US3643262A - Microstrip aerials - Google Patents
Microstrip aerials Download PDFInfo
- Publication number
- US3643262A US3643262A US855234A US3643262DA US3643262A US 3643262 A US3643262 A US 3643262A US 855234 A US855234 A US 855234A US 3643262D A US3643262D A US 3643262DA US 3643262 A US3643262 A US 3643262A
- Authority
- US
- United States
- Prior art keywords
- strips
- edges
- discontinuities
- line
- lines
- 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 - Lifetime
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/20—Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/26—Surface waveguide constituted by a single conductor, e.g. strip conductor
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/20—Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/206—Microstrip transmission line antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/20—Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/28—Non-resonant leaky-waveguide or transmission-line antennas; Equivalent structures causing radiation along the transmission path of a guided wave comprising elements constituting electric discontinuities and spaced in direction of wave propagation, e.g. dielectric elements or conductive elements forming artificial dielectric
Definitions
- the present invention relate to directional aerials and more particularly to directional aerials for-use in moving bodies whose aerodynamical characteristics should be affected as little as possible by the presence of theaerial.
- An aerial according to the invention comprises, at least, one microstrip having a plurality of equally spaced radiating discontinuities obtained by laterally sifting the edges of the strip, thus forming laterally set off rectangular strip portions.
- FIG. I is a diagrammatic top view of the microstrip aerial according to the invention.
- FIG. 2 is a detail of the aerial of FIG. ll;
- FIGS. 3 to it are explanatory curves
- FIG. 9 is an embodiment of a directive aerial according to the invention.
- FIG. 10 illustrates a cross section of the aerial of FIG. 9
- FIG. I1 is an explanatory perspective view
- FIG. 12 is a radiating pattern of an aerial according to the invention. i
- a microstrip line 11 is illustrated as viewed from above, the ground plate being disposed in the plane of the figure.
- this line comprises a plurality of discontinuities 2, spaced from each other by x,, A, designating the wavelength in the line of the energy propagating along the same.
- each discontinuity 2 is formed by laterally shifting the edges of a portion of the strip in a direction perpendicular to the longitudinal axis thereof.
- edge 3 is shifted by a distance c and edge 4 by a distance d.
- each discontinuity is, in the embodiment shown, substantially equal to M4.
- the radiation factor i.e., the ratio of the radiated energy to the incident energy, varies as a function ofd.
- each length d corresponds a length c for which the discontinuity is matched to the line. All discontinuities being matched to the line, the energy fed to the line propagates as a progressive wave.
- the projecting strip portions radiate energy and the reentrant portions insure the matching.
- FIGS. 3, 4 and 5 show curves indicating how different parameters vary as a function of d, namely: the standing wave ratio with F (FIG. 3); the radiation factor p (FIG. A), distance c with the standing wave ratioequal to 1.
- FIG. 6 shows the phase shift 1 due to energy radiation as a function ofd.
- FIG. 9 illustrates a guide, which feeds a plurality of lines 1111, III, 13 and MI, each line being fed at its center. The distance between two adjacent lines is M2, it being the operating wavelength.
- FIG. l0 shows in section how each line is coupled to guide 110.
- a metal plate 5 which is common to microstrips l0 and M, is supported on a metal bloclt II which rests on guide 110.
- a passage 15 is formed in bloclt 9, symmetrically with respect to guide 110, for coupling strips 1111 to M to the guide.
- a dielectric layer 117 rests on plate 5, the same dielectric lining passages 15.
- a probe lb couples the conductive strips 1 to guide It), probe lb and lining 115 thus forming a coaxial cable.
- the discontinuities 20 are all fed in phase; they are separated by an electrical distance I substantially equal to it, and given more precisely by the formula:
- An aerial according to the invention is directional.
- the radiation direction is along a straight line defined by the intersection of:
- a plane including axis by and making an angle 0 with the axis 0x, with cos 0 c./Vg., c being the velocity of light and Vg. the phase velocity of the wave in guide 10.
- FIG. 112 shows the directive pattern obtained with an aerial according to the invention, operating at 10,000 mc., in the above defined planes.
- the width M of the beam at a level 3 db. below the maximum is given by the fonnula;
- the distance between the discontinuities could be different from A.
- the two planes respectively comprising the radiation directions would be inclined over the horizontal.
- the distance between the points where the strips are coupled to the guide could be separated by distance different from M 2.
- a microwave directional aerial comprising at least one microstrip line having a ground plate, an insulating plate and a conductive strip superimposed upon each other, said strip having edges; means for feeding to said line ultrahigh frequency energy; both edges being laterally set off in the same direction at uniformly spaced points, thus forming radiating discontinuities.
