EP0084420A2 - Antenne, besonders zum Empfang von Übertragungssatelliten - Google Patents

Antenne, besonders zum Empfang von Übertragungssatelliten Download PDF

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Publication number
EP0084420A2
EP0084420A2 EP83300106A EP83300106A EP0084420A2 EP 0084420 A2 EP0084420 A2 EP 0084420A2 EP 83300106 A EP83300106 A EP 83300106A EP 83300106 A EP83300106 A EP 83300106A EP 0084420 A2 EP0084420 A2 EP 0084420A2
Authority
EP
European Patent Office
Prior art keywords
reflector
antenna
sub
antenna according
main reflector
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.)
Withdrawn
Application number
EP83300106A
Other languages
English (en)
French (fr)
Other versions
EP0084420A3 (de
Inventor
Graham Leslie Maile
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.)
PA Consulting Services Ltd
Original Assignee
PA Consulting Services 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 PA Consulting Services Ltd filed Critical PA Consulting Services Ltd
Publication of EP0084420A2 publication Critical patent/EP0084420A2/de
Publication of EP0084420A3 publication Critical patent/EP0084420A3/de
Withdrawn legal-status Critical Current

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14—Reflecting surfaces; Equivalent structures
    • H01Q15/141—Apparatus or processes specially adapted for manufacturing reflecting surfaces
    • 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
    • H01Q19/19—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 comprising one main concave reflecting surface associated with an auxiliary reflecting surface

