COMPLEX BLADE OF AXIAL TURBO-MACHINE Russian patent published in 2011 - IPC F01D5/14 

Abstract RU 2416029 C2

FIELD: machine building.

SUBSTANCE: complex blade of axial turbo-machine consists of metal shank end, of radial metal rod tightly connected with shank end, of band flange secured on periphery end of radial rod, of deflector and of profiled hollow case, freely arranged outside radial rod and resting on band flange at their radial transfer along radial rod. The profiled case in its length is complex and consists of at least two not interconnected portions freely arranged on the radial rod outside a deflector between the shank end and the band flange, whereon an upper part of the profiled case rests. All portions of the profiled case are made out of heat resistant ceramic or composite materials.

EFFECT: raised reliability of blade.

2 cl, 1 dwg

Similar patents RU2416029C2

Title Year Author Number
COMPOSITE WORKING BLADE OF TURBOMACHINE 2023
  • Plotnikov Petr Nikolaevich
  • Zankovich Aleksanr Vladlenovich
  • Shlegin Lev Ruslanovich
RU2822437C1
GAS TURBINE CERMET BLADE 2009
  • Sudarev Anatolij Vladimirovich
  • Sur'Janinov Andrej Andreevich
  • Molchanov Aleksandr Sergeevich
  • Kolacheva Julija Vladimirovna
RU2433276C2
GAS TURBINE CERMET BLADE 2012
  • Konjaev Evgenij Alekseevich
  • Kajumov Viktor Pavlovich
RU2510463C2
TURBOMACHINE ROTATING BLADE 1995
  • Tikhoplav V.Ju.
  • Fedotov A.I.
  • Sudarev A.V.
  • Podgorets V.Ja.
  • Tikhoplav T.S.
  • Molchanov A.S.
RU2118462C1
NOZZLE BLADE OF TURBOMACHINE 1995
  • Tikhoplav V.Ju.
  • Fedotov A.I.
  • Sudarev A.V.
  • Shevchenko V.S.
  • Tikhoplav T.S.
  • Podgorets V.Ja.
  • Shmarin I.S.
RU2121063C1
GAS TURBINE COOLED CERAMET BLADES 1999
  • Sudarev A.V.
  • Sur'Janinov A.A.
  • Tikhoplav V.Ju.
  • Grishaev V.V.
  • Podgorets V.Ja.
  • Molchanov A.S.
  • Sudarev B.V.
RU2204020C2
COMPOSITE BLADE FOR COMPRESSOR OF AXIAL TURBOMACHINE AND TURBOMACHINE 2016
  • Jean-Francois Cortequisse
RU2714385C2
GAS TURBINE COOLED CERMET WORKING BLADE 1995
RU2095579C1
WORKING BLADE OF THE GAS TURBINE 2017
  • Leontev Valerij Vladimirovich
RU2656052C1
BLADE FOR AIRCRAFT COMPRESSORS AND TURBINES 2003
  • Lukovkin A.I.
RU2243851C1

RU 2 416 029 C2

Authors

Sudarev Anatolij Vladimirovich

Sur'Janinov Andrej Andreevich

Dates

2011-04-10Published

2009-04-13Filed