GB1378114A - Antenna system - Google Patents
Antenna systemInfo
- Publication number
- GB1378114A GB1378114A GB1126473A GB1126473A GB1378114A GB 1378114 A GB1378114 A GB 1378114A GB 1126473 A GB1126473 A GB 1126473A GB 1126473 A GB1126473 A GB 1126473A GB 1378114 A GB1378114 A GB 1378114A
- Authority
- GB
- United Kingdom
- Prior art keywords
- axis
- reflector
- concave
- reflectors
- plane
- 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
Links
Classifications
-
- 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
- H01Q19/191—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 wherein the primary active element uses one or more deflecting surfaces, e.g. beam waveguide feeds
Landscapes
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
1378114 Aerials NIPPON ELECTRIC CO Ltd 8 March 1973 [8 March 1972] 11264/73 Heading H4A A microwave aerial system comprises an aerial portion I, a feed portion II, and a fixed portion III. The portion I is rotatable relative to the portion II about an axis El (e.g. an elevation axis) and the portions I and II together are rotatable relative to the portion III about an axis Az (e.g. an azimuth axis). The portion I contains a plane reflector B located on the axis El, and the portion II contains a first concave reflector A located on the axis El, a plane reflector B<SP>1</SP> located on the axis Az, and a second concave reflector A<SP>1</SP>. The disposition of the reflectors is such that radiation from a focal point Q of the portion I is directed via the plane reflector B along the axis El to the concave reflector A, then via the concave reflector A<SP>1</SP> to the plane reflector B<SP>1</SP>, and then along the axis Az to a focal point Q<SP>1</SP> of the portion III, and' vice versa. The arrangement of the concave reflectors A, A<SP>1</SP> is such that the mode of transmission of the radiation at the plane reflectors B, B<SP>1</SP> is the same, so minimizing side lobe effects. In one embodiment, the portion I comprises a hyperboloidal sub-reflector 2, Fig. 3, with one focus at the point Q, and a paraboloidal main reflector 3. The portion III comprises communications equipment 5 and an associated feed horn 1, with phase centre at the point Q<SP>1</SP>. The concave reflectors A, A<SP>1</SP> in the portion III are offset from the axis Az, are of paraboloidal form, and are mirror images of each other. In another embodiment, the concave reflectors A, A<SP>1</SP> are parts of ellipsoids of revolution having a common focus F, Fig. 6.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP47023161A JPS4891950A (en) | 1972-03-08 | 1972-03-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1378114A true GB1378114A (en) | 1974-12-18 |
Family
ID=12102869
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1126473A Expired GB1378114A (en) | 1972-03-08 | 1973-03-08 | Antenna system |
Country Status (7)
Country | Link |
---|---|
US (1) | US3845483A (en) |
JP (1) | JPS4891950A (en) |
CA (1) | CA984505A (en) |
DE (1) | DE2311439C2 (en) |
FR (1) | FR2175145B1 (en) |
GB (1) | GB1378114A (en) |
IT (1) | IT981187B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3631735A1 (en) * | 1986-09-18 | 1988-04-07 | Messerschmitt Boelkow Blohm | MESSAGE TRANSFER DEVICE FOR SPACE VEHICLES |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2345222C3 (en) * | 1973-09-07 | 1981-05-14 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Reflector antenna |
FR2265190B1 (en) * | 1974-03-19 | 1978-01-06 | Thomson Csf | |
JPS52140254A (en) * | 1976-05-18 | 1977-11-22 | Mitsubishi Electric Corp | Antenna unit |
FR2429505A1 (en) * | 1978-06-20 | 1980-01-18 | Thomson Csf | PERISCOPIC FEEDING SYSTEM FOR TWO-RANGE ANTENNA |
JPS5744302A (en) * | 1980-08-28 | 1982-03-12 | Mitsubishi Electric Corp | Antenna device |
DE3144466A1 (en) * | 1981-11-09 | 1983-07-07 | AEG-Telefunken Nachrichtentechnik GmbH, 7150 Backnang | Controllable antenna arrangement |
JPS58139503A (en) * | 1982-02-15 | 1983-08-18 | Kokusai Denshin Denwa Co Ltd <Kdd> | Beam feeding device |
JPS5911007A (en) * | 1982-07-12 | 1984-01-20 | Nec Corp | Antenna device in common use as two-frequency band |
