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2 607 490

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IPC

B64C13/00(2006-01-01)

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Application

2015123326, 2015-06-18

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Start date

2015-06-18

(22)

Actual filing date

2015-06-18

(45)

Published

2017-01-10

(72)

Inventor

Zaets Viktor FedorovichAbdulin Rashid RaisovichKulabukhov Vladimir SergeevichMajorova Svetlana YurevnaKhlupnov Andrej YurevichAlimov Enver MyansurovichStitsenko Artem NikolaevichZudilin Aleksej SergeevichTuktarev Nikolaj Alekseevich

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Moskovskij Nauchno-Proizvodstvennyj Kompleks Imeni O.V. Uspenskogo Mnpk

CONTROL SYSTEM ACTUATOR Russian patent published in 2017 - IPC B64C13/00

Abstract RU 2607490 C2

FIELD: control systems.

SUBSTANCE: invention relates to aircraft airfoils control systems. Control system actuator comprises control unit and steering drive. Steering drive comprises velocity generator, rotor position sensor, two-stage reduction gear, ball-screw pair, feedback sensor, connected in certain manner. Control unit comprises secondary power supply source, consumed current sensor, receiving-transmitting unit, microcontroller, power switches control unit, power unit, microcontroller integrity checking unit, damping and braking mode actuation unit, connected in certain manner.

EFFECT: enabling expansion of electromechanical steering drive functional capabilities, increasing stability and accuracy.

1 cl, 3 dwg

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RU 2 607 490 C2

Authors

Zaets Viktor Fedorovich

Abdulin Rashid Raisovich

Kulabukhov Vladimir Sergeevich

Majorova Svetlana Yurevna

Khlupnov Andrej Yurevich

Alimov Enver Myansurovich

Stitsenko Artem Nikolaevich

Zudilin Aleksej Sergeevich

Tuktarev Nikolaj Alekseevich

Dates

2017-01-10—Published

2015-06-18—Filed