TURBINE ROTOR PART RECONDITIONING METHOD Russian patent published in 2000 - IPC

Abstract RU 2151882 C1

FIELD: mechanical engineering; repair of rotor parts of gas turbine engine. SUBSTANCE: method includes removal of defective element of part and finishing. According to this method axial flange fastening disk on turbine shaft with three dimensional defect is cut off, hole is made in disk plate for fastening element, and disk is connected to shaft means of additional inclined flange. EFFECT: reduced cost of repair of highly loaded parts of turbine rotor with three-dimensional defects by excluding rejection and replacement of parts. 3 dwg

Similar patents RU2151882C1

Title Year Author Number
MULTISTAGE TURBINE ROTOR 2002
  • Fadeev S.I.
  • Sychev V.K.
  • Trushnikov A.P.
  • Jazev V.M.
RU2230195C2
GAS-TURBINE ENGINE WITH TWO-STAGE GAS TURBINE 2002
  • Ivanov V.V.
  • Kuznetsov V.A.
RU2224892C2
ONE-SHAFT GAS-TURBINE PLANT 1999
  • Inozemtsev A.A.
  • Sulimov D.D.
  • Kuznetsov V.A.
  • Toropchin S.V.
RU2180043C2
ROTOR SHAFT OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE 2014
  • Simonov Sergej Anatol'Evich
  • Erichev Dmitrij Jur'Evich
  • Zubarev Gennadij Ivanovich
  • Uzbekov Andrej Valer'Evich
  • Kuznetsov Igor' Sergeevich
RU2565090C1
ROTOR SHAFT OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, SPACER OF CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE 2014
  • Marchukov Evgenij Juvenal'Evich
  • Poljakov Konstantin Sergeevich
  • Erichev Dmitrij Jur'Evich
  • Selivanov Nikolaj Pavlovich
RU2565141C1
ATTACHMENT UNIT FOR SECURING DISK OF TURBOMACHINE TO SHAFT 1992
  • Ivanov N.A.
  • Pykhtin Ju.A.
  • Chernjaev I.A.
RU2042832C1
TURBINE OF GAS-TURBINE ENGINE 2002
  • Ivanov V.V.
  • Kuznetsov V.A.
RU2232901C2
ROTOR SHAFT OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, SPACER OF CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE 2014
  • Poljakov Konstantin Sergeevich
  • Erichev Dmitrij Jur'Evich
  • Uzbekov Andrej Valer'Evich
  • Selivanov Nikolaj Pavlovich
RU2565133C1
TURBINE ROTOR OF GAS-TURBINE ENGINE 1999
  • Kuznetsov V.A.
  • Ivanov V.V.
RU2162947C2
MULTISTAGE TURBINE ROTOR 1996
  • Inozemtsev A.A.
  • Ivanov N.A.
  • Pavlov E.K.
  • Jazev V.M.
  • Kuznetsov V.A.
  • Fadeev S.I.
RU2130124C1

RU 2 151 882 C1

Authors

Inozemtsev A.A.

Pavlov E.K.

Jazev V.M.

Kuznetsov V.A.

Vesnina L.B.

Dates

2000-06-27Published

1998-08-03Filed