be square or rectangular, forexample. The reflectors need not be made of mesh and may be solid, perhaps perforated. The material of the reflectors may be any suitable conductive material such as aluminium or steel and need not be copper.
The multiple image theory will now be explained with reference to FIGS. 6 to 10 of the drawings.
As a first approximation, we assume that the two planereflectors M andR are both infinite in extent in order to formulate theproblem in terms of multiple images produced by multiple reflections between the conducting reflectors. The plane reflectors can then be replaced theoretically by two infinite series of images with appropriate direction of current-flow, one to the right of reflector R and one to the left of reflector M. The two series of images A,, A A and A A A I are primarily interested in the radiation field on the right-hand side of the large plane reflector, we shall therefore only consider the contributions from the loop antenna itself together with the image to the left of the large reflector. The back-fire antenna is then shown in FIG. 2 for analysis. This, in fact, reduces to an array of identical elements A A A A alternatively 2D 2D The electric field in the far field due to the N" radiating element can be written as spaced where r is the distance from the origin to the far field point.
r is the unit vector in the direction of T 7,, is the position of the N"? image with respect to the circular loop antenna situated at the origin. Combining (l) and (2) gives the far field due to the n" radiating element as Thus, by the principle of superposition, the far field of the array of (N 1) elements is simply where If the shape of the radiation pattern is identical for each element of the array,
where a is the complex current in the n" element and is sometimes called the feeding coefficient of the element.
E(0, (b) is the element pattern.
Putting (6) into (4), the far field of the array be comes which can be rewritten without the multiplying factor is defined as the array polynomial Radiation Field of a Circular Loop Backfire Antenna The electric field intensity of a circular loop at a large distance, assuming a sinusoidal current distribution (I l sin pip) is given by E. m ae- /rxpl up mo p =J u o n-1( pirmn w where r, 6, 4)) is the position of the far field point p a is the radius of the circular loop I is the maximum current amplitude J,,(a) is the Bessel function of order p and a ka sinB.
If we choose a co-ordinate system such that the loop lies in the xy plane with the reflectors parallel to it, the position of the n'" image from the loop will be given by:
2 r+1)z)+21 1 odd N Po= N Z even N Substituting into (5) yields g 2k(D +D,) cos 6-2kD cos 6 odd N in N 2k(D +D,) cos 0 even N Q HEI odd N N even N (12) With the complex current given by the reflection coefficients Simplic'ation of 13) gives -lp (iii-f 1a exp 'n j(E-l-2a')} 1a exp j(+2a) In order to consider the field due to a series of consecutive images we always have Radiation Field of a Short Backfire Loop Antenna The short backfire loop antenna is essentially a full wavelength circular loop placed midway between two reflectors separated at a distance of )t/Z. In this case Hence the far field radiation patternis J (sin 9) Jail-il um C05 6 C05 ()5 {1-a exp (-j1r cos 0+a')} E l-a exp (-j1r cos 6+a) were calculated using various values of N, and a. A slight departure from D )t/4, however, produced a shift of the maximum in the radiation pattern. This is understandable as the reflectors are plane conductors and the image antenna and the object antenna should have a phase difference of Since a is always less than 1, the effect of varying a amounts to a reduction of the number of images used. Hence a suitable choice of N and a will provide the radiation pattern of any short backfire antenna. The results are illustrated in FIG. 9 and FIG. 10 together with the experiment patterns.
I claim:
1. A backfire loop antenna consisting of a driving element in the form of a conductive loop of at least one turn having a circumference approximating one wavelength at the frequency of operation; a first plane conductive reflector parallel to the plane of the loop spaced apart therefrom on the axis thereof; a second plane conductive reflector parallel to the plane of the loop on the axis thereof and on the'side thereof remote from the first conductive reflector, the second reflector .being smaller than the first reflector; and support means for supporting-the loop and the first and second conductive reflectors intheir said relative positions.
2. A backfire loop antenna as claimed in claim 1 wherein the support means is a common axial shaft on which the loop and reflectors are mounted and which is of insulating material or from which the loop and reflectors are insulated.
3. A backfire loop antenna as claimed in claim 2 wherein one or each reflector is adjustably mounted on the shaft.
4. A backfire loop antenna as claimed in claim 1 wherein the reflectors are spaced apart a distance not greater than the circumference of the loop.
