US3430246A - Plural reflector antenna with polarization rotation to minimize feedshadow - Google Patents

Plural reflector antenna with polarization rotation to minimize feedshadow Download PDF

Info

Publication number
US3430246A
US3430246A US536880A US3430246DA US3430246A US 3430246 A US3430246 A US 3430246A US 536880 A US536880 A US 536880A US 3430246D A US3430246D A US 3430246DA US 3430246 A US3430246 A US 3430246A
Authority
US
United States
Prior art keywords
reflector
polarization
waves
axis
respect
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
US536880A
Inventor
Guy Le Parquier
Robert Pierrot
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.)
Thales SA
Original Assignee
CSF Compagnie Generale de Telegraphie sans Fil 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 CSF Compagnie Generale de Telegraphie sans Fil SA filed Critical CSF Compagnie Generale de Telegraphie sans Fil SA
Application granted granted Critical
Publication of US3430246A publication Critical patent/US3430246A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10Combinations 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
    • H01Q19/18Combinations 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
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10Combinations 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
    • H01Q19/18Combinations 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
    • H01Q19/19Combinations 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 comprising one main concave reflecting surface associated with an auxiliary reflecting surface
    • H01Q19/195Combinations 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 comprising one main concave reflecting surface associated with an auxiliary reflecting surface wherein a reflecting surface acts also as a polarisation filter or a polarising device

Definitions

  • a centrally mounted feed faces a polarization selective first reflector which reflects all the waves to a polarization rotating second split reflector. The second reflector rotates the polarization of the waves and directs them back to the first reflector which is now transparent to the new polarization.
  • the present invention relates to antenna systems with two reflectors, for example of the Cassegrain type. More particularly, the invention relates to antennas wherein the polarization direction is not the same for the incident and the reflected signal.
  • the primary source casts a shadow on the reflecting surface. This adversely affects the antenna gain and increases the secondary lobes. This can be avoided at least in part by offsetting the primary source but the counterpart is that is that a dissymmetry is created.
  • an antenna system having an axis of symmetry comprising: a primary source located on said axis, for radiating waves having a given direction of polarization; a first reflector, positioned on the path of said wave, which is not transparent for the waves having said given direction of polarization and which is transparent for the waves having a different direction of polarization, said first reflector being symmetrical with respect to said axis; a second reflector positioned on the path of the waves reflected by said first reflector and which modifies the direction of polarization of waves incident thereon, said second reflector being symmetrical With respect to said axis; and a dioptric system, symmetrical with respect to said axis and positioned on the path of the waves reflected by said second reflector, said dioptric system making parallel the waves incident thereon.
  • the two reflectors build up an aplanatic system.
  • the system shown comprises a primary source 1, or an array of primary sources, normal to the plane of the fig- 3,430,246 Patented Feb. 25, 1969 ure; a first reflector which is not transparent for the polarization direction of the source 1 and which is formed by two identical paraboloid portions which have the same focus and are symmetrical with respect to the axis of the antenna system; a second reflector 3 formed by two plane reflector elements, also symmetrical with respect to the axis of the antenna system, and a double prism 4.
  • the second reflector is so built that it modifies the polarization direction of the incident signal.
  • the second reflector builds up, together with the first reflector, an aplanatic system.
  • the spherical wave which is generated by the primary source 1 is reflected by reflector 2 as two plane waves which propagate along the respective axes of the two paraboloids building up the reflector 2.
  • the polarization rotating reflector may comprise, as is well known, a reflecting metal surface, covered with a layer of dielectric, such as a resin, in which i incorporated a mesh of parallel wires which are spaced by at most half the maximum operating wavelength and inclined by 45 with respect to the polarization of the incident wave, all this being well known in the art.
  • the antenna system of the invention has an exit aperture without any-shadow or inactive surface portion, thus improving the antenna performance as to gain, secondary lobes and diffused radiations.
  • the standing wave ratio is improved since the waves reflected by reflector 2 do not interfere with the primary source.
  • the invention is not limited to the embodiment described and shown, since obviously the essential component parts of the antenna system according to the invention, namely the semitransparent reflector system, the reflector system which causes the polarization direction to change and the dioptric system used, may be of various types without departing from the spirit and scope of the invention.
  • An antenna system having an axis of symmetry comprising: a primary source located on said axis for radiating waves having a given direction of polarization; a first reflector positioned on the path of said wave which is not transparent for the waves having said given direction of polarization and which is transparent for the waves having a different direction of polarization, said first reflector comprising two parts symmetrical with respect to said axis, the two parts of said reflector being portions of respective surfaces intersecting each other on said axis, the planes respectively tangent to said surfaces on said axes being at an angle with respect to each other; a second reflector positioned on the path of the waves reflected by said first reflector and which modifies the direction of polarization of waves incident thereon, said second reflector being symmetrical with respect to said axis; and a dioptric system symmetrical with respect to said axis and positioned on the path of the waves reflected by said second reflector, said dioptric system making parallel the waves incident thereon.
  • said first reflector is formed by two adjacent identical paraboloid portions which have the same focus and are symmetrical respect to said axis, the axes of said paraboloids being at an angle with respect to each other and said second re- 15 4' flector is formed by two adjacent plane reflector elements, also symmetrical with respect to said axis, the planes of said elements being at an angle with respect to each other.
  • said first and second reflectors build up an aplanatic system.

