FIELD: flying vehicle control systems.
SUBSTANCE: proposed drive has housing with power member and passages connected with hydraulic pressure and return lines, hydraulic motor with differential piston forming rod and rodless cavities, distributor kinematically linked with control crank and three spring-loaded check valves; one check valve is used for admitting working fluid from pressure hydraulic line to distributor and rod cavity of hydraulic motor and excluding its return. Two other spring-loaded check valves are used for admitting working fluid from return line to rod cavity and rodless cavity and excluding its return.
EFFECT: possibility of manual control.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
HYDROMECHANICAL DRIVE | 2003 |
|
RU2238220C2 |
COMBINED DRIVE | 2007 |
|
RU2337856C1 |
ELECTROHYDRAULIC UNIT | 2000 |
|
RU2191297C2 |
ELECTROHYDRAULIC ACTUATOR UNIT | 2005 |
|
RU2288133C1 |
COMBINATION DRIVE | 2002 |
|
RU2235661C2 |
ELECTROHYDRAULIC UNIT | 2005 |
|
RU2298698C2 |
ELECTROHYDRAULIC UNIT | 2002 |
|
RU2233768C1 |
ELECTRO-HYDRAULIC ACTUATOR | 2001 |
|
RU2207300C2 |
SELF-CONTAINED HYDRAULIC DRIVE-ACTUATOR ELECTROHYDRAULIC UNIT | 2003 |
|
RU2262625C2 |
COMBINATION ACTUATOR | 2003 |
|
RU2245462C1 |
Authors
Dates
2005-07-20—Published
2003-09-22—Filed