FIELD: military equipment.
SUBSTANCE: the control actuator unit of the guided missile has a control-surface axle with a rocker, coupled to which are the actuation cylinders with diaphragm-type pistons with a flexural center and one-sided rod, as well the piston center-of-gravity position assemblies. Each center-of-gravity position assembly is made in the form of a central rod of a permanent diameter installed in the cylinder cavity, and annular guide bush made on the rod on the side of the outlet of the axial blind hole formed in the rod, forming a movable fit with the rod. The distance from the axis of the control surfaces to the axis of each cylinder is determined according to a definite dependence.
EFFECT: simplified construction of the control actuator unit and enhanced service characteristic.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| 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 |
| CONTROLLABLE PROJECTILE ACTUATOR | 1981 |
|
SU1839987A1 |
| SERVO UNIT PACKAGE | 1979 |
|
SU1839986A1 |
| GUIDED MISSILE STEERING GEAR | 2008 |
|
RU2370727C1 |
| TWO-CHANNEL AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2002 |
|
RU2224214C2 |
| GUIDED MISSILE AND SERVO UNIT FOR IT | 2000 |
|
RU2184927C1 |
| ELECTROMAGNETIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2005 |
|
RU2283472C1 |
| GUIDED MISSILE | 2007 |
|
RU2351886C1 |
| AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
| CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
