SU1415863A1 - AVIHORIZONT - Google Patents
AVIHORIZONTInfo
- Publication number
- SU1415863A1 SU1415863A1 SU4093508/22A SU4093508A SU1415863A1 SU 1415863 A1 SU1415863 A1 SU 1415863A1 SU 4093508/22 A SU4093508/22 A SU 4093508/22A SU 4093508 A SU4093508 A SU 4093508A SU 1415863 A1 SU1415863 A1 SU 1415863A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- rotor
- axis
- creating
- movable elements
- bearings
- Prior art date
Links
Landscapes
- A Measuring Device Byusing Mechanical Method (AREA)
Abstract
Авиагоризонт, содержащий ротор, установленный на шарикоподшипниках в кардановом подвесе, устройство для создания нижней маятниковости при невращающемся роторе с расположенными в полостях ротора подвижными элементами, систему индикации, отличающийся тем, что, с целью улучшения габаритно-массовых характеристик авиагоризонта при сохранении надежности в обесточенном режиме, подвижные элементы устройства для создания нижней маятниковости выполнены в виде Г-образных рычагов, каждый из которых закреплен в роторе на своей оси с возможностью поворота в плоскости, проходящей через ось вращения ротора, при этом горизонтальный конец плеча каждого Г-образного рычага направлен к центру ротора и кинематически связан с наружным кольцом дополнительно введенного радиально-упорного шарикоподшипника, жестко закрепленного на валу ротора, причем в качестве опор ротора использованы шарикоподшипники с наружным или внутренним кольцом типа гладкая втулка.The artificial horizon contains a rotor mounted on ball bearings in a gimbal suspension, a device for creating lower pendulum with a non-rotating rotor with movable elements located in the rotor cavities, an indication system, characterized in that, in order to improve the overall mass characteristics of the horizon while maintaining reliability in de-energized The movable elements of the device for creating the lower pendulum are made in the form of L-shaped levers, each of which is fixed in the rotor on its own axis with the possibility rotation in the plane passing through the axis of rotation of the rotor, while the horizontal end of the shoulder of each L-shaped lever is directed to the center of the rotor and is kinematically connected with the outer ring of the additionally inserted angular contact ball bearing rigidly mounted on the rotor shaft, and used as bearings of the rotor Ball bearings with outer or inner ring type smooth sleeve.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4093508/22A SU1415863A1 (en) | 1986-07-09 | 1986-07-09 | AVIHORIZONT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4093508/22A SU1415863A1 (en) | 1986-07-09 | 1986-07-09 | AVIHORIZONT |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1415863A1 true SU1415863A1 (en) | 2005-08-10 |
Family
ID=60535810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4093508/22A SU1415863A1 (en) | 1986-07-09 | 1986-07-09 | AVIHORIZONT |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1415863A1 (en) |
-
1986
- 1986-07-09 SU SU4093508/22A patent/SU1415863A1/en active
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