Definitions

  • This invention relates to an antenna, particularly a groundstation antenna for the reception of satellite broadcast television, business satellite communications or marine satellite communications.
  • New television (TV) services based upon the direct broadcast of signals from geostationary satellites are planned. These will become available in several countries in the next few years. Such services will be received, in a domestic context, either by a satellite groundstation devoted to a single home or, alternatively, by a community groundstation and then relayed to a number of homes.
  • the patent application describes the design of a microwave antenna which is suitable for incorporation in a domestic groundstation system.
  • Antennae suitable for satellite broadcast reception fall into two categories, namely reflector antennae and planar array antennae.
  • Reflector antennae are designed either with or without subreflectors, ie Cassegrain or front-fed respectively.
  • the feed and/or sub-reflector(s) may be either along the principal axis of the main reflector (symmetrical) or offset.
  • the simplest reflector antenna configuration a focal front-fed arrangement, generally requires a waveguide or coaxial cable to be routed from the microwave feed to a receiver. This implies a high radio frequency signal loss which is highly undesirable for satellite broadcast reception. Designs have been proposed where the receiver is suspended at the reflector focus; however the additional volume at the focus causes increased antenna aperture blockage (leading to lower efficiency, high sidelobes and depolarisation) and mechanical problems.
  • the Cassegrain configuration overcomes the signal loss problem but requires an extra reflecting surface(s) (sub-reflector(s)) and possesses a greater number of degrees of mechanical freedom, which makes alignment problematical.
  • an antenna comprises a main reflector having a parabolic reflecting surface, a sub-reflector having a hyperbolic reflecting surface and a microwave feed system aligned along the axis of the main reflector, wherein the two reflecting surfaces are accurately, permanently and non-adjustably located one with respect to the other and the two reflecting surfaces are protected from the environment surrounding the antenna.
  • the main reflector and the sub-reflector are formed by an integral body which is conveniently of a foamed synthetic plastics material.
  • the body may be moulded or cast in the desired shape, and have metal coatings over the parabolic and hyperbolic surfaces.
  • the metal coatings may be deposited on the foamed body by spraying.
  • a mounting flange is preferably attached to the parabolic surface by a suitable adhesive.
  • the sub-reflector is integral with its radome support.
  • the latter consists of a conical tube of a microwave transparent material, such as a plastics material, that extends from its base at the perimeter of the main reflector to the sub-reflector.
  • the cone is truncated in the vicinity of the main reflector's primary focus and the truncating section formed by a hyperbolic surface.
  • the inner surface of the hyperbola is coated with conducting material to form the sub-reflector.
  • a simple bayonet or snap fastener arrangement may join the main reflector to the sub- reflector/radome allowing simple assembly and servicing.
  • the main reflector has a diameter of typically 0.5 to 1.0 metres for 12 GHz TV direct broadcast, while suitable dimensions for the sub-reflector diameter and the distance from the feed to the sub-reflector are given in texts on antenna practice and theory, respectively.
  • the fastening between the main reflector and combined radome/sub-reflector should be as waterproof as practically possible to reduce deterioration of the metallic surfaces by exposure to moisture.
  • the surface of either the main reflector or the sub-reflector, or both can be modified to correct for any error caused by the presence of the radome material.
  • the antenna of Figures 1 and 2 comprises a body 1 of foamed plastics material having a metallised hyperbolic surface 2 (forming a main reflector) and a metallised parabolic surface 3.
  • the body 1 has a circular outer periphery marking the transition between the rear parabolic surface 3 and the front frusto-conical surface, in the centre of which is the hyperbolic surface 2.
  • the metallised surfaces 2 and 3 are formed by deposition of metal on appropriate regions of the external surface of the body 1.
  • the body 1 is moulded with a recess 4 to receive a feed horn carried by a mounting flange 5 which is attached to the body 1 by a suitable adhesive.
  • the foamed body 1 is simple and cheap to mould or cast in the desired shape and is light yet robust. It will be appreciated that the body 1 may be made of any shape which presents the required parabolic and hyperbolic surfaces. In particular the external surface of the body surrounding the hyperbolic surface 2 may be shaped differently from the frusto-conical configuration shown.
  • the metallised surfaces 2 and 3 are, where they reflect an incoming signal (e.g. along the single ray path A), covered by the foam meterial and therefore protected from the environment. Also, the surfaces 2 and 3 are maintained in their relative positions by virtue of being deposited on the common body 1 of foamed material.
  • the antenna of the second embodiment has a main reflector 10 which is of metal and plastics with a parabolic reflecting surface 12 having at its centre an orifice 13 surrounded by an antenna mounting flange 14.
  • the sub-reflector 15 ( Figures 5 and 6) has a central hyperbolic reflecting surface 17 integral with and surrounded by a radome 16.
  • the reflecting surfaces 12 and 17 are suitably formed by coating the concave side of the main reflector 10 and the convex side of the sub-reflector 15.
  • Figure 7 shows the main reflector 10 and the sub-reflector 15 assembled together by means of a bayonet attachment around their peripheries, projections on the periphery of the sub-reflector engaging within slots in the periphery of the main reflector.
  • the main reflector 10 and the sub-reflector 15 are in the nature of dished casing members so that the assembled antenna is a hollow shell-like structure which encloses the reflecting surfaces 12 and 17.
  • the orifice 13 accommodates a feed horn 19 which has a feed output flange 20 and which is clamped in position by a detachable split feed clamp 21.
  • the sub-reflector is in effect rigidly positioned and located with respect to the main reflector which is shaped to provide a convenient means of aligning a feed horn.
  • the antenna of each embodiment is designed so that the reflecting surfaces are well protected, and so that the antenna is adaptable to accept future commercially available microwave feeds.

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aerials With Secondary Devices (AREA)
EP83300106A 1982-01-19 1983-01-10 Antenne, besonders zum Empfang von Übertragungssatelliten Withdrawn EP0084420A3 (de)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB8201417 1982-01-19
GB8201417 1982-01-19
GB8203068 1982-02-03
GB8203068 1982-02-03

Publications (2)

Publication Number Publication Date
EP0084420A2 true EP0084420A2 (de) 1983-07-27
EP0084420A3 EP0084420A3 (de) 1983-08-03

Family

ID=26281750

Family Applications (1)

Application Number Title Priority Date Filing Date
EP83300106A Withdrawn EP0084420A3 (de) 1982-01-19 1983-01-10 Antenne, besonders zum Empfang von Übertragungssatelliten

Country Status (1)

