FIELD: rocketry, in particular, control actuators of guided missiles.
SUBSTANCE: a hole for installation of the cylindrical part of the armature is made in the control actuator unit in the yoke of the control electromagnet. A clearance is made between the cylindrical part of the armature and the yoke hole. The upper part of the armature is a component of the magnetic circuit, and the lower part is made in the form of a shutter closing the exit nozzles. Strips are fastened on both sides of the armature, in which the armature is installed on an axle in the bearings, adjusting screws of the spring fastened on the armature axle are installed on one of the strips.
EFFECT: enhanced dynamic characteristics of the control actuator unit of the guided missile.
5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| 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 |
| CONTROL ACTUATOR OF GUIDED MISSILE | 2004 |
|
RU2257534C1 |
| COMPARTMENT OF CONTROLLED MISSILE STEERING DRIVE | 2020 |
|
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| ELECTRO-PNEUMATIC CONTROL ACTUATOR OF GUIDED MISSILE | 1999 |
|
RU2157503C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
| CONTROL ACTUATOR POD OF GUIDED PROJECTILE | 2005 |
|
RU2288440C1 |
| AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
