FIELD: armament.
SUBSTANCE: the control actuator of guided missile has a servo motor with a power cylinder, distribution device and a control electromagnet. The distribution device is positioned in the input channel of the servo motor coupled with the cavities of the power cylinder, installed in which are the filters and throttles, nozzles overlapped by a shutter linked with the armature of the control electromagnet, are installed at the outlet from the cavity of the power cylinder. The area of the throttle and the area of the nozzle are made at a definite relationship.
EFFECT: enhanced reliability of operation of the control actuator on hot gas and improved dynamic characteristics.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
| CONTROL ACTUATOR UNIT OF GUIDED MISSILE | 2004 |
|
RU2276771C2 |
| AIR DYNAMIC PACKAGE OF CONTROLLABLE FLYING VEHICLE CONTROL ACTUATOR | 2006 |
|
RU2309084C1 |
| GUIDED MISSILE AND SERVO UNIT FOR IT | 2000 |
|
RU2184927C1 |
| ACTUATOR OF GUIDED PROJECTILE | 2004 |
|
RU2282134C2 |
| AIR-DYNAMIC UNIT OF GUIDED PROJECTILE ACTUATOR | 2002 |
|
RU2234670C2 |
| GUIDED PROJECTILE | 1998 |
|
RU2150082C1 |
| STEERING DRIVE UNIT OF GUIDED MISSILE | 1997 |
|
RU2121650C1 |
| CONTROLLED PROJECTILE, STEERING DRIVE GROUP OF CONTROLLED PROJECTILE, PNEUMATIC DISTRIBUTION DEVICE OF STEERING DRIVE OF CONTROLLED PROJECTILE, MECHANISM OF INITIATION OF STEERING DRIVE OF CONTROLLED PROJECTILE | 2017 |
|
RU2669979C1 |
