SEPARATION MECHANISM DRIVE Russian patent published in 2024 - IPC B64G1/64 B64C1/00 

Abstract RU 2811613 C1

FIELD: rocket science.

SUBSTANCE: invention relates to units for separating structural elements. The drive of the separation mechanism includes a housing communicating with the engine combustion chamber, a charge with an igniter capsule, a main piston and a firing pin. It includes two parts: In the front part of the body there is a split ring that covers the body of the striker and is made in the form of separate retaining inserts, partially immersed in a groove on the striker body, having the shape of the immersed part, identical to the shape of the groove on the striker body, and covered by a locking piston, pressed by a retaining spring with a stop at main piston. The main piston encloses the striker body and includes a locking piston capture device. The gripping device is installed in a slot made in the body of the striker. In addition, a unidirectional valve is installed in the front part of the body, closing the internal volume formed between the main piston and the striker body. The main piston rests against a limiter installed in the rear part of the housing, which is equipped with a receiving hole in communication with the combustion chamber of the engine.

EFFECT: preservation of mechanical characteristics during long-term operation at elevated temperatures.

1 cl, 3 dwg

Similar patents RU2811613C1

Title Year Author Number
METHOD FOR CREATING SEPARATION MECHANISM DRIVE 2023
  • Strelnikov Aleksandr Sergeevich
RU2811609C1
INITIATING DEVICE FOR ROCKET STAGE SEPARATION MECHANISM 2023
  • Strelnikov Aleksandr Sergeevich
RU2811615C1
METHOD FOR INITIATING ROCKET STAGE SEPARATION MECHANISM 2023
  • Strelnikov Aleksandr Sergeevich
RU2811616C1
MISSILE AND DRIVE OF MISSILE STAGE SEPARATION MECHANISM 2005
  • Shipunov Arkadij Georgievich
  • Kuznetsov Vladimir Markovich
  • Kapustin Anatolij Sergeevich
  • Filippov Valerij Viktorovich
  • Golovanov Nikolaj Sergeevich
  • Fimushkin Valerij Sergeevich
  • Nikanorov Boris Aleksandrovich
RU2284460C1
MISSILE AND GAS GENERATOR OF MISSILE STAGE SEPARATION MECHANISM 2005
  • Shipunov Arkadij Georgievich
  • Kuznetsov Vladimir Markovich
  • Shvykin Jurij Sergeevich
  • Kapustin Anatolij Sergeevich
  • Filippov Valerij Viktorovich
  • Rodin Leonid Alekseevich
RU2284456C1
ROCKET 2002
  • Shipunov A.G.
  • Babichev V.I.
  • Filippov V.V.
  • Kolonitskij E.K.
  • Pavlov A.M.
RU2202761C1
ROCKET 2009
  • Kolikov Vladimir Anatol'Evich
  • Korennoj Aleksandr Vladimirovich
  • Morozov Valerij Dmitrievich
  • Savin Sergej Anatol'Evich
  • Surnachev Aleksandr Fedorovich
  • Vasina Elena Anatol'Evna
RU2399865C1
SAFETY BELT TENSION ADJUSTER 1998
  • Lapichev N.V.
  • Shljapnikov G.P.
  • Janbaev G.M.
RU2149780C1
METHOD FOR SEPARATION OF PROJECTILE SUSTAINER STAGE FROM ZERO-STAGE ENGINE AND DEVICE FOR ITS REALIZATION 2005
  • Kapustin Anatolij Sergeevich
  • Kolikov Vladimir Anatol'Evich
  • Korennoj Aleksandr Vladimirovich
  • Kuznetsov Vladimir Markovich
  • Morozov Valerij Dmitrievich
  • Savin Sergej Anatol'Evich
  • Stepanichev Igor' Veniaminovich
  • Surnachev Aleksandr Fedorovich
RU2313762C2
METHOD OF SHOOTING FROM CANNON UNITARY SHOT AND FIXED ROUND THEREFOR 2015
  • Anikushin Nikolaj Aleksandrovich
  • Djatlov Sergej Ivanovich
  • Kolotilin Vladimir Ivanovich
  • Kosin Mikhail Evgenevich
  • Shigin Aleksandr Viktorovich
  • Judina Julija Vladimirovna
RU2584405C1

RU 2 811 613 C1

Authors

Strelnikov Aleksandr Sergeevich

Dates

2024-01-15Published

2023-07-28Filed