FIELD: rocketry.
SUBSTANCE: invention relates to rocketry, namely to control drives, and can be used in guided missiles. Disclosed is a unit of steering drives of a controlled projectile, which contains a frame, aerodynamic rudders fixed on axes placed in the frame, and steering gears, which are located on both sides of axes of aerodynamic rudders. On the end surface of each steering machine there fixed is a bracket having an axis on which a rocker arm is installed, by one its arm is connected to a rod of the steering machine, and by the other arm – to a tie-rod located between the rocker arm and a lever rigidly fixed on the axis of aerodynamic control surfaces. Rocker arm is connected to the steering machine by means of a hinge mechanism, and the tie-rod has a movable connection to the rocker arm.
EFFECT: compensation of weight of moving parts of steering machine.
3 cl, 1 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 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1997 |
|
RU2138764C1 |
| GUIDED MISSILE AND SERVO UNIT FOR IT | 2000 |
|
RU2184927C1 |
| GUIDED MISSILE STEERING GEAR | 2008 |
|
RU2370727C1 |
| GUIDED MISSILE | 2003 |
|
RU2244897C1 |
| MECHANISM FOR COMBINATION CONTROL OF ROCKET | 2005 |
|
RU2316720C2 |
| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2000 |
|
RU2166727C1 |
| ARRESTER OF STEERING ELECTRIC GEAR OF ROCKET | 2010 |
|
RU2426071C1 |
| FLYING VEHICLE | 1998 |
|
RU2142388C1 |
| COMPARTMENT OF CONTROLLED MISSILE STEERING DRIVE | 2020 |
|
RU2743420C1 |
