GB2242072A - Reflector antenna - Google Patents

Reflector antenna Download PDF

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Publication number
GB2242072A
GB2242072A GB9005915A GB9005915A GB2242072A GB 2242072 A GB2242072 A GB 2242072A GB 9005915 A GB9005915 A GB 9005915A GB 9005915 A GB9005915 A GB 9005915A GB 2242072 A GB2242072 A GB 2242072A
Authority
GB
United Kingdom
Prior art keywords
reflector
feed unit
axis
central axis
polarization
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.)
Granted
Application number
GB9005915A
Other versions
GB2242072B (en
GB9005915D0 (en
Inventor
Joseph Raphael Parkinson
Brian Stuart Collins
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.)
CSA Ltd
C&S Antennas Ltd
Original Assignee
CSA Ltd
C&S Antennas Ltd
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 CSA Ltd, C&S Antennas Ltd filed Critical CSA Ltd
Priority to GB9005915A priority Critical patent/GB2242072B/en
Publication of GB9005915D0 publication Critical patent/GB9005915D0/en
Publication of GB2242072A publication Critical patent/GB2242072A/en
Application granted granted Critical
Publication of GB2242072B publication Critical patent/GB2242072B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • H01Q15/22Reflecting surfaces; Equivalent structures functioning also as polarisation filter
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • H01Q15/16Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal
    • 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
    • H01Q19/12Combinations 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 wherein the surfaces are concave
    • H01Q19/13Combinations 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 wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination
    • H01Q19/132Horn reflector antennas; Off-set feeding

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aerials With Secondary Devices (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

To reduce the wind loading and weight of the antenna reflector (20), its surface is formed from a number of parallel spaced apart rods (24) joined by transverse link bars (26). A reflector mounting (28) permits rotation of the reflector (20) about a central axis (22) to align the nods (24) with the axis of polarization of a signal radiated by the offset antenna feed unit (32). The reflector surface, defined by a section of the surface of a sphere, is symmetrical about the central axis (22), such that the centre of gravity of the reflector lies on the axis (22) and the load on the reflector support structure (30) remains constant as the reflector is rotated. <IMAGE>

Description

REFLECTOR ANTENNA The present invention relates to ref lector antennas and in particular to such antennas which are operable to radiate signals linearly polarised in either a vertical or a horizontal plane, the plane of polarization being defined by the direction of the electric (E) field.
The reflector surface may be a continuous dished surface, but for transportable operation where it is desired to use a lightweignt, easily erected supporting structure, this has the severe disadvantage of presenting an unacceptably large wind-loaded area. Wind loading may be reduced by making the ref lector surface in the form of a grid of rods.
In accordance with the present invention there is provided an antenna assembly including a feed unit, a reflector and a ref lector mounting, in which the reflector surface is substantially syrtirrietrical about a central axis and is formed fram a number of substantially parallel rods, and in which the mounting permits rotation of the ref lector about the central axis to align the rods with the axis of polarization of a signal radiated by the feed unit.
The use of bars extending in only one direction means that the reflector of the present invention has less total surface area and is thus lighter than grid surface reflectors.
The present invention has particular application to antennas having offset geometry, that is to say antennas in which the feed unit is positioned such that the radiation reflected by the reflector surface does not impinge on the feed unit. Such offset antennas thereby avoid the problems of scattering fran the feed unit and blockage of part of the main ref lector aperture.
The conventional form of offset antenna makes use of shape of reflector which represents part of the surface of a paraboloid, but this surface is not symmetrical about its centre. If operation in two planes of polarisation is required (even if not required simultaneously) the ref lector must be provided with rods in both the horizontal and vertical planes, increasing its wind-loaded area.
Since the reflector surface of the present invention is to be substantially symmetrical about a central axis and the reflector mounting permits rotation about that axis, the spatial relationship between the feed unit and reflector remains constant whether the rods of the reflector surface are aligned vertically or horizontally. Additionally, the centre of gravity of the reflector remains constant giving uniform loading on the support structure. A suitable shape for the reflector is a section of the surface of a sphere.
One particular preferred embodiment of the present invention, in the form of an offset antenna, will now be described with reference to the accompanying drawings, in which: Figure 1 is a side sectional view of a known antenna structure illustrating the general principle of operation of an offset antenna; Figure 2 shows an antenna assembly embodying the present invention arranged to radiate vertically polarized signals; and Figure 3 is a schematic elevation showing the relative angular orientation of the reflector and feed unit.
Referring initially to Figure 1, an offset reflector is shown radiating a linearly polarized signal. The reflector surface 10 is in the form of a section of the surface of a sphere with the antenna feed 12 located at a predetermined position relative to the reflector 10. The signal 14 reflected from the reflector surface does not impinge on the feed unit 12. As can be seen, some distortion of the radiated signal 14 may occur at the upper edge of the reflector surface 10 where the angle subtended by the feed unit signal is greatest.
The reflector antenna assembly of the present invention is illustrated in Figure 2. The reflector 20 is in the form of a section of the surface of a sphere and is symmetrical about a central axis 22. The reflector surface is made up of a number of spaced apart parallel rods 24 joined together by transverse link bars 26. The reflector 20 is mounted on a rotatable support 28 with its central axis 22 at a predetermined angle e0 to the horizontal. The rotatable support 28 is in turn mounted on a suitable lightweight support structure 30.
The rotatable support 28 is positioned to allow rotation of the reflector 20 about its axis of symmetry 22, such that the positional relationship between the reflector 20 and the antenna offset feed unit 32 remains the sarre regardless of the degree of rotation of the reflector 20 about the axis 22.
The feed unit 32 is also rotatably mounted, allowing rotation about an axis 34 inclined at a predetermined angle fi to the horizontal. The feed unit 32 radiates a signal having a fixed polarization in relation thereto, the selection of vertical or horizontal polarization being achieved by rotation of the feed unit 32 about its axis.
In operation, when the antenna is set to radiate a vertically polarised signal as shown in Figure 2, the rods 24 making up the ref lector surface are positioned to extend in substantially vertical planes. The feed unit 32 is rotatably positioned such that the signal radiated towards the reflector 20 is vertically polarized.
To adjust the antenna to radiate a horizontally polarized signal, the feed unit 32 and ref lector 20 are rotated by 900 about their respective axes 34, 22, the rods 24 thus becang horizontally orientated.
Referring to figure 3, the reflector 10 has a width D and is defined by a section of the surface of a sphere of radius R centred on a point P. The reflectors' central axis 22 is inclined at an angle e0 to the horizontal. The antenna feed 12 is located between the reflector surface 10 and the point P, at a distance Zf from the point P. The feed axis 34 is inclined at an angle ss f to the horizontal. The maximum angle of elevation ef, with respect to the feed axis 34, of a signal radiated by the feed unit 12 occurs at the top edge of the reflector.
Suitable values for these distances and angles are: R = 1300mm SO = 25.00 D = 1200mm Ef = 50.70 Zf = 805mm /3f = 38.40 The reflector 20 of the present invention has less wind loaded surface area and is lighter than known grid surface reflectors thereby requiring less strengthening of the support structure 30.
In addition, where the reflector 20 is symmetrical about its central axis 22, rotation of the reflector to a vertical orientation from a horizontal orientation or vice versa will not place stress on the support structure, due to the constant position of the centre of gravity of the reflector.

