AXIAL TURBOMACHINE WHEEL Russian patent published in 1994 - IPC

Abstract RU 2022120 C1

FIELD: manufacture of turbomachines. SUBSTANCE: wheel has disk made integral with blades; rim of this disk is provided with slot receiving the damping element. Slot is circular in form and is inclined relative to vertical axis of the disk. Damping element is made in form of multi-layer circular stack of alternating plain and corrugated plates and is mounted in slot at a negative allowance. EFFECT: enhanced efficiency. 2 dwg

Similar patents RU2022120C1

Title Year Author Number
ROTOR OF AIRCRAFT GAS-TURBINE ENGINE COMPRESSOR WITH TWIN OF BLISKS AND TWIN OF BLISK WITH CLASSIC IMPELLER AND WITH TWIN OF CLASSIC IMPELLER WITH IMPELLER WITH FOURTH-TO-SIXTH STAGE WITH DEVICES FOR DAMPING VIBRATIONS OF WORKERS OF THESE CLIPS AND IMPELLERS, FAN ROTOR AND BOOSTER ROTOR WITH DEVICE FOR DAMPING OF VIBRATIONS OF WORKING WIDE CHORD BLADES OF FAN, TWIN ASSEMBLY METHOD WITH DAMPER DEVICE 2016
  • Eskin Izold Davidovich
  • Ermakov Aleksandr Ivanovich
  • Garshin Egor Alekseevich
RU2665789C2
TURBINE WHEEL 2010
  • Kostogryz Valentin Grigor'Evich
  • Kosholap Jurij Grigor'Evich
  • Vigant Vladimir Sergeevich
  • Klimov Vitalij Nikolaevich
  • Radchenko Vladimir Aleksandrovich
RU2433277C1
TURBO MACHINE WHEEL 2010
  • Kostogryz Valentin Grigor'Evich
  • Kosholap Jurij Grigor'Evich
  • Vigant Vladimir Sergeevich
  • Klimov Vitalij Nikolaevich
  • Radchenko Vladimir Aleksandrovich
RU2433278C1
DAMPER 1991
  • Еhskin I.D.
  • Рronichev Ju.N.
RU2020311C1
PLACE OF MOUNTING OF WORKING BLADES OF BOOSTER ROTORS AND COMPRESSOR OF AVIATION ENGINES OF FIFTH GENERATION; BOOSTER ROTOR AND ROTOR OF HIGH PRESSURE COMPRESSOR OF FIRST GENERATION AVIATION ENGINE, WITH WORKING BLADES, FIXED WITH HELP OF SWALLOWTAIL TYPE LOCKS IN RING GROOVES OF THESE DEVICES; METHOD OF ASSEMBLING PLACE OF MOUNTING WORKING BLADES OF BOOSTER ROTORS AND COMPRESSOR 2016
  • Eskin Izold Davidovich
  • Ermakov Aleksandr Ivanovich
  • Garshin Egor Alekseevich
RU2662755C2
VIBRATION DAMPING DEVICE OF BLISK IMPELLERS OF GAS TURBINE ENGINE 2015
  • Gabov Ivan Georgievich
  • Berendorf Jurij Aleksandrovich
  • Balakirev Aleksandr Andreevich
  • Nikhamkin Mikhail Shmerovich
  • Golovkin Andrej Jurevich
  • Sazhenkov Nikolaj Alekseevich
  • Voronov Leonid Vasilevich
  • Khaljapin Aleksandr Alekseevich
  • Konev Ivan Petrovich
  • Semenov Sergej Valerevich
RU2583205C1
HYDRODYNAMIC DAMPER 2000
  • Baljakin V.B.
RU2179666C2
LONG HOLLOW WIDE CHORD FAN BLADE AND METHOD OF ITS MANUFACTURE 2016
  • Eskin Izold Davidovich
  • Ermakov Aleksandr Ivanovich
RU2626523C1
PLACE OF MOUNTING OF WORKING BLADES AND LOW AND HIGH PRESSURE COMPRESSOR OF AVIATION ENGINES OF FIFTH GENERATION, ROTOR OF LOW PRESSURE COMPRESSOR AND ROTOR OF HIGH PRESSURE COMPRESSOR OF FIFTH GENERATION AVIATION ENGINE, WITH WORKING BLADES, FIXED WITH HELP OF DOVETAIL TYPE LOCKS IN RING GROOVES OF THESE DEVICES, METHOD OF ASSEMBLING PLACE OF MOUNTING WORKING BLADES OF ROTORS AND COMPRESSOR 2017
  • Eskin Izold Davidovich
  • Garshin Egor Alekseevich
  • Ermakov Aleksandr Ivanovich
RU2686353C2
AIRCRAFT TURBOJET ENGINE FAN ROTOR WITH LONG WIDE-CHORD HOLLOW BLADES WITH DAMPERS 2019
  • Eskin Izold Davidovich
  • Falaleev Sergej Viktorinovich
RU2727314C1

RU 2 022 120 C1

Authors

Frolov V.A.

Malyshev S.Ju.

Malysheva A.V.

Dates

1994-10-30Published

1991-06-05Filed