AIR BLEEDER WITH INERTIAL FILTER IN COMPRESSOR TANDEM ROTOR Russian patent published in 2014 - IPC F04D27/02 F04D29/28 

Abstract RU 2519009 C2

FIELD: engines and pumps.

SUBSTANCE: invention relates to auxiliary air system of radial- and mixed-flow compressor with rotary shaft. Note here that said compressor can compress oxidiser gas. Auxiliary air system comprises oxidiser gas bleeder system arranged in the rotor.

EFFECT: resistance against fouling with oxidiser gas.

8 cl, 5 dwg

Similar patents RU2519009C2

Title Year Author Number
TURBINE UNIT, WHICH CORRESPONDS TO TUBE FOR COLLISION COOLING AND GAS TURBINE ENGINE 2012
  • Magglstoun Dzhonatan
RU2587032C2
GAS TRANSFER UNIT 2020
  • Bolotin Nikolaj Borisovich
RU2735881C1
GAS TRANSFER UNIT 2020
  • Bolotin Nikolaj Borisovich
RU2735040C1
AXIAL-CENTRIFUGAL MULTISTAGE COMPRESSOR 2017
  • Voevodin Nikolaj Nikolaevich
RU2659657C1
SYSTEM OF PROPELLERS RUNNING IN OPPOSITE DIRECTIONS AND DRIVEN BY EPICYCLOIDAL MECHANISM THAT ENSURES BALANCED DISTRIBUTION OF TORQUE BETWEEN TWO PROPELLERS 2009
  • Bal'K Vuter
  • Shar'E Zhil' Alen
  • Galle Fransua
RU2509903C2
MOUNTING STRUCTURE OF NOZZLE GUIDE VANES AT INLET CHANNEL OF RADIAL GAS TURBINE OF ENGINE 2011
  • Dvorak Marek
  • Mouvill R. Jan
RU2558731C2
ANTI-ICE SYSTEM OF AIRCRAFT GAS TURBINE ENGINE INLET CONE 2007
  • Eharit Toma Zhjul'En Rolan
  • Pikar Zhan-Iv Daniel'
RU2444638C2
METHOD OF AND DEVICE FOR TURBO-FAN GAS TURBINE ENGINE CLEANING 2004
  • Jerpe Karl-Jokhan
  • Asplund Peter
RU2331487C2
TURBO-COMPRESSOR INTERNAL COMBUSTION ENGINE 2005
  • Jadegar Dzherri Irazh
RU2393362C2
SUPERSONIC COMPRESSOR UNIT (VERSIONS) AND METHOD FOR ASSEMBLY THEREOF 2011
  • Hofer Douglas Carl
  • Michelassi Vittorio
RU2591750C2

RU 2 519 009 C2

Authors

Brije Kristof Mishel' Zhorzh Marsel'

Porodo Zherom Iv Feliks Zhil'Ber

Tarnovski Loran P'Er

Dates

2014-06-10Published

2010-03-31Filed