FIELD: flying vehicle control systems.
SUBSTANCE: end face of plunger of cut-in valve is communicated through grooves and beads of spool valve with return hydraulic line and plunger is moved by spring to extreme position, thus ensuring cross-feed of chambers of hydraulic motor bringing them into communication with return line and disconnecting the inter-bead cavity of spool valve distributor from delivery hydraulic line. Provision is made for shift to mechanical control due to motion of input member, double-arm lever and cut-off valve of drive, i.e. imparting motion to control members by muscle force in case of seizing of spool valve distributor.
EFFECT: enhanced operational reliability of system.
4 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
STANDBY SERVO HYDROMECHANICAL DRIVE | 2008 |
|
RU2370411C1 |
HYDROMECHANICAL DRIVE FOR FLYING VEHICLE CONTROL SYSTEMS | 2003 |
|
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COMBINATION DRIVE | 2001 |
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|
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COMBINATION ACTUATOR | 2003 |
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REDUNDANT HYDROMECHANICAL SERVO DRIVE FOR FLYING VEHICLE CONTROL SYSTEM | 2004 |
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ELECTROHYDRAULIC SERVO DRIVE | 2004 |
|
RU2268400C1 |
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 |
COMBINED DRIVE | 2007 |
|
RU2337856C1 |
ELECTROHYDRAULIC UNIT | 2005 |
|
RU2298698C2 |
Authors
Dates
2004-10-20—Published
2003-01-08—Filed