GYROCOMPASS

FIELD: physics.SUBSTANCE: gyrocompass has a housing 1 configured to rotate about its axis 2, which is mounted on a thrust bearing 3 and fixed in a vertical hollow shaft 4 of a worm gear 5, the input shaft 6 of which is linked to an actuating stepper motor 7. The housing 1 is linked to an external fr...

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Hauptverfasser: GROMOV VLADIMIR VJACHESLAVOVICH, MOSALEV SERGEJ MIKHAJLOVICH, EGOROV VIKTOR JUR'EVICH, RYBKIN IGOR' SEMENOVICH, GORBACHEV ALEKSANDR EVGEN'EVICH, KHITROV VLADIMIR ANATOL'EVICH
Format: Patent
Sprache:eng ; rus
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Zusammenfassung:FIELD: physics.SUBSTANCE: gyrocompass has a housing 1 configured to rotate about its axis 2, which is mounted on a thrust bearing 3 and fixed in a vertical hollow shaft 4 of a worm gear 5, the input shaft 6 of which is linked to an actuating stepper motor 7. The housing 1 is linked to an external frame 8 which is configured to rock on the bearings 9, fixed in the housing 1. The external frame 8 is in turn linked to an internal frame 10, which is configured to rock in a perpendicular direction on the bearings 11, fixed in the external frame 8. On the internal frame 10 on the rocking axis, there is a first vertical post 12 on which a single-axis angular velocity metre is mounted, said metre being a fibre-optic gyroscope 13 with a closed feedback loop. On the housing 1 there is a second vertical post 14 on which there is a linear stepper motor 15, the drive screw 16 of which is connected through a shaft 17 with a nut 18 to the external frame 8. On the external frame 8 there is a third vertical post 9 on which there is a similar linear stepper motor 15, the drive screw 16 of which is connected through a shaft 17 with a nut 18 to the internal frame 10. A first accelerometer 20 is mounted on the outer part of the first post 12, which is rigidly connected to the internal frame 10. A second accelerometer 22 is mounted on a supporting arm 21 located below the outer frame 8, perpendicular to the first accelerometer 20. The whole structure is mounted on a plate 23.EFFECT: high accuracy, reduced size of the measuring device designed for use in different engineering fields to measure and monitor angular velocity and angular position in inertial space.2 dwg Использование: изобретение относится к гироскопическим приборам для навигации, геодезии, измерения азимута на земной поверхности. Сущность: гирокомпас содержит корпус 1, выполненный с возможностью вращения на своей оси 2, которая установлена на упорном подшипнике 3 и зафиксирована в вертикально расположенном полом валу 4 червячного редуктора 5, входной вал 6 которого связан с приводным шаговым двигателем 7. Корпус 1 связан с внешней рамкой 8, установленной с возможностью качания в подшипниках 9, зафиксированных в корпусе 1. Внешняя рамка 8 в свою очередь связана с внутренней рамкой 10, установленной с возможностью качания в перпендикулярном направлении в подшипниках 11, зафиксированных во внешней рамке 8. На внутренней рамке 10 по оси качания размещена первая вертикальная стойка 12 с закрепленным на ней одноосным изм