GB1084065A - - Google Patents
Info
- Publication number
- GB1084065A GB1084065A GB1084065DA GB1084065A GB 1084065 A GB1084065 A GB 1084065A GB 1084065D A GB1084065D A GB 1084065DA GB 1084065 A GB1084065 A GB 1084065A
- Authority
- GB
- United Kingdom
- Prior art keywords
- waveguide
- shaft
- lever arms
- reflector
- stand member
- 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.)
- Active
Links
Classifications
-
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/08—Means for collapsing antennas or parts thereof
- H01Q1/084—Pivotable antennas
Landscapes
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
1,084,065. Aerials. BOFORS A.B. Feb. 21, 1966 [March 2, 1965], No. 7560/66. Heading H4A. [Also in Division H1] An aerial system, suitable for the fire control radar of a fighting vehicle, comprises a dish reflector 4 which is pivoted on a horizontal shaft (10), Fig. 2 (not shown), carried in an upper stand member 6 resting on a lower stand member 5, the whole being rotatable about a vertical axis and mounted upon a base such as a gun turret 2. The two stand members are coupled by means of a horizontal shaft (8) so that the upper member 6 carrying the aerial may be swung down to a transport position beside the lower member 5 as is shown in dotted lines in Fig. 1. The primary radiator for the reflector 4 is fed from equipment within the turret 2 by a waveguide (31), Fig. 3 (not shown) which is coupled through a rotating waveguide joint (30) to the lower end of a waveguide (29) fixed to the lower stand member 5 and extending along or near its vertical axis of rotation, the upper end of the said waveguide being bent and inserted through the shaft (8) to a rotating waveguide joint (32). From this joint, the feed is continued through a waveguide (33), fixed to the upper stand member 6, to a rotating waveguide joint (34), from which another waveguide passes through the shaft (10) to the said primary radiator. Rotation of the aerial system in azimuth is effected by a motor (25) inside the turret 2 which is connected by gearing (26), (27), (28) to the lower stand member 5. An elevation drive motor (24), also inside the turret 2, is connected by gears (23) to a horizontal shaft (22) carrying a fork-shaped lever arm (21), motion from which is transmitted by a vertical tubular rod (15), disposed around the waveguide (29), to a similar fork-shaped lever arm (18) carried on a horizontal shaft (14), journalled in the lower stand member 5. There are heads (16), (19) at the ends of the tubular rod (15) having horizontal grooves (17), (20) to receive pins on the ends of the lever arms (18), (21), a rotational joint being provided between one head and the tubular arm. The pins on the ends of the lever arms may each be provided with two rollers, such as (37), (38), Fig. 4 (not shown), which bear on individual tracks (35), (36) formed in the co-operating horizontal groove (17) of the head (16) concerned, to reduce friction and backlash. The motion of the shaft (14) is communicated to the reflector 4 by means of lever arms (13), Fig. 2 (not shown), connecting rods (12), and lever arms (11) attached to the said reflector. The effective radius of the lever arms (13) is made substantially equal to the distance between the axes of the shafts (8) and (14) and when the reflector 4 is to be stowed it is first tilted back so that the pivot joints between the lever arms (13) and the connecting rods (12) lie on or close to the axis of the shaft (8).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE270465 | 1965-03-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1084065A true GB1084065A (en) |
Family
ID=20260500
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1084065D Active GB1084065A (en) | 1965-03-02 |
Country Status (9)
Country | Link |
---|---|
US (1) | US3412404A (en) |
AT (1) | AT270757B (en) |
BE (1) | BE677264A (en) |
CH (1) | CH458456A (en) |
DE (1) | DE1491903C2 (en) |
DK (1) | DK113223B (en) |
ES (1) | ES323703A1 (en) |
GB (1) | GB1084065A (en) |
NL (1) | NL6602705A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2165999A (en) * | 1984-02-09 | 1986-04-23 | Gen Electric Plc | A transportable antenna |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3665477A (en) * | 1969-01-08 | 1972-05-23 | Barker Mfg Co Inc | Elevatable and foldable antenna |
US3739387A (en) * | 1969-01-08 | 1973-06-12 | Barker Mfg Co Inc | Dual purpose antenna control |
