GB1194535A - Improvements relating to Satellite Tracking Arrangements - Google Patents
Improvements relating to Satellite Tracking ArrangementsInfo
- Publication number
- GB1194535A GB1194535A GB34107/66A GB3410766A GB1194535A GB 1194535 A GB1194535 A GB 1194535A GB 34107/66 A GB34107/66 A GB 34107/66A GB 3410766 A GB3410766 A GB 3410766A GB 1194535 A GB1194535 A GB 1194535A
- Authority
- GB
- United Kingdom
- Prior art keywords
- movement
- axis
- dish
- mount
- tower
- 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
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/125—Means for positioning
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
Abstract
1,194,535. Aerials. PLESSEY CO. Ltd. 31 July, 1967 [29 July, 1966], No. 34107/66. Heading H4A. A geostationary satellite executes a small figure-of-eight movement relative to the earth during one revolution of the latter, due to slight earth #wobble"; such a satellite is tracked by an aerial system incorporating a dish reflector, the dish structure first being moved coarsely about an axis, then being locked against such movement, and finally the dish is moved in azimuth and elevation to track the figure-ofeight movement. In one embodiment the coarse movement is about an axis 4, Fig. 1, parallel to the earth's polar axis, mount 3 being fixed to a shaft 5 mounted for rotation in pedestal bearings 6, 7. Mount 3 may be filled with concrete to counterbalance structure 1, 2. Thrust on bearing 7 is relieved by free-running rollers, e.g. 8, which bear against semicircular surface 9 of mount 3. The drive for mount 3 is electric via a gear-box and chain drive, Fig. 6 (not shown). Locking of the mount is effected by bolting contoured plates to a concrete bollard forming part of tower structure 19, see also Fig. 6B (not shown). The fine movement of dish 1 is done by two ball screw-jacks, e.g. 23, see also Fig. 4 (not shown); a movement of about 15 degrees in two directions is arranged for. Movement of one jack or both together affords elevational movement of dish 1 about bearings, e.g. 25, having an axis perpendicular to polar axis 4; differential movement between the jacks gives azimuth displacement about an axis 27. The aerial arrangement includes a horn 35, Fig. 5, a waveguide circular polarizer 36, a diplexer 37, and a waveguide feeder 39. Two test horns 41 are added. Waveguides pass into a hollow cylinder 42 having its axis coincident with polar axis 4 and carrying a cabin 43 housing receiving apparatus; dish 1 can rotate about axis 4 without corresponding movement of cabin 43. However, the waveguide structure and receiving apparatus in the cabin rotate: hence the waveguide structure need not be modified for different coarse settings of mount 3. To accommodate cabin movement as the aerial moves in elevation whilst giving access from tower 19, Fig. 1, a concertina passageway 45 is provided. Tower 19 has several floors for housing apparatus. To cater for upward thrust on upper bearing 6 in high winds corresponding rollers may be added. In another embodiment the supporting tower comprises an open framework 51, Figs. 8, 9, incorporating a triangular upper frame 53. A "tilt" frame 54 is connected to frame 53 at points 55, 56 so that frame 54 can pivot about an axis 57 by means of a ball screw-jack 58 generally the same as in the first embodiment. A further ball screw-jack 61 is incorporated. The initial, coarse, setting of the aerial is effected by rotating tower 51 about a vertical axis: the tower is jacked up on to rollers, rotated manually and lowered off the rollers on to the ground. Adjusting reflector profile, Fig. 9.-The reflecting surface of the dish may be made from panels secured to a support framework. A panel 65 includes a support 66 of honeycomb construction to which is attached a reflecting sheet 67. Metal members, e.g. 69, are set by epoxy resin 68; a universal joint structure 70 at one end of a threaded bolt 71 is received by a bore. Annular member 72 swivels on a ball 73 and is locked in the bore of member 69 by a clip 74. The lower end of bolt 71 threads into a block 75 which can swivel about a bolt 76 passing through a flange 77 of a channel-shaped bracket 78; that bracket is attached to one of the frame members of the supporting structure. When the desired reflecting surface profile is achieved, corresponding swivel blocks and brackets are welded together.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34107/66A GB1194535A (en) | 1966-07-29 | 1966-07-29 | Improvements relating to Satellite Tracking Arrangements |
