COMPRESSOR BLADE (VERSIONS) AND ITS APPLICATION Russian patent published in 2002 - IPC

Abstract RU 2191930 C2

FIELD: compressors for stationary gas turbines. SUBSTANCE: profile of proposed blade provides for especially low aerodynamic losses when blade is washed off at high Reynolds number. EFFECT: low aerodynamic losses. 11 cl, 6 dwg

Similar patents RU2191930C2

Title Year Author Number
COMPRESSOR ROTATING BLADE FOR AXIAL COMPRESSOR 2010
  • Kreger Georg
  • Kornelius Kristian
  • Nikke Ehberkhard
RU2534190C2
AXIAL TURBOMACHINE WITH LOW CLEARANCE LOSSES 2009
  • Kreger Georg
  • Kornelius Kristian
  • Aulikh Martsel'
RU2498084C2
TWISTED GAS TURBINE ENGINE AERODYNAMIC PROFILE HAVING TWISTED RIB 2014
  • Li Chin-Pan
RU2666717C2
CASTING CORE FOR TWISTED GAS TURBINE ENGINE AIRFOIL HAVING A TWISTED RIB 2014
  • Li, Chin-Pan
RU2647395C2
GUIDE BLADE OR ROTATING BLADE FOR AXIAL COMPRESSOR 2009
  • Li Jan Sheng
RU2493438C2
STREAMLINED BODY, PRIMARILY FOR AIRCRAFT 2010
  • Gerber Martin
  • Shrauf Getsa
RU2496680C1
CURVED BLADE OF COMPRESSOR 2000
  • Vud Piter Dzhon
  • Deker Dzhon Dzhared
  • Shtajnmetts Gregori Todd
  • Mil'Ke Mark Dzhozef
RU2220329C2
RADIAL COMPRESSOR 2015
  • Hermes Viktor
RU2674844C2
COMPRESSOR BLADE FEATHER 2018
  • Bruni, Giuseppe
  • Krishnababu, Senthil
RU2748318C1
BLADE FOR GAS TURBINE, IMPLEMENTATION OF TURBINE BLADE AND PROCEDURE FOR TURBINE BLADE COOLING 2005
  • Bal'Dauf Shtefan
  • Khendler Mikhel'
  • Lerner Kristian
RU2393356C2

RU 2 191 930 C2

Authors

Keller Ul'F

Menig Rejnkhard

Dates

2002-10-27Published

1998-06-15Filed