FIELD: flying vehicle equipment.
SUBSTANCE: proposed unit has feedback electric sensor, piston with two-sided rod, hydraulic mid-position retainer with working chamber, spacer plunger, stop and position indicator. One end of piston rod is located in working chamber of hydraulic retainer with spacer piston mounted in it; spacer plunger has blind bore and transversal flat on end surface. Cavity of bore is constantly communicated with working chamber though flat. Rod has circular groove forming bead on end of rod which is engageable with inner bead of plunger.
EFFECT: improved dynamic characteristics due to compensation of piston backlash.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
ELECTROHYDRAULIC MULTICHANNEL STEERING GEAR | 2001 |
|
RU2211962C2 |
MULTI-CHANNEL SERVO UNIT | 1972 |
|
SU1840186A1 |
MULTI-CHANNEL ACTUATOR FOR FLYING VEHICLE CONTROL UNIT | 1986 |
|
SU1839992A1 |
UNIT OF COMBINED HYDRAULIC ACTUATORS | 2018 |
|
RU2685115C1 |
FOUR-PORT THREE-POSITION HYDRAULIC CONTROL VALVE WITH RESERVED ELECTRIC POWER CONTROLLED WHEEL STEERING DRIVE OF FRONT CHASSIS SUPPORT OF VEHICLE WITH HYDRAULIC DAMPER | 2007 |
|
RU2342283C1 |
COMBINATION ACTUATOR | 2003 |
|
RU2245462C1 |
COMBINATION DRIVE | 2001 |
|
RU2190783C1 |
REDUNDANT ELECTROHYDRAULIC DRIVE | 2007 |
|
RU2347717C1 |
ELECTRO-HYDRAULIC ACTUATOR | 2001 |
|
RU2207300C2 |
COMBINATION DRIVE | 2002 |
|
RU2235661C2 |
Authors
Dates
2006-05-27—Published
1980-04-18—Filed