SU1338264A1 - DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER - Google Patents
DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZERInfo
- Publication number
- SU1338264A1 SU1338264A1 SU3962577/23A SU3962577A SU1338264A1 SU 1338264 A1 SU1338264 A1 SU 1338264A1 SU 3962577/23 A SU3962577/23 A SU 3962577/23A SU 3962577 A SU3962577 A SU 3962577A SU 1338264 A1 SU1338264 A1 SU 1338264A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- axes
- sensors
- rocking chair
- main
- control system
- Prior art date
Links
Abstract
1. Устройство сигнализации положения стабилизатора летательного аппарата, содержащее основную качалку, соединенную с осями датчиков системы управления, закрепленных на кронштейне, одно плечо которой кинематически связано со стабилизатором, а другое через тягу и дополнительную качалку - с другими датчиками системы управления, закрепленными на этом же кронштейне, отличающееся тем, что, с целью уменьшения габаритов и массы, а также повышения технологичности обслуживания, кронштейн выполнен П-образным, а датчики установлены на его параллельных сторонах попарно, а также соосно между собой и осями вращения качалок, размещенных между ними, причем основная качалка снабжена механизмами регулировки углов установки осей датчиков, размещенными по внутренней полости основной качалки и взаимодействующими с осями соответствующих датчиков.2. Устройство по п.1, отличающееся тем, что механизмы регулировки углов установки осей датчиков системы управления выполнены в виде двух независимых червячных передач, расположенных вдоль оси вращения основной качалки и направленных, перпендикулярно к ней, при этом оси червячных колес связаны с осью основной качалки посредством фрикционной передачи.1. The device for signaling the position of the stabilizer of the aircraft, containing the main rocking chair connected to the axes of the sensors of the control system mounted on a bracket, one arm of which is kinematically connected to the stabilizer, and the other through traction and an additional rocking chair to other sensors of the control system attached to the same bracket, characterized in that, in order to reduce dimensions and weight, as well as improve the manufacturability of the service, the bracket is U-shaped, and the sensors are installed on its parallel The two sides are in pairs, as well as coaxially between themselves and the axes of rotation of the rockers placed between them, the main rocker being equipped with mechanisms for adjusting the angles of the sensor axes located along the internal cavity of the main rocker and interacting with the axes of the respective sensors.2. The device according to claim 1, characterized in that the mechanisms for adjusting the angles of installation of the axes of the sensors of the control system are made in the form of two independent worm gears located along the axis of rotation of the main rocking chair and directed perpendicular to it, while the axes of the worm wheels are connected to the axis of the main rocking chair by friction transmission.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3962577/23A SU1338264A1 (en) | 1985-10-14 | 1985-10-14 | DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3962577/23A SU1338264A1 (en) | 1985-10-14 | 1985-10-14 | DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1338264A1 true SU1338264A1 (en) | 2005-02-20 |
Family
ID=60534884
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3962577/23A SU1338264A1 (en) | 1985-10-14 | 1985-10-14 | DEVICE FOR SIGNALING THE POSITION OF THE AIRCRAFT STABILIZER |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1338264A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2673755C1 (en) * | 2015-10-21 | 2018-11-29 | Сафран Электроникс Энд Дифенс | Aircraft flight control device |
-
1985
- 1985-10-14 SU SU3962577/23A patent/SU1338264A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2673755C1 (en) * | 2015-10-21 | 2018-11-29 | Сафран Электроникс Энд Дифенс | Aircraft flight control device |
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