COMPARTMENT OF CONTROLLED MISSILE STEERING DRIVE Russian patent published in 2021 - IPC F42B15/01 B64C13/02 

Abstract RU 2743420 C1

FIELD: weapons.

SUBSTANCE: invention relates to weapons and specifically to power elements of control systems and can be used in guided missiles with aerodynamic rudders. Device contains frames. Anchor is installed on it. It is located perpendicular to longitudinal axis of missile and is connected with rudders and cores with coils connected with frame by fasteners. Frames are equipped with side posts with a transverse bar between them. On the crossbar shunts in the form of planks are installed. Besides, two cores with coils are additionally introduced into compartment of steering drive. Their longitudinal axes are located in plane parallel to longitudinal axis of missile. Cores with coils are installed in pairs on planks of magnetically soft material, with possibility of position adjustment, under each armature arm, symmetrically to axis of its rotation, on both sides relative to central window, without overlapping it. Each pair of single-pole cores with coils forms working gaps with anchor, through which magnetic flux is closed.

EFFECT: technical result is higher power of electromagnetic drive steering due to winding parameters, which increase magnetizing force without changing missile calibre and while preserving armour penetration of warhead.

5 cl, 3 dwg

Similar patents RU2743420C1

Title Year Author Number
GUIDED PROJECTILE ACTUATOR UNIT 2003
  • Shipunov A.G.
  • Zybin I.M.
  • Fimushkin V.S.
RU2234672C1
GUIDED PROJECTILE 2009
  • Gusev Andrej Viktorovich
  • Fimushkin Valerij Sergeevich
  • Ovchelupov Nikolaj Vasil'Evich
RU2406063C1
GUIDED MISSILE 2022
  • Stakanov Nikolai Vladimirovich
  • Stakanov Aleksandr Nikolaevich
  • Gundarev Vladimir Vladimirovich
  • Vinogradov Vitalii Valerevich
  • Butymov Valerii Viacheslavovich
RU2772089C1
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
  • Aleksandrov Nikolaj Alekseevich
  • Balzamov Igor Anatolevich
  • Evteev Konstantin Petrovich
  • Elesin Vladimir Pavlovich
  • Kuznetsov Mikhail Yurevich
  • Nikanorov Boris Aleksandrovich
  • Fimushkin Valerij Sergeevich
  • Shumilin Aleksej Yurevich
  • Shigin Aleksandr Viktorovich
RU2669979C1
GUIDED SHELL 2007
  • Stepanichev Igor' Veniaminovich
  • Gusev Andrej Viktorovich
  • Fimushkin Valerij Sergeevich
  • Ovchelupov Nikolaj Vasil'Evich
  • Nikanorov Boris Aleksandrovich
RU2351887C1
ELECTROMAGNETIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR 2005
  • Ovchelupov Nikolaj Vasil'Evich
  • Gusev Andrej Viktorovich
  • Zaslavskij Arkadij Arkadievich
  • Stepanichev Igor' Veniaminovich
  • Fimushkin Valerij Sergeevich
RU2283472C1
GUIDED MISSILE 2001
  • Aristarkhov I.V.
  • Varentsov S.E.
  • Zybin I.M.
  • Ovchelupov N.V.
RU2218546C2
METHOD OF GUIDED MISSLE LAUNCH 2007
  • Stepanichev Igor' Veniaminovich
  • Gusev Andrej Viktorovich
  • Fimushkin Valerij Sergeevich
  • Ovchelupov Nikolaj Vasil'Evich
  • Galkin Viktor Nikolaevich
RU2358232C2
GUIDED MISSILE 2007
  • Stepanichev Igor' Veniaminovich
  • Gusev Andrej Viktorovich
  • Fimushkin Valerij Sergeevich
  • Ovchelupov Nikolaj Vasil'Evich
  • Galkin Viktor Nikolaevich
RU2351886C1
GUIDED MISSLE 2007
  • Stepanichev Igor' Veniaminovich
  • Gusev Andrej Viktorovich
  • Fimushkin Valerij Sergeevich
  • Ovchelupov Nikolaj Vasil'Evich
  • Kuznetsov Mikhail Jur'Evich
RU2358229C2

RU 2 743 420 C1

Authors

Ovchelupov Nikolaj Vasilevich

Zaslavskij Arkadij Arkadevich

Fimushkin Valerij Sergeevich

Aleksandrov Nikolaj Alekseevich

Dates

2021-02-18Published

2020-05-18Filed