Country Link
EP (1) EP0084420A3 (de)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0108515A1 (de) * 1982-10-11 1984-05-16 Cambridge Electronic Industries plc Parabolspiegelantenne
EP0170726A1 (de) * 1984-07-13 1986-02-12 Siemens Aktiengesellschaft Zweireflektor-Richtantenne
US4581615A (en) * 1983-02-08 1986-04-08 Levy Stanley P Double reflector antenna with integral radome reflector support
GB2168854A (en) * 1984-12-17 1986-06-25 Shamah M Antenna systems
US4977407A (en) * 1981-07-23 1990-12-11 Crane Patrick E Optical collimator
GB2221351B (en) * 1988-07-27 1991-12-04 British Telecomm Antenna
US5351060A (en) * 1991-02-25 1994-09-27 Bayne Gerald A Antenna
EP2510576A4 (de) * 2009-12-11 2014-05-14 Andrew Llc Bandklemme zur anbringung an einem reflektorantennenradom
WO2017152988A1 (en) * 2016-03-10 2017-09-14 Telefonaktiebolaget Lm Ericsson (Publ) A reflector antenna arrangement
CN112635965A (zh) * 2020-12-31 2021-04-09 西安恒达微波技术开发有限公司 一种应用于leo低轨卫星通信的双圆极化卡塞格伦天线

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3374482A (en) * 1958-09-30 1968-03-19 Navy Usa Radar dish in plastic casement
US3296685A (en) * 1962-05-31 1967-01-10 Sylvania Electric Prod Method of making dielectric foam antenna
US3430244A (en) * 1964-11-25 1969-02-25 Radiation Inc Reflector antennas
GB1100391A (en) * 1965-01-12 1968-01-24 Malifaud Pierre Receivers for directional waves
GB1531242A (en) * 1975-01-21 1978-11-08 Post Office Splash plate feed assemblies for aerials
DE2842298A1 (de) * 1978-09-28 1980-05-22 Siemens Ag Richtantenne fuer sehr kurze elektromagnetische wellen

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4977407A (en) * 1981-07-23 1990-12-11 Crane Patrick E Optical collimator
EP0108515A1 (de) * 1982-10-11 1984-05-16 Cambridge Electronic Industries plc Parabolspiegelantenne
US4581615A (en) * 1983-02-08 1986-04-08 Levy Stanley P Double reflector antenna with integral radome reflector support
EP0170726A1 (de) * 1984-07-13 1986-02-12 Siemens Aktiengesellschaft Zweireflektor-Richtantenne
GB2168854A (en) * 1984-12-17 1986-06-25 Shamah M Antenna systems
GB2168854B (en) * 1984-12-17 1989-06-14 Shamah M Antenna systems
GB2221351B (en) * 1988-07-27 1991-12-04 British Telecomm Antenna
US5351060A (en) * 1991-02-25 1994-09-27 Bayne Gerald A Antenna
EP2510576A4 (de) * 2009-12-11 2014-05-14 Andrew Llc Bandklemme zur anbringung an einem reflektorantennenradom
WO2017152988A1 (en) * 2016-03-10 2017-09-14 Telefonaktiebolaget Lm Ericsson (Publ) A reflector antenna arrangement
US10263343B2 (en) 2016-03-10 2019-04-16 Telefonaktiebolaget Lm Ericsson (Publ) Reflector antenna arrangement
CN112635965A (zh) * 2020-12-31 2021-04-09 西安恒达微波技术开发有限公司 一种应用于leo低轨卫星通信的双圆极化卡塞格伦天线
CN112635965B (zh) * 2020-12-31 2025-06-13 西安恒达微波技术开发有限公司 一种应用于leo低轨卫星通信的双圆极化卡塞格伦天线

Also Published As

Publication number Publication date
EP0084420A3 (de) 1983-08-03

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PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

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Designated state(s): CH DE FR GB IT LI SE

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Owner name: P.A. CONSULTING SERVICES LIMITED

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Withdrawal date: 19860405

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Inventor name: MAILE, GRAHAM LESLIE