BOARD DETACHABLE JOINT Russian patent published in 2013 - IPC F16L37/20 

Abstract RU 2473003 C1

FIELD: machine building.

SUBSTANCE: board detachable pipeline joint contains inlet neck fixed on board of rocket and detachable pipe connected to flanges with conical outer surfaces and locking device. Locking device is designed as V-shaper shoe arranged in a circumferential direction and installed on flanges, the shoes are attached to pipe by elastic elements and are enveloped by rope system provided with tension elements and consisting of several branches connected to each other and pipe by cylindrical rods arranged inside of fixed by shearing elements movable stocks connected to ground withdrawal mechanism. At that elastic elements are designed as zigzagging leaf springs. There is a gap between thrust faces of cylindrical rods and movable stocks, its size is not less than pitch of locking member shear. Ends of rope system branches are enveloped by limiting sleeves fixed on brackets.

EFFECT: reducing of force impact on rocket upon detachment of pipeline connected to the rocket to minimum possible level.

Similar patents RU2473003C1

Title Year Author Number
DETACHABLE CONNECTION 2015
  • Kolyaskin Georgij Yakovlevich
RU2596706C1
DEVICE FEEDING THERMOSTATING MEDIUM INTO LAUNCH VEHICLE COMPARTMENT 2007
  • Bolotin Viktor Aleksandrovich
  • Djad'Kin Anatolij Aleksandrovich
  • Serafimov Vladimir Petrovich
  • Simakova Tat'Jana Vladimirovna
  • Trashkov Gennadij Anatol'Evich
RU2368548C2
METHOD OF FILLING OXIDIZER TANK OF LAUNCH VEHICLE OF AEROSPACE SYSTEM WITH LIQUID OXYGEN 2000
  • Borisenko A.A.
  • Denisov A.V.
  • Egorov A.M.
  • Kirsanov G.V.
  • Luk'Janova Eh.A.
  • Mark V.A.
  • Syrovets M.N.
  • Tupitsyn N.N.
  • Fedorov V.I.
  • Khaspekov V.G.
RU2167086C1
METHOD OF FILLING OXIDIZER TANK OF LAUNCH VEHICLE OF AIR-SPACE SYSTEM WITH LIQUID OXYGEN 2001
  • Tupitsyn N.N.
  • Katkov R.Eh.
  • Syrovets M.N.
  • Fedorov V.I.
  • Khaspekov V.G.
RU2197413C1
DEVICE FOR MOVING VERTICALLY TURNABLE SUPPORT BOOM FROM SIDE OF LAUNCH VEHICLE 2003
  • Lednev V.G.
RU2246436C2
METHOD OF CHARGING OXIDIZER TANK OF LAUNCH VEHICLE OF AERO-SPACE SYSTEM WITH LIQUID OXYGEN 2001
  • Egorov A.M.
  • Luk'Janova Eh.A.
  • Sidorov Ju.N.
  • Sukhacheva O.V.
  • Syrovets M.N.
  • Tupitsyn N.N.
  • Fedorov V.I.
  • Khaspekov V.G.
RU2208563C2
SYSTEM FOR ROCKET LAUNCHING FROM WATER AREA 1999
  • Kruglov Ju.A.
  • Im Ju.Ja.
  • Sinil'Shchikov B.E.
  • Zjuzlikov V.P.
RU2151995C1
QUICK-DETACHABLE PIPE JOINT 2002
  • Petrov R.A.
  • Smol'Janinov V.A.
  • Stroev V.E.
RU2260737C2
HATCH COVER ASSEMBLY UNIT OF FLYING VEHICLE THERMOSTATING SYSTEM 1999
  • Tolmachev S.M.
  • Tarasova G.A.
  • Nevmjanov V.S.
RU2158215C1
APPARATUS FOR SUSPENDING SOFT CONTAINER 1988
  • Kuznetsov A.P.
  • Lekhanov O.N.
  • Sergeev A.M.
  • Rogach M.S.
  • Novitskij N.N.
  • Aleshin A.A.
SU1605479A1

RU 2 473 003 C1

Authors

Soin Valerij Ivanovich

Tolmachev Sergej Mikhajlovich

Tugolukov Anatolij Vasil'Evich

Dates

2013-01-20Published

2011-10-17Filed