JPS54143047A - Antenna unit - Google Patents
Antenna unitInfo
- Publication number
- JPS54143047A JPS54143047A JP5141078A JP5141078A JPS54143047A JP S54143047 A JPS54143047 A JP S54143047A JP 5141078 A JP5141078 A JP 5141078A JP 5141078 A JP5141078 A JP 5141078A JP S54143047 A JPS54143047 A JP S54143047A
- Authority
- JP
- Japan
- Prior art keywords
- antenna
- fitted
- motor
- stopped
- support material
- 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.)
- Pending
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
- H01Q3/04—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 one co-ordinate of the orientation
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
PURPOSE:To make it possible to realize the driving system of each antenna by an independent servo mechanism by fitting the motor, which drives the upper side antenna, and a deceleractor to the same fitting base as the motor for driving the lower side antenna, etc. CONSTITUTION:Double-structure transmission path 2 is coupled with antennas 3 and 5 by couplers 4 and 6 respectively. Antenna 3 is fitted to rotary support material 8, and support material 8 is rotated freely while being stopped by servo-motor 10, output gear 12 of decelerator 11 and gear 9 which are fitted to base 1. Antenna 5 is fitted to rotary support material 14 supported by the bearing which is fitted to support material 8, and servo-motor 16 and decelerator 17 are fitted to base 1, and output gear 18 is stopped to gear 21. The rotation of motor 16 is propagated through gears 18, 21, 22, 25 and 15 to rotate antenna 5. Gears 22 and 15 have the same number of teeth. As a result, antenna 5 maintains a stop state in case that antenna 5 is stopped to rotate antenna 3. Similarly, antenna 3 maintains a stop state in case that antenna 3 is stopped to rotate antenna 5.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5141078A JPS54143047A (en) | 1978-04-28 | 1978-04-28 | Antenna unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5141078A JPS54143047A (en) | 1978-04-28 | 1978-04-28 | Antenna unit |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS54143047A true JPS54143047A (en) | 1979-11-07 |
Family
ID=12886156
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP5141078A Pending JPS54143047A (en) | 1978-04-28 | 1978-04-28 | Antenna unit |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS54143047A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2555820A1 (en) * | 1983-11-28 | 1985-05-31 | Lerc Lab Etudes Rech Chim | Mast able to support at least two orientable devices and elements constituting this mast |
US5410316A (en) * | 1984-03-05 | 1995-04-25 | Hughes Missile Systems Company | Quick-reaction antijamming search radar |
-
1978
- 1978-04-28 JP JP5141078A patent/JPS54143047A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2555820A1 (en) * | 1983-11-28 | 1985-05-31 | Lerc Lab Etudes Rech Chim | Mast able to support at least two orientable devices and elements constituting this mast |
US5410316A (en) * | 1984-03-05 | 1995-04-25 | Hughes Missile Systems Company | Quick-reaction antijamming search radar |
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