FIELD: military equipment, guided missile control actuators. SUBSTANCE: guided missile control actuator unit has a body, actuation cylinder, disk-type distribution device and control electromagnet, whose case carries a fixed disk furnished with a location shoulder with a supporting fillet. Configuration of the front end of the fixed disk is similar to that of the control actuator body in the point of their joint, and ports having an area at least of five areas of the grooves in the disks are made in the zone of the running clearance. EFFECT: improved design.
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2089838C1 |
AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 1996 |
|
RU2092782C1 |
CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
STEERING DRIVE UNIT OF GUIDED MISSILE | 1997 |
|
RU2121650C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
GUIDED MISSILE | 1997 |
|
RU2124695C1 |
Authors
Dates
1997-10-10—Published
1996-01-04—Filed