Landscapes

  • Aerials With Secondary Devices (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Description

3 4: :5 6 U U I i QLHHUH HUVI Feb. 25, 1969 G. LE-PARQUIER ETAL 3,
PLURAL REFLECTOR ANTENNA WITH POLARIZATION ROTATION TO MINIMIZE FEED SHADOW Filed March 25, 1966 United States Patent US. Cl. 343-756 Int. Cl. H0111 19/14, 15/22 5 Claims ABSTRACT OF THE DISCLOSURE A Cassegrain antenna having a feed system to minimize shadow effect. A centrally mounted feed faces a polarization selective first reflector which reflects all the waves to a polarization rotating second split reflector. The second reflector rotates the polarization of the waves and directs them back to the first reflector which is now transparent to the new polarization.
The present invention relates to antenna systems with two reflectors, for example of the Cassegrain type. More particularly, the invention relates to antennas wherein the polarization direction is not the same for the incident and the reflected signal.
In an antenna system comprising a reflector, the primary source casts a shadow on the reflecting surface. This adversely affects the antenna gain and increases the secondary lobes. This can be avoided at least in part by offsetting the primary source but the counterpart is that is that a dissymmetry is created.
It is an object of the invention to provide an antenna system wherein the shadow effect is avoided and yet the primary source remains in a central position.
According to the invention there is provided an antenna system having an axis of symmetry comprising: a primary source located on said axis, for radiating waves having a given direction of polarization; a first reflector, positioned on the path of said wave, which is not transparent for the waves having said given direction of polarization and which is transparent for the waves having a different direction of polarization, said first reflector being symmetrical with respect to said axis; a second reflector positioned on the path of the waves reflected by said first reflector and which modifies the direction of polarization of waves incident thereon, said second reflector being symmetrical With respect to said axis; and a dioptric system, symmetrical with respect to said axis and positioned on the path of the waves reflected by said second reflector, said dioptric system making parallel the waves incident thereon.
According to a preferred embodiment of the invention, the two reflectors build up an aplanatic system.
For a better understanding of the invention and to show how the same may be carried into effect, reference will be made to the drawing accompanying the following description and the only figure of which shows by way of example one embodiment of the system according to the invention.
The system shown comprises a primary source 1, or an array of primary sources, normal to the plane of the fig- 3,430,246 Patented Feb. 25, 1969 ure; a first reflector which is not transparent for the polarization direction of the source 1 and which is formed by two identical paraboloid portions which have the same focus and are symmetrical with respect to the axis of the antenna system; a second reflector 3 formed by two plane reflector elements, also symmetrical with respect to the axis of the antenna system, and a double prism 4. The second reflector is so built that it modifies the polarization direction of the incident signal. Preferably, the second reflector builds up, together with the first reflector, an aplanatic system.
The spherical wave which is generated by the primary source 1 is reflected by reflector 2 as two plane waves which propagate along the respective axes of the two paraboloids building up the reflector 2.
These two plane waves are respectively reflected, while their polarization direction is modified, by the two plane elements 3 and then propagate through reflector 2, which is transparent, for the polarization direction they have by now, towards the double prism 4 which receives the two incident waves and changes their respective propagation directions to make them parallel, so that there is, at the output of the prism, a single plane wave propagating along the axis of the antenna system.
It should be noted that all the elements building up the system of the invention are entirely conventional and therefore need not be described in more detail.
Thus, the polarization rotating reflector may comprise, as is well known, a reflecting metal surface, covered with a layer of dielectric, such as a resin, in which i incorporated a mesh of parallel wires which are spaced by at most half the maximum operating wavelength and inclined by 45 with respect to the polarization of the incident wave, all this being well known in the art.
The antenna system of the invention has an exit aperture without any-shadow or inactive surface portion, thus improving the antenna performance as to gain, secondary lobes and diffused radiations.
Also the standing wave ratio is improved since the waves reflected by reflector 2 do not interfere with the primary source.
Of course the invention is not limited to the embodiment described and shown, since obviously the essential component parts of the antenna system according to the invention, namely the semitransparent reflector system, the reflector system which causes the polarization direction to change and the dioptric system used, may be of various types without departing from the spirit and scope of the invention.
What is claimed is:
1. An antenna system having an axis of symmetry comprising: a primary source located on said axis for radiating waves having a given direction of polarization; a first reflector positioned on the path of said wave which is not transparent for the waves having said given direction of polarization and which is transparent for the waves having a different direction of polarization, said first reflector comprising two parts symmetrical with respect to said axis, the two parts of said reflector being portions of respective surfaces intersecting each other on said axis, the planes respectively tangent to said surfaces on said axes being at an angle with respect to each other; a second reflector positioned on the path of the waves reflected by said first reflector and which modifies the direction of polarization of waves incident thereon, said second reflector being symmetrical with respect to said axis; and a dioptric system symmetrical with respect to said axis and positioned on the path of the waves reflected by said second reflector, said dioptric system making parallel the waves incident thereon.
2. A system according to claim 1, wherein said different direction is perpendicular to said given direction.
3. A system according to claim 2, wherein said parts are adjacent surface portions, symmetrical with respect to said axis.
4. A system according to claim 2, wherein said first reflector is formed by two adjacent identical paraboloid portions which have the same focus and are symmetrical respect to said axis, the axes of said paraboloids being at an angle with respect to each other and said second re- 15 4' flector is formed by two adjacent plane reflector elements, also symmetrical with respect to said axis, the planes of said elements being at an angle with respect to each other. 5. A system according to claim 2, wherein said first and second reflectors build up an aplanatic system.
References Cited UNITED STATES PATENTS 2,736,895 2/1956 Cochrane 343-756 ELI LIEBERMAN, Primary Examiner.
US. Cl. X.R. 343-781, 837, 914
US536880A 1965-03-31 1966-03-23 Plural reflector antenna with polarization rotation to minimize feedshadow Expired - Lifetime US3430246A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR11338A FR1438482A (en) 1965-03-31 1965-03-31 Dual reflector antenna without source shadow

