CENTRIFUGAL OIL SEPARATOR WITH VARIABLE FLOW CROSS SECTION Russian patent published in 2013 - IPC F02C7/06 

Abstract RU 2477806 C2

FIELD: machine building.

SUBSTANCE: shaft has at least one air passage opening and a piston placed inside the shaft so that inner shaft of the shaft is divided into two compartments, which are sealed relative to each other; at that, outlet compartment is provided with one or more passage openings for the air being under environmental pressure, and the other inlet compartment is under variable pressure existing inside air/oil cavity. When under action of difference of pressures existing in two compartments, the piston obtains the possibility of performing translational movement inside inner part of the shaft by movement from one extreme position to another one; at that, when in the first position, one or more air passage openings are fully opened, and when in the second position, one or more air passage openings are partially closed with the piston.

EFFECT: providing high tightness of air-oil cavities at the engine operation in any modes and maintaining the lowest possible oil consumption.

7 cl, 3 dwg

Similar patents RU2477806C2

Title Year Author Number
METHOD AND DEVICE FOR BALANCING PRESSURE IN TURBOJET BEARINGS CHAMBER 2009
  • Fehnteskju Jon
  • Zhill' Loran
  • Murlan Zhan-P'Er
RU2486358C2
TURBOJET ENGINE OIL CHAMBER SEAL 2011
  • Got'E Zherar Filipp
  • Morreal' Serzh Rene
RU2568723C2
WATER-MIXING COCK CARTRIDGE, COCK CONTAINING THIS CARTRIDGE, AND THERMOSTATIC UNIT FOR EQUIPPING THIS CARTRIDGE 2005
  • Mas Kristian
RU2379432C2
DEVICE FOR SEPARATING AIR FROM OIL IN GAS-TURBINE ENGINE 1999
  • Korolev O.G.
  • Zlygostev D.M.
  • Kirievskij Ju.E.
RU2171386C2
CARTER FOR ENGINE OR COMPRESSOR 2016
  • Herbiet, Olivier
RU2664606C1
DEVICE FOR COOLING OIL IN GAS TURBINE ENGINES 2014
  • Muller Jean-Louis
  • Mouton Pierre Charles
RU2665799C2
METHOD OF AND DEVICE TO INCREASE ECONOMY OF TURBOJET ENGINE (VERSIONS) 2004
  • Chebotareva Irina Dmitrievna
  • Kolesnichenko Vladimir Grigor'Evich
  • Rybkina Natal'Ja Vladimirovna
RU2295644C9
GAS TURBINE ENGINE WITH STATOR MOUNTED ON GEARBOX OF ASSEMBLY UNITS 2008
  • Avila Kloeh
  • Sharbonnel' Zhan-Lui
  • Dardenn Mari-Liz
  • Follon'E Korinn
  • Muton P'Er
RU2443881C2
FILTRATION OF FLOW CONSISTING OF GAS AND PARTICLES 2015
  • Bauduin Lionel
  • Guillemont Maxence
  • Viel Julien
  • Prunera-Usach Stephane
RU2685346C2
TURBO-COMPRESSOR INTERNAL COMBUSTION ENGINE 2005
  • Jadegar Dzherri Irazh
RU2393362C2

RU 2 477 806 C2

Authors

Morreal' Serzh Rene

Dates

2013-03-20Published

2009-03-11Filed