US4491848A (en) * | 1982-08-30 | 1985-01-01 | At&T Bell Laboratories | Substantially frequency-independent aberration correcting antenna arrangement |
DE3330284A1 (en) * | 1983-08-22 | 1985-03-21 | Siemens AG, 1000 Berlin und 8000 München | Satellite-radio ground-station antenna arrangement operating on the Cassegrain principle |
JPS6089104A (en) * | 1983-09-22 | 1985-05-20 | ブリテイツシユ・エアロスペイス・パブリツク・リミテツド・カンパニー | Antenna unit |
US4668955A (en) * | 1983-11-14 | 1987-05-26 | Ford Aerospace & Communications Corporation | Plural reflector antenna with relatively moveable reflectors |
US4692771A (en) * | 1985-03-28 | 1987-09-08 | Satellite Technology Services, Inc. | Antenna dish reflector with integral azimuth track |
US4716416A (en) * | 1985-03-28 | 1987-12-29 | Satellite Technology Services, Inc. | Antenna dish reflector with integral declination adjustment |
US5003321A (en) * | 1985-09-09 | 1991-03-26 | Sts Enterprises, Inc. | Dual frequency feed |
FR2589284B1 (en) * | 1985-10-28 | 1988-05-20 | Alcatel Espace | MULTI-REFLECTOR ANTENNA RADIATING A STEERABLE BEAM WITH A LARGE TRAVEL |
FR2592742B1 (en) * | 1986-01-09 | 1988-03-18 | Alcatel Espace | DEVICE FOR ORIENTING AN ANTENNA FOR PERFORMING A SCANNING ACCORDING TO TWO ORTHOGONAL DIRECTIONS |
US5673057A (en) * | 1995-11-08 | 1997-09-30 | Trw Inc. | Three axis beam waveguide antenna |
GB2336341A (en) * | 1997-02-14 | 1999-10-20 | Easat Antennas Ltd | Method and apparatus for the remote clearance of explosive devices |
GB9703077D0 (en) * | 1997-02-14 | 1997-04-02 | Easat Antennas Ltd | Method and apparatus for the remote clearance of explosive devices |
US6061033A (en) * | 1997-11-06 | 2000-05-09 | Raytheon Company | Magnified beam waveguide antenna system for low gain feeds |
US6225961B1 (en) | 1999-07-27 | 2001-05-01 | Prc Inc. | Beam waveguide antenna with independently steerable antenna beams and method of compensating for planetary aberration in antenna beam tracking of spacecraft |
US7129903B2 (en) * | 2001-09-27 | 2006-10-31 | The Boeing Company | Method and apparatus for mounting a rotating reflector antenna to minimize swept arc |
US7042409B2 (en) * | 2001-09-27 | 2006-05-09 | The Boeing Company | Method and apparatus for mounting a rotating reflector antenna to minimize swept arc |
US7030831B2 (en) * | 2002-11-14 | 2006-04-18 | Wifi-Plus, Inc. | Multi-polarized feeds for dish antennas |
US7556389B2 (en) * | 2006-03-30 | 2009-07-07 | Raytheon Company | Pointable optical system with coude optics having a short on-gimbal path length |
RU2449436C1 (en) * | 2010-10-04 | 2012-04-27 | Открытое акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнева" | Deployable large-size double-mirror antenna of spacecraft |
EP2996197B1 (en) * | 2014-09-10 | 2021-10-20 | MacDonald, Dettwiler and Associates Corporation | Wide scan steerable antenna |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1516826A1 (en) * | 1966-04-26 | 1969-08-14 | Siemens Ag | Directional antenna arrangement for very short electromagnetic waves |
JPS5211872B2 (en) * | 1971-11-17 | 1977-04-02 |
-
1972
- 1972-03-08 JP JP47023161A patent/JPS4891950A/ja active Pending
-
1973
- 1973-03-01 US US00336957A patent/US3845483A/en not_active Expired - Lifetime
- 1973-03-07 IT IT21292/73A patent/IT981187B/en active
- 1973-03-07 FR FR7308168A patent/FR2175145B1/fr not_active Expired
- 1973-03-07 CA CA165,418A patent/CA984505A/en not_active Expired
- 1973-03-08 DE DE2311439A patent/DE2311439C2/en not_active Expired
- 1973-03-08 GB GB1126473A patent/GB1378114A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3631735A1 (en) * | 1986-09-18 | 1988-04-07 | Messerschmitt Boelkow Blohm | MESSAGE TRANSFER DEVICE FOR SPACE VEHICLES |
Also Published As
Publication number | Publication date |
---|---|
JPS4891950A (en) | 1973-11-29 |
IT981187B (en) | 1974-10-10 |
DE2311439A1 (en) | 1973-10-04 |
DE2311439C2 (en) | 1982-10-14 |
FR2175145B1 (en) | 1982-05-07 |
US3845483A (en) | 1974-10-29 |
CA984505A (en) | 1976-02-24 |
FR2175145A1 (en) | 1973-10-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PE20 | Patent expired after termination of 20 years |
Effective date: 19930307 |