ELECTROHYDRAULIC SERVO UNIT OF FLYING VEHICLE WING LEADING EDGE CONTROL SYSTEM

FIELD: aeronautical engineering.SUBSTANCE: proposed servo unit has body, electrohydraulic booster connected with pressure line of hydraulic system through filter and electrohydraulic valve for cutting-in hydraulic supply system; it is also connected with cavities of hydraulic cylinder connected with...

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Bibliographische Detailangaben
Hauptverfasser:	Rostokin Konstantin Petrovich, Parmenov Jurij Alekseevich, Shapkov Vjacheslav Ivanovich, Kuprijanov Fedor Fedorovich, Popov Aleksandr Danilovich
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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