US2852775A - Aerial for wide frequency bands - Google Patents

Aerial for wide frequency bands Download PDF

Info

Publication number
US2852775A
US2852775A US588374A US58837456A US2852775A US 2852775 A US2852775 A US 2852775A US 588374 A US588374 A US 588374A US 58837456 A US58837456 A US 58837456A US 2852775 A US2852775 A US 2852775A
Authority
US
United States
Prior art keywords
aerial
slot
frequency bands
fin
wide frequency
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
Application number
US588374A
Inventor
Zisler Siegfried
Welser Sigmund Von
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sadir Carpentier SA
Original Assignee
Sadir Carpentier SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sadir Carpentier SA filed Critical Sadir Carpentier SA
Application granted granted Critical
Publication of US2852775A publication Critical patent/US2852775A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC 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

Definitions

  • the present invention relates to broad frequency band aerials in the range of short and very short waves.
  • Aerials of this type which comprise two coplanar circular discs located in the proximity of each other. High frequency voltage is applied to the aerial across the points of the discs which are the nearest to each other.
  • Fig. 1 illustrates an antenna arrangement of the prior art
  • Figs. 2 and 3 show respectively two portions of an aerial according to the invention
  • Fig. 4 shows an aerial according to the invention
  • Figs. 5 and 6 show modifications of the aerial of Fig. 4.
  • FIG. 1 Referring to the known aerial shown in Fig. 1, two circular discs 1 and 2 are shown in the plane of the figure and high frequency voltage is applied across points 3 and 4 corresponding to the minimum spacing between the discs.
  • Fig. 1 The applicants have considered the aerial of Fig. 1 as being constituted by the parallel arrangement of two aerials, each comprising two semi-circular discs as shown in Fig. 2 which illustrates two semi-circular discs bordered by vertical diameters passing respectively through.
  • disc sections removed from discs 1 and 2 may be advantageously replaced by a metal plate of the shape illustrated in Fig. 3.
  • This plate forms a semi-circular disc, the vertical diameter of which is defined by the distance 78 in Fig. 2 and in which a medial rectangular slot is cut out, the apices of which are points 3, 4, 5 and 6.
  • Sides 3-5 and 4-6 are normal to the diameter 78, and equal to one quarter the average operating wavelength.
  • the aerial shown in Fig. 4 has an impedance which is substantially equal to that of the assembly of Fig. 2, i. e. an impedance which is twice that of the aerial illustrated in Fig. 1.
  • the characteristic impedance of the slot 3-6 is preferable for the characteristic impedance of the slot 3-6 to be practically above 200 ohms, which may be readily obtained.
  • the radiation pattern of the aerial according to the invention is substantially identical to that of the aerial of Fig. 1 with practically the same frequency band.
  • the slot 36 it is not essential for the slot 36 to have a length exactly equal to one quarter of the average working wave length. It suflices that the impedance of the slot be, within the frequency band considered, high with respect to the impedance of the aerial.
  • the right hand portions of the antenna of Fig. 4 which correspond to those shown in Fig. 2 need not be exactly circular and can depart from this shape and still preserve the essential characteristics of the antenna shown in Fig. 4. This latter is symmetrical with reference to the horizontal axis of the slot 3-45-6.
  • Fig. 5 illustrates the application of the theory of electrical images to the embodiment of Fig. 4; in other words, the aerial shown in Fig. 4 is cut along its horizontal axis of symmetry and a metal sheet which for all practical purposes may be considered as infinite, is substituted for its lower section.
  • the aerial of Fig. 5 comprises an upper section, having a right hand portion in the shape of half a circle limited by the diameter 3-7, or having a similar shape, and an adjacent left hand portion equivalent to the half of the plate of Fig. 3, and a lower section in the shape of a continuous sheet 11, connected to the above left hand portion along the line 910.
  • the impedance of the aerial according to this modification is equal to half that of the aerial illustrated in Fig. 4.
  • the modification shown in Fig. 5 can be used in a particularly advantageous manner as an airplane aerial, because such an aerial may be easily fitted on the rear section of a vertical fin without any modification of the original contour of the fin, as shown in Fig. 6.
  • This figure shows the upper end of an airplane fin 16 with the aerial formed by the rear portion thereof, while the contour of its leading edge 15 remains unaltered.
  • the lower part of the fin i. e. the partwhich is below the slot, can be used as the metal sheet 11 of Fig. 5.
  • An insulating element 20 is fitted into the trailing edge of the fin for obvious reasons.
  • an airplane fin of the type illustrated has two metal surfaces arranged symmetrically with reference to the median plane, it is possible to provide two aerials according to the invention on either sides of such a fin respectively. Due to the small distance betweensuch two aerials, it is possible to feed them in parallel and consequently to consider them as forming together a single aerial.
  • An aerial comprising a substantially quarter-circular metal sheet defining a substantially quarter-circular peripheral arc and two mutually perpendicular radii connected to the ends of the arc, said sheet defining a rectangular recess longitudinally disposed along one of the radii and intersecting the other of the radii, an arcuate metal sheet with a peripheral are connected intermediate the recess and the quarter-circular arc, said metal sheets being connected, and a conductive element connected to said quarter-circular sheet and bordering the recess so as to make a slot thereof.
  • An aerial as claimed in claim 2 comprising means for feeding energy across the slot.