Claims (6)

1. An antenna assembly including a feed unit, a reflector and a reflector mounting, in which the reflector surface is substantially symmetrical about a central axis and is formed from a number of substantially parallel rods, and in which the mounting permits rotation of the reflector about the central axis to align the rods with the axis of polarization of a signal radiated by the feed unit.
2. Apparatus according to claim 1 in which the reflector surface is defined by a section of the surface of a sphere.
3. Apparatus according to claim 1 or claim 2 in which the feed unit is an offset feed unit.
4. An antenna assembly including a feed unit, a reflector and a reflector mounting, in which the reflector surface is defined by a section of the surface of a sphere, is substantially symmetrical about a central axis and is formed from a number of substantially parallel rods; in which the feed unit is an offset feed unit, and in which the mounting permits rotation of the reflector about the central axis to align the rods with the axis of polarization of a signal radiated by the feed unit.
5. Apparatus according to any preceding claim in which the signal radiated by the feed unit has a fixed polarization axis in relation thereto, and in which the feed unit is rotatably mounted to permit rotation of the said polarization axis.
6. An antenna assembly substantially as hereinbefore described with reference to Figure 2 of the accompanying drawings.
GB9005915A 1990-03-16 1990-03-16 Reflector antenna Expired - Fee Related GB2242072B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9005915A GB2242072B (en) 1990-03-16 1990-03-16 Reflector antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9005915A GB2242072B (en) 1990-03-16 1990-03-16 Reflector antenna

Publications (3)

Publication Number Publication Date
GB9005915D0 GB9005915D0 (en) 1990-05-09
GB2242072A true GB2242072A (en) 1991-09-18
GB2242072B GB2242072B (en) 1993-12-08

Family

ID=10672709

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9005915A Expired - Fee Related GB2242072B (en) 1990-03-16 1990-03-16 Reflector antenna

Country Status (1)

Country Link
GB (1) GB2242072B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009131177A1 (en) * 2008-04-23 2009-10-29 マスプロ電工株式会社 Offset parabola antenna
CN102683855A (en) * 2012-04-28 2012-09-19 深圳光启创新技术有限公司 Portable satellite antenna

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2096398A (en) * 1981-03-24 1982-10-13 Era Patents Ltd High performance radio antenna
GB2135132A (en) * 1983-01-26 1984-08-22 Anixter Bros Grid parabolic antenna

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2096398A (en) * 1981-03-24 1982-10-13 Era Patents Ltd High performance radio antenna
GB2135132A (en) * 1983-01-26 1984-08-22 Anixter Bros Grid parabolic antenna

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009131177A1 (en) * 2008-04-23 2009-10-29 マスプロ電工株式会社 Offset parabola antenna
CN102683855A (en) * 2012-04-28 2012-09-19 深圳光启创新技术有限公司 Portable satellite antenna

Also Published As

Publication number Publication date
GB2242072B (en) 1993-12-08
GB9005915D0 (en) 1990-05-09

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940316