FIELD: aircraft engineering.
SUBSTANCE: proposed drive comprises stepped master motor, differential, distributor, booster actuator, stepped motor zero position sensor, telemetry transducer and feedback redactor. As the result, drive weight and overall dimensions are decreased. Note here that equal force is used to extend and to retract differential cylinder rod, that is, results an equivalent bidirectional action. In feedback signal operation, conversion of energy types is not required in feedback internal circuit.
EFFECT: higher reliability and accuracy of control.
6 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ELECTROHYDRAULIC DISCRETE ROTARY DRIVE | 2016 |
|
RU2642010C1 |
| DIGITAL ELECTROHYDRAULIC DRIVE | 0 |
|
SU792002A1 |
| MACHINE | 2009 |
|
RU2401762C1 |
| TRACTION AND-TRANSPORT VEHICLE | 2002 |
|
RU2232685C1 |
| AIRCRAFT ELECTRIC DRIVE (VERSIONS) | 2016 |
|
RU2630966C1 |
| ELECTROHYDRAULIC STEERING GEAR OF VEHICLE | 0 |
|
SU1337306A1 |
| WHEELED VEHICLE | 0 |
|
SU948704A1 |
| VEHICLE | 0 |
|
SU935325A1 |
| HEELED CATERPILLAR TRANSPORT FACILITY | 2009 |
|
RU2407668C2 |
| ELECTROHYDRAULIC MULTICHANNEL STEERING GEAR | 2001 |
|
RU2211962C2 |