- a microwave directional aerial comprising a plurality of parallel, equally spaced lines having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; means for feeding to said lines ultrahigh frequency energy; both edges of each line being laterally set off in the same direction at uniformly spaced points, thus forming radiating discontinuities.
- a microwave directional aerial comprising a plurality of parallel equally spaced lines, having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; means for feeding to said lines ultrahigh frequency energy; both said edges being laterally set off in the same direction, thus forming along a predetermined length of said strips radiating discontinuities, said discontinuities being spaced apart by the length in said microstrip of the operating wave and said predetermined length being the same for all the strips.
- a microwave directional aerial comprising a plurality of parallel equally spaced strip lines, having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; both said edges being laterally set off in the same direction thus forming along a predetermined length of said strips radiating discontinuities, said discontinuities being spaced apart by the length in said microstrip of the operating wave and said predetermined length being the same for all the strips; a wave guide extending normally to said strip lines, said guide having a pair of large walls, one of said walls supporting said ground plate; and probes respectively coupling said strips to said guide.
Abstract
A microstrip aerial having a plurality of equally spaced radiating discontinuities obtained by laterally shifting the edges of the strip.
Description
1111mm @inim Wmem mnmmmihin 11 Feb, 11%, W72
[54] MlllQfiUfiTBMEP AEMHAiLfi [56] Reiierences (filled [72] inventor: Winger Drrmnnch'nn, Paris, France UNITED STATES PATENTS [7 Assigns-er rw German-Me fi Telermpme S 2,605,413 7/1952 Alvarez ..343/771 )1 Fill, France [22] Filed: Wm M, 1959 FOREIGN PATENTS OR APPLTCATIONS {21] APPLNOJ $553M 1,123,769 6/1952 France "343/ 776 Primary ExaminerRodney D. Bennett, Jr.
[30] Waning Alpphwmm mom? mam Assistant Examiner Richard E. Berger Dec. 5, 1958 France ..780929 flrwmekwatmlloditwSchwartz 52] 10.5131 .MEi/W, 343/708, 343/908 [571 Answer issi 1111131 111 Search ..343/772 776705 20% 428 AmicmsmP aerialhavingaplumlity fequauy5paced ing discontinuities obtained by latenally shifting the edges of the strip.
4 Clinims, 112 Drawing Tigures PATENTEUFEB 15 I872 SHEET 0F 4 0 INVENTOR ROGER DUMANCH/N Micnosrnrn xnnrxrs The present invention relate to directional aerials and more particularly to directional aerials for-use in moving bodies whose aerodynamical characteristics should be affected as little as possible by the presence of theaerial.
An aerial according to the invention comprises, at least, one microstrip having a plurality of equally spaced radiating discontinuities obtained by laterally sifting the edges of the strip, thus forming laterally set off rectangular strip portions.
The invention will be best understood from the following description and appended drawing wherein;
FIG. I is a diagrammatic top view of the microstrip aerial according to the invention;
FIG. 2 is a detail of the aerial of FIG. ll;
FIGS. 3 to it are explanatory curves;
FIG. 9 is an embodiment of a directive aerial according to the invention;
FIG. 10 illustrates a cross section of the aerial of FIG. 9;
FIG. I1 is an explanatory perspective view; and
FIG. 12 is a radiating pattern of an aerial according to the invention. i
In FIG. I, a microstrip line 11 is illustrated as viewed from above, the ground plate being disposed in the plane of the figure. According to the invention this line comprises a plurality of discontinuities 2, spaced from each other by x,, A, designating the wavelength in the line of the energy propagating along the same.
As shown in FIG. 2, each discontinuity 2 is formed by laterally shifting the edges of a portion of the strip in a direction perpendicular to the longitudinal axis thereof. In FIG. 2, edge 3 is shifted by a distance c and edge 4 by a distance d.
The length l of each discontinuity is, in the embodiment shown, substantially equal to M4. The radiation factor i.e., the ratio of the radiated energy to the incident energy, varies as a function ofd.
To each length d corresponds a length c for which the discontinuity is matched to the line. All discontinuities being matched to the line, the energy fed to the line propagates as a progressive wave.
The projecting strip portions radiate energy and the reentrant portions insure the matching.
FIGS. 3, 4 and 5 show curves indicating how different parameters vary as a function of d, namely: the standing wave ratio with F (FIG. 3); the radiation factor p (FIG. A), distance c with the standing wave ratioequal to 1.
FIG. 6 shows the phase shift 1 due to energy radiation as a function ofd.
