SU1707664A1 - For satellite communication - Google Patents
For satellite communication Download PDFInfo
- Publication number
- SU1707664A1 SU1707664A1 SU894756593A SU4756593A SU1707664A1 SU 1707664 A1 SU1707664 A1 SU 1707664A1 SU 894756593 A SU894756593 A SU 894756593A SU 4756593 A SU4756593 A SU 4756593A SU 1707664 A1 SU1707664 A1 SU 1707664A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- axis
- hinges
- linear
- reflector
- opu
- Prior art date
Links
Landscapes
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
Изобретение относитс к антенной технике и может использоватьс в антеннах спутниковой телесв зи. Цель изобретени состоит Б пор.ыи;ении. точности наведени . Антенна спутниковой св зи состоит из установленных нз основании 1 рефлектора 2, контррефлектора 15, опорно-поворотного устройства (ОПУ) 3 с часовой осью 4 и угло- местной осью, образованной шарнирами 7. осью скоплени , образованной шарнирами 8 креплени рефлектора 2 к ОПУ 3 и шарнир- но установленными линейными приводами наведени 9,10, 11. Один из шарниров угло- местной оси 5 соединен с шарниром 8 оси склонени посредством линейного привода нзэедени 10 по часовой оси 4. Примем ось склонени , угломестна ось и линейный привод наведени 10 лежат в одной плоскости , перпендикул рной часовой оси 4. В процессе работы линейный привод наведени 10 сохран ет свое положение в плоскости . Шарниры его соединений с угломестной осью и рефлектором 2 выполнены одноосными. 2 ил. tThe invention relates to antenna technology and can be used in satellite TV antennas. The purpose of the invention consists of Porosi; hover accuracy. The satellite communication antenna consists of the installed reflector base 1 of the reflector 2, counter reflector 15, a turntable (OPU) 3 with a clock axis 4 and an angular axis formed by the hinges 7. an axis of accumulation formed by the hinges 8 of the reflector 2 to the OPU 3 and pivotally mounted linear hover drives 9, 10, 11. One of the hinges of the angular axis 5 is connected to the hinge 8 of the inclination axis by means of a linear drive 10 ning 10 in a clockwise axis 4. Let us assume an inclination axis, an elevation axis and a linear hover drive 10 at one plane perpendicular to the clock axis 4. During operation, the linear pointing drive 10 maintains its position in the plane. The hinges of its connections with the elevation axis and the reflector 2 are made uniaxial. 2 Il. t
Description
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Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU894756593A SU1707664A1 (en) | 1989-11-04 | 1989-11-04 | For satellite communication |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU894756593A SU1707664A1 (en) | 1989-11-04 | 1989-11-04 | For satellite communication |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1707664A1 true SU1707664A1 (en) | 1992-01-23 |
Family
ID=21478278
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU894756593A SU1707664A1 (en) | 1989-11-04 | 1989-11-04 | For satellite communication |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1707664A1 (en) |
-
1989
- 1989-11-04 SU SU894756593A patent/SU1707664A1/en active
Non-Patent Citations (1)
Title |
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Патент US Nk 3945015. кл. НОЮ 3/08, 1976. Патент US te 4232323. wi. Н 01 Q 3/08, 1980. * |
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