FIELD: armament.
SUBSTANCE: the folding aerodynamic member of the guided projectile has a control surface, journal, folding pivot, springs and locks. A slot is made in the control surface in which the journal with the pivot is installed. Spring-loaded locks with a tapered end and the folding pivot with a spring are positioned in the control surface and journal symmetrically on both sides of the control surface longitudinal axis. One end of the spring of the folding axis is connected to the control surface, and the other - to the journal.
EFFECT: simplified construction of the guided projectile.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FOLDING AERODYNAMIC CONTROL | 2005 |
|
RU2284450C1 |
| FORLING AERODYNAMIC UNIT | 2003 |
|
RU2243488C1 |
| COLLAPSIBLE AERODYNAMIC MEMBER | 2001 |
|
RU2197704C1 |
| FOLDING AERODYNAMIC ROCKET RUDDER | 2023 |
|
RU2803760C1 |
| FOLDING AERODYNAMIC RUDDER | 2013 |
|
RU2535789C1 |
| CONTROL SYSTEM UNIT FOR MISSILE LAUNCHED FROM TUBULAR GUIDE | 2023 |
|
RU2806773C1 |
| 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 | 2005 |
|
RU2289782C1 |
| COLLAPSIBLE AIRFOIL | 2012 |
|
RU2492412C1 |
| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2004 |
|
RU2275584C2 |
