RELAY PNEUMO-HYDRAULIC DRIVE WITH LINEARIZATION BY OSCILLATION OF ROCKET CONTROL SYSTEMS AND ARMAMENT INSTALLATIONS Russian patent published in 2004 - IPC

Abstract RU 2243491 C1

FIELD: defense equipment, guided missiles and armament installations.

SUBSTANCE: the relay pneumo-hydraulic drive with linearization by oscillation of the rocket control systems and armament installations has a series-connected adder, whose first input serves as the drive input, relay element, power amplifier, electromechanical transducer with an armature, switch-gear and an actuating motor, whose output serves as the drive output and is connected via a feedback transducer to the second input of the adder, the transducer is made neutral with an operating time determined from the preset mathematical relation.

EFFECT: enhanced technical-and-economic indices as far as enhanced speed of response and accuracy of operation are concerned, reduced mass and overall dimensions, enhanced reliability of operation, reduced labour content of manufacture and cost.

7 dwg

Similar patents RU2243491C1

Title Year Author Number
ELECTROHYDRAULIC DRIVE OF CONTROL SYSTEM OF ROCKETS AND ARMAMENT INSTALLATIONS 2005
  • Artjushchev Vladimir Vasil'Evich
  • Galanteh Aleksandr Iosifovich
  • Toshnov Fedor Fedorovich
RU2295699C1
INTERRUPTED PNEUMATIC ACTUATOR OF CONTROL SYSTEM OF SPIN-STABILIZED MISSILES AND METHOD FOR MONITORING OF ITS DYNAMICS 2000
  • Fimushkin V.S.
  • Gusev A.V.
  • Toshnov F.F.
RU2184340C2
RELAY-SUPPLY PNEUMATIC ACTUATOR EQUIPPED WITH MISSILE CONTROL SYSTEM VIBRATION LINEARISATION 2007
  • Fimushkin Valerij Sergeevich
  • Gusev Andrej Viktorovich
  • Alenichev Aleksandr Nikolaevich
  • Toshnov Fedor Fedorovich
  • Korneev Vladimir Stanislavovich
  • Koechkin Nikolaj Nikolaevich
RU2337309C1
METHOD TO CONTROL AIRCRAFT WITH SELF-OSCILLATING DEVICE OF AERODYNAMIC CONTROL SURFACES 2010
  • Gusev Andrej Viktorovich
  • Kuznetsov Vladimir Markovich
  • Morozov Vladimir Ivanovich
  • Petrushin Vladimir Vasil'Evich
RU2435131C1
SELF-SUSTAINED AUTOPILOT OF GUIDED MISSILE 1992
  • Babichev V.I.
  • Zybin I.M.
  • Toshnov F.F.
  • Fimushkin V.S.
RU2092784C1
METHOD FOR CONTROL OF MISSILE CONTROL ACTUATOR ELECTRO-PNEUMATIC DRIVE AND DEVICE FOR ITS REALIZATION 2001
  • Fimushkin V.S.
  • Gusev A.V.
  • Valov I.B.
  • Toshnov F.F.
RU2206861C2
MISSILE CONTROL METHOD AND CONTROL SYSTEM FOR ITS IMPLEMENTATION 2013
  • Morozov Vladimir Ivanovich
  • Chukanov Mikhail Nikolaevich
  • Ukhabova Ol'Ga Nikolaevna
RU2536838C2
SELF-OSCILLATING CONTROL ACTUATOR OF SPIN-STABILIZED GUIDED MISSILE 2000
  • Fimushkin V.S.
  • Gusev A.V.
  • Toshnov F.F.
  • Rogov S.G.
RU2184926C2
METHOD AND SYSTEM FOR CONTROL OVER ROCKET 2012
  • Morozov Vladimir Ivanovich
  • Chukanov Mikhail Nikolaevich
  • Ukhabova Ol'Ga Nikolaevna
RU2527391C2
CONTROLLED MISSILE STEERING DRIVE CONTROL METHOD 2023
  • Fimushkin Valerij Sergeevich
  • Ovsenev Sergej Sergeevich
  • Nikanorov Boris Aleksandrovich
  • Masherov Pavel Evgenevich
  • Vasilev Aleksandr Anatolevich
  • Gusev Dmitrij Andreevich
RU2823085C1

RU 2 243 491 C1

Authors

Fimushkin V.S.

Gusev A.V.

Zaslavskij A.A.

Toshnov F.F.

Dates

2004-12-27Published

2003-06-18Filed