5. A backfire loop antenna as claimed in claim 1 wherein one or each refelctor is constituted by a conductive mesh. I p
6. A backfire loopantenna as claimed in claim 1 wherein the first reflector has'a minimum linear dimension which is'greater than the circumference of the loop.
7. A backfire loop antenna as claimed in claim 1 wherein the second reflector has a minimum linear dimension which is greater than one quarter of the circumference of the loop.
Claims (7)
1. A backfire loop antenna consisting of a driving element in the form of a conductive loop of at least one turn having a circumference approximating one wavelength at the frequency of operation; a first plane conductive reflector parallel to the plane of the loop spaced apart therefrom on the axis thereof; a second plane conductive reflector parallel to the plane of the loop on the axis thereof and on the side thereof remote from the first conductive reflector, the second reflector being smaller than the first reflector; and support means for supporting the loop and the first and second conductive reflectors in their said relative positions.
2. A backfire loop antenna as claimed in claim 1 wherein the support means is a common axial shaft on which the loop and reflectors are mounted and which is of insulating material or from which the loop and reflectors are insulated.
3. A backfire loop antenna as claimed in claim 2 wherein one or each reflector is adjustably mounted on the shaft.
4. A backfire loop antenna as claimed in claim 1 wherein the reflectors are spaced apart a distance not greater than the circumference of the loop.
5. A backfire loop antenna as claimed in claim 1 wherein one or each refelctor is constituted by a conductive mesh.
6. A backfire loop antenna as claimed in claim 1 wherein the first reflector has a minimum linear dimension which is greater than the circumference of the loop.
7. A backfire loop antenna as claimed in claim 1 wherein the second reflector has a minimum linear dimension which is greater than one quarter of the circumference of the loop.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00382388A US3833908A (en) | 1973-07-25 | 1973-07-25 | Back-fire loop antenna |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US00382388A US3833908A (en) | 1973-07-25 | 1973-07-25 | Back-fire loop antenna |
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US3833908A true US3833908A (en) | 1974-09-03 |
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US00382388A Expired - Lifetime US3833908A (en) | 1973-07-25 | 1973-07-25 | Back-fire loop antenna |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4128360A1 (en) * | 1991-08-27 | 1993-03-04 | Aeg Sensorsysteme Gmbh | Identification appts. for moving vehicles - uses aerials on information carrier and checking device with reflectors for data exchange |
US5838283A (en) * | 1995-01-18 | 1998-11-17 | Nippon Antenna Kabushiki Kaishya | Loop antenna for radiating circularly polarized waves |
US7091843B1 (en) | 2002-11-05 | 2006-08-15 | Rajiv Singh Lal | Functional and ornamental vehicle accessories |
USD535984S1 (en) * | 2003-01-06 | 2007-01-30 | Rajiv S. Lal | Ring-shaped vehicle accessory |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3438043A (en) * | 1968-07-02 | 1969-04-08 | Hermann W Ehrenspeck | Short backfire antenna |
US3491361A (en) * | 1968-03-07 | 1970-01-20 | Ralph W Campbell | Endfire antenna array having loop directors |
-
1973
- 1973-07-25 US US00382388A patent/US3833908A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3491361A (en) * | 1968-03-07 | 1970-01-20 | Ralph W Campbell | Endfire antenna array having loop directors |
US3438043A (en) * | 1968-07-02 | 1969-04-08 | Hermann W Ehrenspeck | Short backfire antenna |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4128360A1 (en) * | 1991-08-27 | 1993-03-04 | Aeg Sensorsysteme Gmbh | Identification appts. for moving vehicles - uses aerials on information carrier and checking device with reflectors for data exchange |
US5838283A (en) * | 1995-01-18 | 1998-11-17 | Nippon Antenna Kabushiki Kaishya | Loop antenna for radiating circularly polarized waves |
US7091843B1 (en) | 2002-11-05 | 2006-08-15 | Rajiv Singh Lal | Functional and ornamental vehicle accessories |
US20070013505A1 (en) * | 2002-11-05 | 2007-01-18 | Mr. Rajiv Lai | Functional and ornamental vehicle accessories |
US8330595B2 (en) | 2002-11-05 | 2012-12-11 | Rajiv Lal | Functional and ornamental vehicle accessories |
USD535984S1 (en) * | 2003-01-06 | 2007-01-30 | Rajiv S. Lal | Ring-shaped vehicle accessory |
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