SU1129837A1 - SYSTEM OF AUTOMATIC LONGITUDINAL BALANCING OF THE PLANE - Google Patents
SYSTEM OF AUTOMATIC LONGITUDINAL BALANCING OF THE PLANEInfo
- Publication number
- SU1129837A1 SU1129837A1 SU3546865/23A SU3546865A SU1129837A1 SU 1129837 A1 SU1129837 A1 SU 1129837A1 SU 3546865/23 A SU3546865/23 A SU 3546865/23A SU 3546865 A SU3546865 A SU 3546865A SU 1129837 A1 SU1129837 A1 SU 1129837A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- shoulder
- elevator
- gear ratio
- rocking chair
- control wiring
- Prior art date
Links
Abstract
Система автоматической продольной балансировки самолета, содержащая блок автоматической перестановки стабилизатора, связанный с приводом стабилизатора, механическую проводку управления от штурвала к рулю высоты, датчик положения руля высоты, выход которого соединен с входом блока автоматической перестановки стабилизатора, и механизм изменения передаточного отношения проводки управления, выполненный в виде качалки, одно плечо которой - плечо постоянной длины соединено со штурвалом и рулевой машиной автопилота, а на другом ее плече закреплена промежуточная качалка, одно плечо которой, образующее переменное плечо механизма изменения передаточного отношения, сочленено с проводкой управления к рулю высоты, а другое плечо соединено с приводом изменения передаточного отношения, отличающаяся тем, что, с целью улучшения эксплуатационных характеристик путем обеспечения возможности изменения диапазона балансировочных отклонений руля высоты в соответствии с режимом полета, промежуточная качалка снабжена дополнительным плечом, соединенным посредством тяги с входным звеном датчика положений руля высоты и образующим второе переменное плечо механизма изменения передаточного отношения.An automatic longitudinal balancing system for an aircraft containing a stabilizer automatic relocation unit associated with a stabilizer drive, mechanical control wiring from the handwheel to the elevator, a rudder position sensor, the output of which is connected to the stabilizer automatic permutation input, and a control wiring change mechanism, in the form of a rocking chair, one shoulder of which is a shoulder of constant length connected to the steering wheel and the autopilot steering machine, and on its other shoulder an intermediate rocking chair is fixed, one shoulder of which, forming the variable shoulder of the gear ratio changing mechanism, is articulated with the control wiring to the elevator, and the other shoulder is connected to the drive of the gear ratio change, characterized in that, in order to improve the performance characteristics by enabling the balance balancing deviations of the elevator in accordance with the flight mode, the intermediate rocking chair is equipped with an additional arm connected by means of thrust to the entrance link th position of the sensor wheel height and forming the second shoulder variable gear ratio change mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU3546865/23A SU1129837A1 (en) | 1983-01-25 | 1983-01-25 | SYSTEM OF AUTOMATIC LONGITUDINAL BALANCING OF THE PLANE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU3546865/23A SU1129837A1 (en) | 1983-01-25 | 1983-01-25 | SYSTEM OF AUTOMATIC LONGITUDINAL BALANCING OF THE PLANE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU1129837A1 true SU1129837A1 (en) | 2004-12-27 |
Family
ID=60539058
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU3546865/23A SU1129837A1 (en) | 1983-01-25 | 1983-01-25 | SYSTEM OF AUTOMATIC LONGITUDINAL BALANCING OF THE PLANE |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU1129837A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2460670C2 (en) * | 2007-03-15 | 2012-09-10 | Эрбус Оперейшнс Гмбх | Method and device to control shift of movable stabiliser on aircraft |
-
1983
- 1983-01-25 SU SU3546865/23A patent/SU1129837A1/en active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2460670C2 (en) * | 2007-03-15 | 2012-09-10 | Эрбус Оперейшнс Гмбх | Method and device to control shift of movable stabiliser on aircraft |
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