FIELD: aeronautical engineering.
SUBSTANCE: proposed servo unit has pump station, hydraulic mixer, hydraulic compensator and actuating cylinder with rod, locking mechanism and cross-feed valve. Locking mechanism is made in form of spring-loaded plunger with longitudinal slot where two rollers are fitted; these rollers are engageable with bevels available on rod.
EFFECT: enhanced reliability.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
SELF-CONTAINED SERVO UNIT | 1973 |
|
SU1840184A1 |
ELECTROHYDRAULIC DRIVE FOR FLIGHT VEHICLE CONTROL SYSTEMS | 1971 |
|
SU1840664A1 |
ELECTRO-HYDROSTATIC OPERATING MECHANISM INCORPORATING RESETTING HYDRAULIC COMPENSATOR | 2005 |
|
RU2289878C1 |
ELECTROHYDROSTATIC DRIVE UNIT HAVING ELECTROHYDRAULIC REVERSE VALVE AND RESET HYDRAULIC COMPENSATOR | 2005 |
|
RU2296892C1 |
FLYING VEHICLE ACTUATOR | 1976 |
|
SU1840183A1 |
MULTI-CHANNEL SERVO UNIT | 1972 |
|
SU1840186A1 |
FLYING VEHICLE CONTROL ACTUATOR | 1977 |
|
SU1840180A1 |
ELECTROHYDRAULIC SERVO UNIT AT MECHANICAL LIMIT OF ACTUATING ROD TRAVEL | 1976 |
|
SU1840182A1 |
ELECTRO-HYDRAULIC ACTUATOR | 2001 |
|
RU2207300C2 |
ELECTROHYDROSTATIC DRIVE | 2005 |
|
RU2289189C1 |
Authors
Dates
2006-06-27—Published
1973-04-06—Filed