Description

Sept. 16, 1958 s. ZlSLER ETAL 2,352,775
AERIAL FOR WIDE FREQUENCY BANDS Filed May 31, 1956 United States Patent AERIAL FOR WIDE FREQUENCY BANDS Siegfried Zisler, Bievres, and Sigmund Von Welser, Paris, France, assignors to Sadir-Carpentier, Paris, France, a corporation of France Application May 31, 1956, Serial No. 588,374
Claims priority, application France June 16, 1955 6 Claims. (Cl. 343767) The present invention relates to broad frequency band aerials in the range of short and very short waves.
Aerials of this type are known which comprise two coplanar circular discs located in the proximity of each other. High frequency voltage is applied to the aerial across the points of the discs which are the nearest to each other.
The invention will be best understood from the following drawing wherein:
Fig. 1 illustrates an antenna arrangement of the prior art;
Figs. 2 and 3 show respectively two portions of an aerial according to the invention;
Fig. 4 shows an aerial according to the invention;
Figs. 5 and 6 show modifications of the aerial of Fig. 4.
Referring to the known aerial shown in Fig. 1, two circular discs 1 and 2 are shown in the plane of the figure and high frequency voltage is applied across points 3 and 4 corresponding to the minimum spacing between the discs.
The applicants have considered the aerial of Fig. 1 as being constituted by the parallel arrangement of two aerials, each comprising two semi-circular discs as shown in Fig. 2 which illustrates two semi-circular discs bordered by vertical diameters passing respectively through.
points 3, 7 and 4, 8, ultra high frequency energy being fed, as in the case of Fig. 1, across points 3 and 4.
Applicants have also found that the disc sections removed from discs 1 and 2 may be advantageously replaced by a metal plate of the shape illustrated in Fig. 3. This plate forms a semi-circular disc, the vertical diameter of which is defined by the distance 78 in Fig. 2 and in which a medial rectangular slot is cut out, the apices of which are points 3, 4, 5 and 6. Sides 3-5 and 4-6 are normal to the diameter 78, and equal to one quarter the average operating wavelength.
The presence of this quarter-wave slot makes the impedance of the arrangement shown in Fig. 3 very high relative to that of the aerial of Fig. 2. Furthermore the continuity of the metal structure, obtained by integrally assembling the plate of Fig. 3 with the two semi-circular discs of Fig. 2 on the left hand side thereof, to provide the complete aerial shown in Fig. 4, is such that the electric field of the two semi-circular discs is practically identical in Fig. 4 and in Fig. 1.
Consequently the aerial shown in Fig. 4 has an impedance which is substantially equal to that of the assembly of Fig. 2, i. e. an impedance which is twice that of the aerial illustrated in Fig. 1.
In order to obtain favorable results, it is preferable for the characteristic impedance of the slot 3-6 to be practically above 200 ohms, which may be readily obtained.
Under such conditions, the radiation pattern of the aerial according to the invention is substantially identical to that of the aerial of Fig. 1 with practically the same frequency band.
It should be remarked that it is not essential for the slot 36 to have a length exactly equal to one quarter of the average working wave length. It suflices that the impedance of the slot be, within the frequency band considered, high with respect to the impedance of the aerial.
The right hand portions of the antenna of Fig. 4 which correspond to those shown in Fig. 2 need not be exactly circular and can depart from this shape and still preserve the essential characteristics of the antenna shown in Fig. 4. This latter is symmetrical with reference to the horizontal axis of the slot 3-45-6.
Fig. 5 illustrates the application of the theory of electrical images to the embodiment of Fig. 4; in other words, the aerial shown in Fig. 4 is cut along its horizontal axis of symmetry and a metal sheet which for all practical purposes may be considered as infinite, is substituted for its lower section. The aerial of Fig. 5 comprises an upper section, having a right hand portion in the shape of half a circle limited by the diameter 3-7, or having a similar shape, and an adjacent left hand portion equivalent to the half of the plate of Fig. 3, and a lower section in the shape of a continuous sheet 11, connected to the above left hand portion along the line 910. The impedance of the aerial according to this modification is equal to half that of the aerial illustrated in Fig. 4.
The modification shown in Fig. 5 can be used in a particularly advantageous manner as an airplane aerial, because such an aerial may be easily fitted on the rear section of a vertical fin without any modification of the original contour of the fin, as shown in Fig. 6. This figure shows the upper end of an airplane fin 16 with the aerial formed by the rear portion thereof, while the contour of its leading edge 15 remains unaltered. Experience has shown that the lower part of the fin, i. e. the partwhich is below the slot, can be used as the metal sheet 11 of Fig. 5. An insulating element 20 is fitted into the trailing edge of the fin for obvious reasons.
Experience shows that the aerial thus incorporated into the airplane fin operates substantially in the same manner as that illustrated in Fig. 5, its radiation diagram, its impedance and its frequency bandwidth being the same.
Since an airplane fin of the type illustrated has two metal surfaces arranged symmetrically with reference to the median plane, it is possible to provide two aerials according to the invention on either sides of such a fin respectively. Due to the small distance betweensuch two aerials, it is possible to feed them in parallel and consequently to consider them as forming together a single aerial.
Obviously the embodiments described can undergo many other modifications Without departing from the scope of the invention as defined in the accompanying claims.
What we claim is:
1. An aerial comprising a substantially quarter-circular metal sheet defining a substantially quarter-circular peripheral arc and two mutually perpendicular radii connected to the ends of the arc, said sheet defining a rectangular recess longitudinally disposed along one of the radii and intersecting the other of the radii, an arcuate metal sheet with a peripheral are connected intermediate the recess and the quarter-circular arc, said metal sheets being connected, and a conductive element connected to said quarter-circular sheet and bordering the recess so as to make a slot thereof.
2. An aerial as claimed in claim 1 wherein the length of the slot is substantially equal to one quarter of the average wavelength to be processed.
3. An aerial as claimed in claim 2 wherein the metal sheets and conductive element form a symmetrical configuration about the longitudinal axes of the slot.
4. An aerial as claimed in claim 2 wherein the conductive element is a metal sheet.
5. An aerial as claimed in claim 2, wherein the sheets and conductive elements are parts of an airplane fin, comprising an insulator fillet filling in the slot and rounding ofi the contour of the fin.
6. An aerial as claimed in claim 2 comprising means for feeding energy across the slot.
4 7 References Cited in the file of this patent VUNITED STATES PATENTS Harvey June 5, 1951
US588374A 1955-06-16 1956-05-31 Aerial for wide frequency bands Expired - Lifetime US2852775A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR2852775X 1955-06-16

