FIELD: armament.
SUBSTANCE: the actuator of the guided projectile has a power cylinder with a base, piston with a rod, distribution device and a control electromagnet. The piston is provided with cups, in which turnings are made for engagement with the cylindrical shoulders made in the middle part of the piston, and their working surface has a cylindrical band changing into a cone. The cups are fastened on the piston by means of the respective nuts with a groove located in the area of the shoulder. In the base serving as a rod guide inclined ducts linked with the distributing device are made.
EFFECT: enhanced reliability of the actuator.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2000 |
|
RU2172927C1 |
| AERODYNAMIC UNIT OF STEERING GEAR OF GUIDED MISSILE | 2002 |
|
RU2206058C1 |
| 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 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 1996 |
|
RU2092782C1 |
| AIR DYNAMIC PACKAGE OF CONTROLLABLE FLYING VEHICLE CONTROL ACTUATOR | 2006 |
|
RU2309084C1 |
| GUIDED MISSILE AND SERVO UNIT FOR IT | 2000 |
|
RU2184927C1 |
| CONTROL ACTUATOR UNIT OF GUIDED PROJECTILE | 2004 |
|
RU2266511C1 |
| CONTROL ACTUATOR OF GUIDED MISSILE | 2004 |
|
RU2257534C1 |
| AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