US656786A US3546704A (en) | 1966-07-29 | 1967-07-28 | Satellite tracking dish antenna with course and fine driving mechanism |
FR1550143D FR1550143A (en) | 1966-07-29 | 1967-07-28 | |
DE19671591375 DE1591375A1 (en) | 1966-07-29 | 1967-07-28 | Satellite tracking arrangement |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34107/66A GB1194535A (en) | 1966-07-29 | 1966-07-29 | Improvements relating to Satellite Tracking Arrangements |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1194535A true GB1194535A (en) | 1970-06-10 |
Family
ID=10361463
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34107/66A Expired GB1194535A (en) | 1966-07-29 | 1966-07-29 | Improvements relating to Satellite Tracking Arrangements |
Country Status (4)
Country | Link |
---|---|
US (1) | US3546704A (en) |
DE (1) | DE1591375A1 (en) |
FR (1) | FR1550143A (en) |
GB (1) | GB1194535A (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2252663B1 (en) * | 1973-11-22 | 1978-12-01 | Gueguen Michel | |
JPS6013321B2 (en) * | 1975-11-11 | 1985-04-06 | イギリス国 | satellite tracking device |
US4251819A (en) * | 1978-07-24 | 1981-02-17 | Ford Aerospace & Communications Corp. | Variable support apparatus |
FR2495734B1 (en) * | 1980-12-08 | 1985-05-31 | Framatome Sa | ADJUSTABLE SUPPORT DEVICE FOR A LARGE-DIMENSIONAL PART IN THE FORM OF A SPHERICAL CAP |
FR2505560B1 (en) * | 1981-05-08 | 1986-11-14 | Thomson Csf | ANTENNA SUPPORT |
US4654670A (en) * | 1985-02-27 | 1987-03-31 | Tracker Mounts Inc. | Tracker mount assembly for microwave dishes |
US5077560A (en) * | 1986-02-19 | 1991-12-31 | Sts Enterprises, Inc. | Automatic drive for a TVRO antenna |
US4866456A (en) * | 1986-07-16 | 1989-09-12 | Fulton Manufacturing Corporation | Horizon-to-horizon satellite antenna drive mechanism |
US5469182A (en) * | 1993-08-20 | 1995-11-21 | Orbitron Division Of Greenbriar Products, Inc. | Antenna drive assembly |
US7229024B2 (en) * | 2004-12-16 | 2007-06-12 | International Business Machines Corporation | Collimating signals |
JP4275663B2 (en) * | 2005-11-02 | 2009-06-10 | 三菱電機株式会社 | Telescope system |
US7518569B1 (en) * | 2007-09-28 | 2009-04-14 | Winegard Company | Stabilizing mechanism for a deployed reflector antenna in a mobile satellite antenna system and method |
US8941554B2 (en) | 2010-08-06 | 2015-01-27 | Pro Band International, Inc. | Anti-backlash device |
CN104832601B (en) * | 2015-04-24 | 2017-06-09 | 南京信息工程大学 | A kind of clino-axis type telescope frame driving device |
CN109002061A (en) * | 2018-06-20 | 2018-12-14 | 上海卫星工程研究所 | A kind of active face adjusting method and device for microwave antenna |
CN110242727B (en) * | 2019-05-19 | 2022-06-03 | 中国电子科技集团公司第三十九研究所 | Universal azimuth zero-crossing and limiting device for antenna |
CN112928422B (en) * | 2021-01-25 | 2023-07-07 | 中粤通建技术有限公司 | Mounting bracket for satellite communication |
CN113112844A (en) * | 2021-03-18 | 2021-07-13 | 浙江金乙昌科技股份有限公司 | Vehicle remote control system based on 5G communication and high-precision positioning and control device thereof |
CN115782767A (en) * | 2022-12-02 | 2023-03-14 | 华南农业大学 | Active vertical stable long rod holder mechanism for non-road vehicle satellite positioning receiving antenna |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2985881A (en) * | 1958-12-05 | 1961-05-23 | Holland Herman | A reflector utilizing pre-stressed elements |
US3105969A (en) * | 1960-12-23 | 1963-10-01 | North American Aviation Inc | Antenna reflector construction |
US3392398A (en) * | 1961-03-23 | 1968-07-09 | Usa | Radio telescope |
US3233475A (en) * | 1963-07-23 | 1966-02-08 | Philco Corp | Antenna structure |
US3215391A (en) * | 1964-06-29 | 1965-11-02 | Collins Radio Co | Positioning device continuous in azimuth and elevation using multiple linear drives |
US3375523A (en) * | 1964-10-16 | 1968-03-26 | Whittaker Corp | Antenna structure movable in azimuth and elevation directions |
US3401390A (en) * | 1965-05-28 | 1968-09-10 | Whittaker Corp | Adjustable positioning and support device for antenna reflector panels |
-
1966
- 1966-07-29 GB GB34107/66A patent/GB1194535A/en not_active Expired
-
1967
- 1967-07-28 US US656786A patent/US3546704A/en not_active Expired - Lifetime
- 1967-07-28 DE DE19671591375 patent/DE1591375A1/en active Pending
- 1967-07-28 FR FR1550143D patent/FR1550143A/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3546704A (en) | 1970-12-08 |
FR1550143A (en) | 1968-12-20 |
DE1591375A1 (en) | 1970-09-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |