FIELD: aviation. SUBSTANCE: servo unit has electrohydraulic actuator 5 in each subchannel 1, actuating hydraulic cylinder 8 with hollow rod 9 which is brought in communication with delivery line and two pistons 10 and 11 located inside it, feedback transmitter 14, electrohydraulic valve 7, cross-feed valve 6, failure indication microswitch 13, delivery and return lines; piston 11 is hollow and has piston 10 inside it forming working chamber between pistons. Hollow rod 9 is provided with projection engageable with hollow piston 11 which is provided with shoulder engageable with piston 10 connected with bell crank by means of articulated rod. EFFECT: improved static and dynamic characteristics through avoidance of backlash. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTI-CHANNEL SERVO UNIT | 1972 |
|
SU1840186A1 |
MULTI-CHANNEL ACTUATOR FOR FLYING VEHICLE CONTROL UNIT | 1986 |
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MULTI-CHANNEL ACTUATOR | 1976 |
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MULTI-CHANNEL SERVO UNIT FOR FLYING VEHICLE CONTROL SYSTEM | 1979 |
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SU1839991A1 |
ELECTROHYDRAULIC SERVO UNIT OF FLYING VEHICLE WING LEADING EDGE CONTROL SYSTEM | 1978 |
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SU1840177A1 |
CORRECTING HYDRAULIC UNIT OF MULTI-CHANNEL DRIVE | 1980 |
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ELECTROHYDROMECHANICAL DRIVE | 2000 |
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SELF-CONTAINED HYDRAULIC DRIVE- ELECTROHYDRAULIC SERVO UNIT MODULE | 2004 |
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RU2261195C1 |
0 |
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SU220056A1 | |
PUMP-AND-ACCUMULATOR HYDRAULIC DRIVE | 2000 |
|
RU2184281C2 |
Authors
Dates
1995-11-10—Published
1977-07-28—Filed