TURBINE ROTOR FOR THERMAL POWER PLANT AND METHOD OF ITS ASSEMBLY Russian patent published in 2015 - IPC F01D5/30 

Abstract RU 2547679 C2

FIELD: electricity.

SUBSTANCE: turbine rotor of a thermal power plant contains a set of blades, a rotor disk and a fixing device. The rotor disk is attached to the shaft and has on the periphery the ledges to which the blades are attached. The rotor disk has a groove open towards the axial direction and having the bottom and top surfaces, and the bottom surface of the groove is located on the rotor disk periphery, and the top surface of the groove is located on ledges and faces towards the bottom surface. The groove of the rotor disk has in the area of its ledges an axial section with a deepening and an open section on which the groove is open towards the axial direction, and the radial width of the deepening is greater, than the radial width of the open section. Each blade has the shank lateral ledge having on the lower part a groove with the top surface located after the top surface of the rotor disk groove. The fixing device is installed in the rotor disk groove for fixing of blades. During assembly of the named turbine rotor the blades are installed between rotor disk ledges, and in the rotor disk groove and in the blade groove the bottom and top profiles are installed. Then the intermediate closing element is installed for strong pressing of bottom and top profiles respectively to the bottom surface of the rotor disk groove and to the top surfaces of the rotor disk groove and grooves of blades.

EFFECT: group of inventions allows to increase service life of the turbine rotor and to simplify a design of fixing devices.

7 cl, 12 dwg

Similar patents RU2547679C2

Title Year Author Number
FAN, IN PARTICULAR, FOR TURBINE ENGINE 2014
  • Perdrizhon Kristof
  • Yablonski Loren
  • Zholi Filipp Zherar Edmon
RU2677769C1
AXIAL-FLOW TURBOMACHINE RUNNER 2005
  • Solov'Ev Aleksandr Fedorovich
RU2296864C1
BLADE ROOT, CORRESPONDING BLADE, ROTOR DISC AND TURBOMACHINE UNIT 2012
RU2612675C2
GAS TURBINE ENGINE WORKING WHEEL OF ROTOR 2018
  • Dontsov Sergej Nikolaevich
  • Kikot Nikolaj Vladimirovich
  • Uzbekov Andrej Valerevich
RU2682217C1
CLAMP FOR BLADE WITH T-SHAPE FASTENER, APPROPRIATE COMPRESSOR DISC, COMPRESSOR AND TURBO MACHINE 2009
  • Bel'Mont Oliv'E
  • Bosko Frank Ehmmanjuehl'
RU2515572C2
ROTARY ASSEMBLY FOR TURBINE ENGINE COMPRISING SELF-SUPPORTING ROTOR CASING 2015
  • Marsal, David
  • Leduc, Mathieu, Louis, Jean
  • Groleau, Claire, Charlotte
  • Carlos, Pierre-Louis, Alexandre
  • Evain, Gael, Frederic, Claude, Cyrille
RU2712560C2
SYSTEM FOR AXIAL FIXATION OF WORKING BLADES IN ROTOR, PACKING ELEMENT FOR SUCH SYSTEM, AND ALSO IMPLEMENTATION OF THIS SYSTEM 2006
  • Brillert Diter
  • Khell' Kharal'D
  • Khjul'Fenkhaus Armin
  • Fegelin Klaus
RU2413073C2
DEVICE WITH CENTRIFUGAL SEPARATOR 2012
  • Andersson Ajinger Tomas
RU2554587C1
SEAL RING FOR TURBINE STAGE AIRCRAFT TURBINE MACHINE CONTAINING SHUTOFF PROJECTIONS WITH SLOTS, ROTOR STAGE OF TURBOMACHINE, TURBOMACHINE AND METHOD OF MAKING SEALING RING 2012
  • Puze Emili
  • Kazalidzhi Paskal
  • Paske Dide
RU2594392C2
DEVICE FOR MOUNTING AND LOCKING OF ROTOR BLADES IN AXIAL-FLOW COMPRESSOR 2002
  • Arinchi Paolo
  • Bachchiottini Karlo
RU2296889C2

RU 2 547 679 C2

Authors

Berk'E Kristof

Bato Andre

Dates

2015-04-10Published

2013-03-14Filed