FIELD: aeronautical engineering.
SUBSTANCE: each sub-channel of proposed servo unit is provided with electrohydraulic valve for cutting-in pressure, electrohydraulic booster, actuating hydraulic cylinder whose piston is rigidly connected with pistons of actuating hydraulic cylinders of other sub-channels and its cavities are hydraulically connected with cross-feed valve and unit for monitoring and disconnecting defective sub-channel; each sub-channel is also provided with over-power valve and feedback sensor. Over-power valve is made in form of hydraulic cylinder with piston and double-sided spring-loaded rod whose cavities are hydraulically connected with cavities of actuating cylinder. Hydraulic cylinder is provided with ports forming slots together with flats of piston in its extreme positions; these slots connect the cavities of hydraulic cylinder. Mounted on hydraulic cylinder body is microswitch engageable with hydraulic cylinder rod; it is used for closing the electric circuit of pressure cut-in valve.
EFFECT: enhanced reliability.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTI-CHANNEL ACTUATOR FOR FLYING VEHICLE CONTROL UNIT | 1986 |
|
SU1839992A1 |
THREE-CHANNEL ELECTROHYDRAULIC SERVO UNIT | 1977 |
|
SU1826414A1 |
MULTI-CHANNEL SERVO UNIT FOR FLYING VEHICLE CONTROL SYSTEM | 1979 |
|
SU1839991A1 |
MULTI-CHANNEL ACTUATOR | 1976 |
|
SU1839995A1 |
CORRECTING HYDRAULIC UNIT OF MULTI-CHANNEL DRIVE | 1980 |
|
SU1839882A1 |
ELECTROHYDRAULIC SERVO UNIT OF FLYING VEHICLE WING LEADING EDGE CONTROL SYSTEM | 1978 |
|
SU1840177A1 |
ELECTROHYDRAULIC MULTICHANNEL STEERING GEAR | 2001 |
|
RU2211962C2 |
ACTUATOR UNIT FOR FLYING VEHICLE CONTROL SYSTEMS | 1986 |
|
SU1840018A1 |
0 |
|
SU244837A1 | |
ELECTROHYDRAULIC SERVO DRIVE | 2004 |
|
RU2262467C1 |
Authors
Dates
2006-06-27—Published
1972-04-06—Filed