Publications (1)

Publication Number Publication Date
US3430246A true US3430246A (en) 1969-02-25

Family

ID=8575289

Family Applications (1)

Application Number Title Priority Date Filing Date
US536880A Expired - Lifetime US3430246A (en) 1965-03-31 1966-03-23 Plural reflector antenna with polarization rotation to minimize feedshadow

Country Status (5)

Country Link
US (1) US3430246A (en)
DE (1) DE1516741A1 (en)
FR (1) FR1438482A (en)
GB (1) GB1123951A (en)
NL (1) NL6604261A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4011525A (en) * 1975-01-21 1977-03-08 Compagnie Generale D'electricite Gas laser generator
US4712111A (en) * 1984-12-26 1987-12-08 Sharp Kabushiki Kaisha Antenna system
US4823143A (en) * 1988-04-22 1989-04-18 Hughes Aircraft Company Intersecting shared aperture antenna reflectors
US20150022391A1 (en) * 2013-07-18 2015-01-22 Rohde & Schwarz Gmbh & Co. Kg System and a method for illumination and imaging of an object

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736895A (en) * 1951-02-16 1956-02-28 Elliott Brothers London Ltd High frequency radio aerials

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736895A (en) * 1951-02-16 1956-02-28 Elliott Brothers London Ltd High frequency radio aerials

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4011525A (en) * 1975-01-21 1977-03-08 Compagnie Generale D'electricite Gas laser generator
US4712111A (en) * 1984-12-26 1987-12-08 Sharp Kabushiki Kaisha Antenna system
US4823143A (en) * 1988-04-22 1989-04-18 Hughes Aircraft Company Intersecting shared aperture antenna reflectors
US20150022391A1 (en) * 2013-07-18 2015-01-22 Rohde & Schwarz Gmbh & Co. Kg System and a method for illumination and imaging of an object
US9658320B2 (en) * 2013-07-18 2017-05-23 Rohde & Schwarz Gmbh & Co. Kg System and a method for illumination and imaging of an object

Also Published As

Publication number Publication date
DE1516741A1 (en) 1969-06-26
GB1123951A (en) 1968-08-14
NL6604261A (en) 1966-10-03
FR1438482A (en) 1966-05-13

Similar Documents

Publication Publication Date Title
US3231892A (en) Antenna feed system simultaneously operable at two frequencies utilizing polarization independent frequency selective intermediate reflector
US3797020A (en) Microwave antenna structure with aperture blocking elimination
US3394378A (en) Multiple reflector multiple frequency band antenna system
US3828352A (en) Antenna system employing toroidal reflectors
US3821746A (en) Antenna system with distortion compensating reflectors
US3340535A (en) Circular polarization cassegrain antenna
US4096483A (en) Reflector with frequency selective ring of absorptive material for aperture control
US4144535A (en) Method and apparatus for substantially reducing cross polarized radiation in offset reflector antennas
US4223316A (en) Antenna structure with relatively offset reflectors for electromagnetic detection and space telecommunication equipment
US4208661A (en) Antenna with two orthogonally disposed parabolic cylindrical reflectors
US3102265A (en) New aerial system radiating several beams
US3414904A (en) Multiple reflector antenna
US3430246A (en) Plural reflector antenna with polarization rotation to minimize feedshadow
US3710341A (en) Gregorian antenna with ring focus
Dragone New grids for improved polarization diplexing of microwaves in reflector antennas
US4977407A (en) Optical collimator
US3241147A (en) Antenna utilizing intermediate cuspate reflector to couple energy from feed to main reflector
US2942266A (en) Antenna with means for preventing re-radiation into feed guide
US2607010A (en) Wave guide antenna system
US3514779A (en) Antennae with focusing devices
US2656464A (en) Feed locus for semiparabolic reflector
US3370295A (en) Doubly reflecting latticed antenna
US3122745A (en) Reflection antenna employing multiple director elements and multiple reflection of energy to effect increased gain
JPS6019303A (en) Antenna
GB1342892A (en) Aircraft antennas