CONTROL ACTUATOR UNIT OF GUIDED MISSILE Russian patent published in 2005 - IPC

Abstract RU 2248520 C1

FIELD: guided missiles, in particular, their control actuators.

SUBSTANCE: the control surfaces are connected by means of a half-axle, in which a central hole is made along the missile longitudinal axis, alkane holes are made perpendicularly to the longitudinal axis for installation of the axles of the control surfaces. The half-axle has components for coupling to the actuation cylinders.

EFFECT: enhanced efficiency of armor-piercing capacity of the missile.

4 cl, 2 dwg

Similar patents RU2248520C1

Title	Year	Author	Number
GUIDED MISSILE	2000	Shipunov A.G. Zybin I.M. Fimushkin V.S. Ovchelupov N.V.	RU2165586C1
GUIDED MISSILE	1995	Shipunov A.G. Zakharov L.G. Zybin I.M. Fimushkin V.S. Kopylov Ju.D.	RU2092778C1
COMPARTMENT OF CONTROLLED MISSILE STEERING DRIVE	2020	Ovchelupov Nikolaj Vasilevich Zaslavskij Arkadij Arkadevich Fimushkin Valerij Sergeevich Aleksandrov Nikolaj Alekseevich	RU2743420C1
NOSE OF GUIDED ARTILLERY PROJECTILE	2001	Glazkov K.M. Gorev L.V. Korchigo G.V. Filisov A.D. Omarbekov B.R.	RU2194942C1
GUIDED PROJECTILE	1998	Shipunov A.G. Zybin I.M. Fimushkin V.S.	RU2150082C1
GUIDED PROJECTILE ACTUATOR UNIT	2003	Shipunov A.G. Zybin I.M. Fimushkin V.S.	RU2234672C1
GUIDED MISSILE NOSE CONE	1996	Zybin I.M. Fimushkin V.S.	RU2100767C1
GUIDED MISSILE	1998	Shipunov A.G. Zakharov L.G. Zybin I.M. Filimonov G.D.	RU2125230C1
GUIDED MISSILE	2003	Shipunov A.G. Zybin I.M. Fimushkin V.S.	RU2257533C1
GUIDED MISSILE	2005	Zybin Igor' Mikhajlovich Ovchelupov Nikolaj Vasil'Evich Fimushkin Valerij Sergeevich	RU2295698C1

RU 2 248 520 C1

Authors

Zybin I.M.

Fimushkin V.S.

Dates

2005-03-20—Published

2003-07-02—Filed