FIELD: defensive equipment, in particular, guided missile control actuator units. SUBSTANCE: air intakes 9 in the control actuator unit have rectangular shape; in the upper and lower parts they are furnished with an air-intake opening changing into a vertical duct. Spring 12 is installed in the duct. A groove is made in the front wall, which receives stop 13, a bore with sealing ring 14 is provided in the bottom part. Made in bedplate 2, which carries the air intakes, are vertical ducts connected to actuators 4; and stops 13 retaining the air takes in the open position are installed. EFFECT: improved design. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2087841C1 |
| METHOD OF CHECK-UP OF BRINGING TO SERVICEABLE CONDITION OF SEALED AUTOPILOT UNIT | 1997 |
|
RU2126949C1 |
| GUIDED ARTILLERY PROJECTILE | 2004 |
|
RU2258897C1 |
| GUIDED MISSILE ACTUATOR ASSEMBLY | 1996 |
|
RU2101666C1 |
| GUIDED MISSILE ACTUATOR ASSEMBLY | 1996 |
|
RU2101665C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1997 |
|
RU2124697C1 |
| CONTROL ACTUATOR UNIT OF GUIDED PROJECTILE | 2004 |
|
RU2280231C1 |
| GUIDED MISSILE | 1994 |
|
RU2084809C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| GUIDED MISSILE NOSE CONE | 1996 |
|
RU2100767C1 |