Publications (1)

Publication Number Publication Date
US2852775A true US2852775A (en) 1958-09-16

Family

ID=9689324

Family Applications (1)

Application Number Title Priority Date Filing Date
US588374A Expired - Lifetime US2852775A (en) 1955-06-16 1956-05-31 Aerial for wide frequency bands

Country Status (1)

Country Link
US (1) US2852775A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0377858A1 (en) * 1989-01-10 1990-07-18 Ball Corporation Embedded surface wave antenna
AU633458B1 (en) * 1991-08-26 1993-01-28 Hughes Aircraft Company Asymmmetrically flared notch radiator
US7595765B1 (en) 2006-06-29 2009-09-29 Ball Aerospace & Technologies Corp. Embedded surface wave antenna with improved frequency bandwidth and radiation performance
US8736502B1 (en) 2008-08-08 2014-05-27 Ball Aerospace & Technologies Corp. Conformal wide band surface wave radiating element

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2555433A (en) * 1951-06-05 Automatic safety shutqff system for

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2555433A (en) * 1951-06-05 Automatic safety shutqff system for

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0377858A1 (en) * 1989-01-10 1990-07-18 Ball Corporation Embedded surface wave antenna
AU633458B1 (en) * 1991-08-26 1993-01-28 Hughes Aircraft Company Asymmmetrically flared notch radiator
US5187489A (en) * 1991-08-26 1993-02-16 Hughes Aircraft Company Asymmetrically flared notch radiator
US7595765B1 (en) 2006-06-29 2009-09-29 Ball Aerospace & Technologies Corp. Embedded surface wave antenna with improved frequency bandwidth and radiation performance
US8736502B1 (en) 2008-08-08 2014-05-27 Ball Aerospace & Technologies Corp. Conformal wide band surface wave radiating element

Similar Documents

Publication Publication Date Title
US2455403A (en) Antenna
US2760169A (en) Microwave filters
US3031665A (en) Wide band slot antenna
US2921276A (en) Microwave circuits
US2575571A (en) Wave-signal directional coupler
US2472106A (en) Broad band antenna
US3218644A (en) Frequency independent slot antenna
US2852775A (en) Aerial for wide frequency bands
US2321521A (en) Frequency band filter
US2597081A (en) Joint for wave guides
US3087159A (en) Microwave scimitared antenna
US3039095A (en) Broadband aircraft foil antenna
GB708008A (en) Improvements in or relating to folded slot aerials
US2825062A (en) Antenna
US2632851A (en) Electromagnetic radiating or receiving apparatus
GB798821A (en) Improvements in or relating to aerials for metric, decimetric or centimetric waves, of flat form and capable of being applied to flat surfaces
US2493514A (en) Multiply-resonant stub antenna
GB1042620A (en) High frequency electron discharge devices embodying slow-wave structures
RU146938U1 (en) BROADBAND SUBSCRIBER ANTENNA (OPTIONS)
US2714659A (en) Broad band unidirectional antenna
US3224004A (en) Radiating slot ridged waveguides
US2845624A (en) Low drag airplane antenna
US2568710A (en) Wide-band antenna
US2456803A (en) High-frequency energy leakage suppressor
US3824504A (en) Microwave filter