FIELD: aeronautical engineering.
SUBSTANCE: proposed actuator has several control channels with electro-hydraulic amplifier, cut-in valve, auxiliary hydraulic cylinder, pressure drop correction unit, feedback sensor and main hydraulic cylinder whose piston is rigidly connected with pistons of similar actuating cylinders of other sub-channels. Each sub-channel is provided with spool valve hydraulically connecting the cavities of auxiliary hydraulic cylinder with respective cavities of main hydraulic cylinder at arising of design pressure in its cavities.
EFFECT: improved static and dynamic characteristics.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTI-CHANNEL ACTUATOR FOR FLYING VEHICLE CONTROL UNIT | 1986 |
|
SU1839992A1 |
MULTI-CHANNEL SERVO UNIT | 1972 |
|
SU1840186A1 |
MULTI-CHANNEL SERVO UNIT FOR FLYING VEHICLE CONTROL SYSTEM | 1979 |
|
SU1839991A1 |
THREE-CHANNEL ELECTROHYDRAULIC SERVO UNIT | 1977 |
|
SU1826414A1 |
ACTUATOR UNIT FOR FLYING VEHICLE CONTROL SYSTEMS | 1986 |
|
SU1840018A1 |
ELECTROHYDRAULIC MULTICHANNEL STEERING GEAR | 2001 |
|
RU2211962C2 |
CORRECTING HYDRAULIC UNIT OF MULTI-CHANNEL DRIVE | 1980 |
|
SU1839882A1 |
ELECTROHYDRAULIC SERVO DRIVE | 2004 |
|
RU2262467C1 |
STANDBY ELECTROHYDRAULIC DRIVE UNIT | 2000 |
|
RU2190129C2 |
ELECTROHYDRAULIC POWER DRIVE | 1987 |
|
SU1432936A1 |
Authors
Dates
2006-06-20—Published
1976-05-20—Filed