FIELD: aeronautical engineering.
SUBSTANCE: proposed servo unit has body in each sub-channel where electrohydraulic valve with spool valve, electrohydraulic amplifier, auxiliary correcting piston with rod and centering mechanism, power piston and pressure and return lines are arranged. End face of rod of auxiliary piston is located in cavity of body connected via spool valve with return line when electrohydraulic valve is cut in and with pressure line when this valve is cut out.
EFFECT: possibility of indicating failure of electrohydraulic valve.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTI-CHANNEL ACTUATOR FOR FLYING VEHICLE CONTROL UNIT | 1986 |
|
SU1839992A1 |
MULTI-CHANNEL SERVO UNIT | 1972 |
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SU1840186A1 |
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SU1839995A1 |
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SU1839883A1 |
THREE-CHANNEL ELECTROHYDRAULIC SERVO UNIT | 1977 |
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SU1826414A1 |
ELECTROHYDRAULIC SERVO UNIT AT MECHANICAL LIMIT OF ACTUATING ROD TRAVEL | 1976 |
|
SU1840182A1 |
ELECTROHYDRAULIC MULTICHANNEL STEERING GEAR | 2001 |
|
RU2211962C2 |
ELECTRO-HYDRAULIC ACTUATOR | 2001 |
|
RU2207300C2 |
ELECTRO-HYDRAULIC SERVO UNIT | 1978 |
|
SU1840178A1 |
Authors
Dates
2006-06-20—Published
1979-09-17—Filed