SU1415863A1 - AVIHORIZONT - Google Patents

AVIHORIZONT

Info

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
Application number
SU4093508/22A
Other languages
Russian (ru)
Inventor
В.М. Елькин
Original Assignee
В.М. Елькин
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by В.М. Елькин filed Critical В.М. Елькин
Priority to SU4093508/22A priority Critical patent/SU1415863A1/en
Application granted granted Critical
Publication of SU1415863A1 publication Critical patent/SU1415863A1/en

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  • 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.

SU4093508/22A 1986-07-09 1986-07-09 AVIHORIZONT SU1415863A1 (en)

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)

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