GB1347276A (en) * | 1971-07-07 | 1974-02-27 | Westland Aircraft Ltd | Helicopters |
FR2522883A1 (en) * | 1982-03-05 | 1983-09-09 | Thomson Csf | SWIVEL JOINT FOR MICROWAVE WAVEGUIDES |
US4491388A (en) * | 1982-05-28 | 1985-01-01 | Wood Douglas E | Support carriage for a solar concentrator |
US4691207A (en) * | 1984-09-04 | 1987-09-01 | Nissho Iwai American Corporation | Antenna positioning apparatus |
WO1989000772A1 (en) * | 1985-08-07 | 1989-01-26 | Radov Mitchell C | Satellite earth station |
US4663633A (en) * | 1985-10-15 | 1987-05-05 | Wilson John E | Vehicle mounted satellite antenna system |
CA1261653A (en) * | 1986-10-23 | 1989-09-26 | John N. Leavitt | Steerable windowed enclosures |
US4811026A (en) * | 1987-11-16 | 1989-03-07 | Bissett William R | Mobile satellite receiving antenna especially for recreation vehicle |
US5528250A (en) * | 1992-11-18 | 1996-06-18 | Winegard Company | Deployable satellite antenna for use on vehicles |
US5337062A (en) * | 1992-11-18 | 1994-08-09 | Winegard Company | Deployable satellite antenna for use on vehicles |
US5414435A (en) * | 1994-03-08 | 1995-05-09 | Wolf Coach, Inc. | Space frame satellite dish and aimer support |
US5554998A (en) * | 1995-03-31 | 1996-09-10 | Winegard Company | Deployable satellite antenna for use on vehicles |
US5961092A (en) * | 1997-08-28 | 1999-10-05 | Satellite Mobile Systems, Inc. | Vehicle with a satellite dish mounting mechanism for deployably mounting a satellite dish to the vehicle and method for deployably mounting a satellite dish to a vehicle |
US7397435B2 (en) * | 2004-08-13 | 2008-07-08 | Winegard Company | Quick release stowage system for transporting mobile satellite antennas |
US7230581B2 (en) * | 2004-08-13 | 2007-06-12 | Winegard Company | Nomadic storable satellite antenna system |
US7791553B2 (en) * | 2007-04-13 | 2010-09-07 | Winegard Company | High wind elevation mechanism for a satellite antenna system |
DE102009042162B3 (en) * | 2009-09-10 | 2011-05-19 | Apexsat Gmbh | Holding device for fastening satellite antenna of satellite receiving device at e.g. facade of building, has transverse bar with end pivotably connected with actuator, and another transverse bar longer than former transverse bar |
US9310479B2 (en) * | 2012-01-20 | 2016-04-12 | Enterprise Electronics Corporation | Transportable X-band radar having antenna mounted electronics |
CN104081135B (en) | 2012-01-22 | 2016-08-31 | 黑利福卡斯有限公司 | Solar concentrating system |
US20130341294A1 (en) * | 2012-05-02 | 2013-12-26 | Gossamer Space Frames | Brake system and method for a rotating frame in a solar power generation system |
JP6061646B2 (en) * | 2012-11-27 | 2017-01-18 | 古野電気株式会社 | Radar antenna |
JP6014473B2 (en) * | 2012-11-27 | 2016-10-25 | 古野電気株式会社 | Radar antenna and method for manufacturing radar antenna |
EP3235055B1 (en) * | 2014-12-19 | 2020-05-27 | Saab Ab | Pivot axle arrangement |
PL70964Y1 (en) * | 2017-07-11 | 2022-09-12 | Pit Radwar Spolka Akcyjna | Stabilizing support arm |
CA3051985C (en) * | 2018-08-24 | 2022-08-09 | Fuel Automation Station, LLC | Mobile distribution station having satellite dish |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3286265A (en) * | 1962-11-12 | 1966-11-15 | Ca Nat Research Council | Scanning reflector on stabilized platform having a stowed position |
-
0
- GB GB1084065D patent/GB1084065A/en active Active
-
1966
- 1966-02-22 AT AT161166A patent/AT270757B/en active
- 1966-02-22 CH CH251966A patent/CH458456A/en unknown
- 1966-02-24 US US529869A patent/US3412404A/en not_active Expired - Lifetime
- 1966-02-24 DE DE1491903A patent/DE1491903C2/en not_active Expired
- 1966-03-01 ES ES0323703A patent/ES323703A1/en not_active Expired
- 1966-03-02 DK DK108666AA patent/DK113223B/en unknown
- 1966-03-02 NL NL6602705A patent/NL6602705A/xx unknown
- 1966-03-02 BE BE677264D patent/BE677264A/xx unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2165999A (en) * | 1984-02-09 | 1986-04-23 | Gen Electric Plc | A transportable antenna |
Also Published As
Publication number | Publication date |
---|---|
DE1491903C2 (en) | 1975-01-23 |
ES323703A1 (en) | 1967-02-01 |
DK113223B (en) | 1969-03-03 |
US3412404A (en) | 1968-11-19 |
CH458456A (en) | 1968-06-30 |
NL6602705A (en) | 1966-09-05 |
AT270757B (en) | 1969-05-12 |
DE1491903B1 (en) | 1970-05-27 |
BE677264A (en) | 1966-08-01 |
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