All these diagrams have been established for a line operating in the 10,000 Mc.-band. The line is constituted by a rexolite plate 1.6-mm.-thiclt and metallized on both faces. The strips are established according to the printed circuit techniques. The strip is 34p. thick and 4.5 mm. wide. The wavelength in such a microstrip is 19.8 mm. at 10,000 mc., and l=xs/4=5 mm.
It appears from the diagrams of FIGS. 3 and that, for c=0 and d=2, the standing wave ratio is 1.6, the radiation ratio p being equal to 0.2.
It will be apparent from FIG. 5 that, for each value of d less than d=2 mm., there is a value of e such that the standing wave ratio is made equal to I. For d greater than 2, this correction is no longer possible. This may be clearly seen from FIGS. 7 and b. FIG. 7 illustrates the standing wave ratio as a function of c for (i=2 mm. It is seen that this ratio is about 1.7 for c=0 and equal to l for $3.
In FIG. b, for d=2.5 mm., the standing wave ratio has a minimum equal to L5, for c=2.5.
FIG. 9 illustrates a guide, which feeds a plurality of lines 1111, III, 13 and MI, each line being fed at its center. The distance between two adjacent lines is M2, it being the operating wavelength. FIG. l0 shows in section how each line is coupled to guide 110. A metal plate 5 which is common to microstrips l0 and M, is supported on a metal bloclt II which rests on guide 110. A passage 15 is formed in bloclt 9, symmetrically with respect to guide 110, for coupling strips 1111 to M to the guide. A dielectric layer 117 rests on plate 5, the same dielectric lining passages 15. A probe lb couples the conductive strips 1 to guide It), probe lb and lining 115 thus forming a coaxial cable.
The discontinuities 20 are all fed in phase; they are separated by an electrical distance I substantially equal to it, and given more precisely by the formula:
An aerial according to the invention is directional. The radiation direction is along a straight line defined by the intersection of:
a. The symmetry plane of the large side of guide in which all the discontinuities are radiating in phase. This plane corresponds to plane x02 in FIG. llll, 0x being the axis of guide 10 and by parallel to the longitudinal axis of the strips.
b. A plane including axis by and making an angle 0 with the axis 0x, with cos 0=c./Vg., c being the velocity of light and Vg. the phase velocity of the wave in guide 10.
FIG. 112 shows the directive pattern obtained with an aerial according to the invention, operating at 10,000 mc., in the above defined planes. The width M of the beam at a level 3 db. below the maximum is given by the fonnula;
M =)t/a where a is the transversal dimension of the aerial. The highest secondary lobes are 25 db. lower than the main lobe. The gain is 27 db., i.e., 2 db. above the gain given by formula:
G=41T,)\2 where sis the surface of the aerial.
The invention, is of course, not limited to the embodiment shown, which is given by way of example. In particular, the distance between the discontinuities could be different from A. In this case the two planes respectively comprising the radiation directions would be inclined over the horizontal. The distance between the points where the strips are coupled to the guide could be separated by distance different from M 2.
What is claimed is:
l. A microwave directional aerial comprising at least one microstrip line having a ground plate, an insulating plate and a conductive strip superimposed upon each other, said strip having edges; means for feeding to said line ultrahigh frequency energy; both edges being laterally set off in the same direction at uniformly spaced points, thus forming radiating discontinuities.
2. A microwave directional aerial comprising a plurality of parallel, equally spaced lines having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; means for feeding to said lines ultrahigh frequency energy; both edges of each line being laterally set off in the same direction at uniformly spaced points, thus forming radiating discontinuities.
3. A microwave directional aerial comprising a plurality of parallel equally spaced lines, having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; means for feeding to said lines ultrahigh frequency energy; both said edges being laterally set off in the same direction, thus forming along a predetermined length of said strips radiating discontinuities, said discontinuities being spaced apart by the length in said microstrip of the operating wave and said predetermined length being the same for all the strips.
4. A microwave directional aerial comprising a plurality of parallel equally spaced strip lines, having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; both said edges being laterally set off in the same direction thus forming along a predetermined length of said strips radiating discontinuities, said discontinuities being spaced apart by the length in said microstrip of the operating wave and said predetermined length being the same for all the strips; a wave guide extending normally to said strip lines, said guide having a pair of large walls, one of said walls supporting said ground plate; and probes respectively coupling said strips to said guide.
Claims (4)
1. A microwave directional aerial comprising at least one microstrip line having a ground plate, an insulating plate and a conductive strip superimposed upon each other, said strip having edges; means for feeding to said line ultrahigh frequency energy; both edges being laterally set off in the same direction at uniformly spaced points, thus forming radiating discontinuities.
2. A microwave directional aerial comprising a plurality of parallel, equally spaced lines having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; means for feeding to said lines ultrahigh frequency energy; both edges of each line being laterally set off in the same direction at uniformly spaced points, thus forming radiating discontinuities.
3. A microwave directional aerial comprising a plurality of parallel equally spaced lines, having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edgeS; means for feeding to said lines ultrahigh frequency energy; both said edges being laterally set off in the same direction, thus forming along a predetermined length of said strips radiating discontinuities, said discontinuities being spaced apart by the length in said microstrip of the operating wave and said predetermined length being the same for all the strips.
4. A microwave directional aerial comprising a plurality of parallel equally spaced strip lines, having a common ground plate and a common insulating plate, each line having a conductive strip, said strips having edges; both said edges being laterally set off in the same direction thus forming along a predetermined length of said strips radiating discontinuities, said discontinuities being spaced apart by the length in said microstrip of the operating wave and said predetermined length being the same for all the strips; a wave guide extending normally to said strip lines, said guide having a pair of large walls, one of said walls supporting said ground plate; and probes respectively coupling said strips to said guide.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR780929 | 1958-12-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3643262A true US3643262A (en) | 1972-02-15 |
Family
ID=8708979
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US855234A Expired - Lifetime US3643262A (en) | 1958-12-05 | 1959-11-24 | Microstrip aerials |
Country Status (2)
Country | Link |
---|---|
US (1) | US3643262A (en) |
FR (1) | FR1603303A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4063245A (en) * | 1975-02-17 | 1977-12-13 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Microstrip antenna arrays |
US4152762A (en) * | 1976-03-03 | 1979-05-01 | Operating Systems, Inc. | Associative crosspoint processor system |
US4180817A (en) * | 1976-05-04 | 1979-12-25 | Ball Corporation | Serially connected microstrip antenna array |
US4475107A (en) * | 1980-12-12 | 1984-10-02 | Toshio Makimoto | Circularly polarized microstrip line antenna |
US4689629A (en) * | 1982-09-27 | 1987-08-25 | Rogers Corporation | Surface wave antenna |
US4937585A (en) * | 1987-09-09 | 1990-06-26 | Phasar Corporation | Microwave circuit module, such as an antenna, and method of making same |
US20090160612A1 (en) * | 2005-07-04 | 2009-06-25 | Valtion Teknillinen Tutkimuskeskus | Measurement System, Measurement Method and New Use of Antenna |
US9585203B2 (en) * | 2011-08-04 | 2017-02-28 | Panasonic Intellectual Property Management Co., Ltd. | Microwave heating device |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2605413A (en) * | 1943-11-10 | 1952-07-29 | Luis W Alvarez | Antenna system with variable directional characteristic |
FR1123769A (en) * | 1955-03-17 | 1956-09-27 | Csf | Built-in overhead for mobile vehicles |
-
1959
- 1959-11-24 US US855234A patent/US3643262A/en not_active Expired - Lifetime
-
1968
- 1968-12-05 FR FR780929A patent/FR1603303A/fr not_active Expired
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2605413A (en) * | 1943-11-10 | 1952-07-29 | Luis W Alvarez | Antenna system with variable directional characteristic |
FR1123769A (en) * | 1955-03-17 | 1956-09-27 | Csf | Built-in overhead for mobile vehicles |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4063245A (en) * | 1975-02-17 | 1977-12-13 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Microstrip antenna arrays |
US4152762A (en) * | 1976-03-03 | 1979-05-01 | Operating Systems, Inc. | Associative crosspoint processor system |
US4180817A (en) * | 1976-05-04 | 1979-12-25 | Ball Corporation | Serially connected microstrip antenna array |
US4475107A (en) * | 1980-12-12 | 1984-10-02 | Toshio Makimoto | Circularly polarized microstrip line antenna |
US4689629A (en) * | 1982-09-27 | 1987-08-25 | Rogers Corporation | Surface wave antenna |
US4937585A (en) * | 1987-09-09 | 1990-06-26 | Phasar Corporation | Microwave circuit module, such as an antenna, and method of making same |
US20090160612A1 (en) * | 2005-07-04 | 2009-06-25 | Valtion Teknillinen Tutkimuskeskus | Measurement System, Measurement Method and New Use of Antenna |
US8525647B2 (en) * | 2005-07-04 | 2013-09-03 | Valtion Teknillinen Tutkimiskeskus | Measurement system, measurement method and new use of antenna |
US9585203B2 (en) * | 2011-08-04 | 2017-02-28 | Panasonic Intellectual Property Management Co., Ltd. | Microwave heating device |
Also Published As
Publication number | Publication date |
---|---|
FR1603303A (en) | 1971-04-05 |
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