FIELD: weapons and ammunition.
SUBSTANCE: guided missile steering gear comprises two one-way actuating motors jointed, via rocker, with rudders axles. Actuating motors represent plunger electromagnets with armatures furnished with rods provided with end caps. The latter represent a lug with opening for pivot bolt displaced relative to rod axial line in perpendicular direction. Caps and rocker are pivoted together so that rocker arm length to the pivot makes less than half the OD of plunger electromagnet casing.
EFFECT: higher stability, simplified design.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE AND SERVO UNIT FOR IT | 2000 |
|
RU2184927C1 |
AIR DYNAMIC PACKAGE OF CONTROLLABLE FLYING VEHICLE CONTROL ACTUATOR | 2006 |
|
RU2309084C1 |
AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
METHOD FOR ADJUSTMENT OF FLIGHT VEHICLE CONTROL ACTUATOR AND CONTROL ACTUATOR ELECTROMAGNETIC UNIT FOR ITS REALIZATION | 2005 |
|
RU2291383C1 |
ELECTROMAGNETIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2005 |
|
RU2283472C1 |
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 |
METHOD OF ASSEMBLY OF A GUIDED MISSILE STEERING ENGINE AND A METHOD TO CHECK GUIDED MISSILE PNEUMOSHUTTER LEAKAGE CHECK | 2002 |
|
RU2235285C2 |
METHOD FOR CONTROL OF MISSILE AND CONTROL ACTUATOR POD (MODIFICATIONS) | 2005 |
|
RU2288439C1 |
AIR-DYNAMIC UNIT OF GUIDED PROJECTILE ACTUATOR | 2002 |
|
RU2234670C2 |
METHOD AND DEVICE FOR INITIATING AN AIR-DYNAMIC STEERING DRIVE OF A GUIDED AERIAL BOMB, A METHOD FOR CHECKING THE READINESS OF AN AIR-DYNAMIC STEERING DRIVE BEFORE DROPPING A GUIDED AERIAL BOMB, AN AIR-DYNAMIC STEERING GEAR AND CONTROL EQUIPMENT FOR AN AIR-DYNAMIC STEERING DRIVE OF AN AERIAL BOMB | 2020 |
|
RU2748828C1 |
Authors
Dates
2009-10-20—Published
2008-06-16—Filed