TURBINE BLADE AND PROCEDURE FOR ITS MANUFACTURE Russian patent published in 2015 - IPC F01D5/22 

Abstract RU 2541078 C2

FIELD: machine building.

SUBSTANCE: turbine blade contains a vertex section with a shroud and, at least, one rim facing radially from the shroud. The edge has the first and second side walls spaced apart with reference to each other and joined with the shroud, and also a cutting edge, joined with the first and second side walls, forming a cavity between the side walls, the shroud and the cutting edge. The cutting edge is arranged with reference to the first and second side walls in a radial direction. The width of the first side wall and second side wall is constant in a radial direction, at least, up to 50% of height of the named side walls. The fabrication of the named turbine blade includes the one-piece-casting of the blade with hollow rim with the first and second side walls and the cutting edge, or the named blade is stamped and the edge is machine processed for formation of the first and second side walls, cutting edge and cavity between them.

EFFECT: invention allows to decrease a mass of a turbine blade without worsening its durability and reliability.

10 cl, 11 dwg

Similar patents RU2541078C2

Title Year Author Number
METHOD AND COOLING SYSTEM FOR COOLING BLADES OF AT LEAST ONE BLADE RIM IN ROTARY MACHINE 2013
  • Yustl Sasha
  • Simon-Delgado Karlos
  • Khajdekke Aksel
  • Olmes Sven
RU2592095C2
TURBINE IMPELLER 2021
  • Igarashi, Shota
  • Watanabe, Yasuyuki
  • Murakata, Tadashi
  • Sakamoto, Yoshiki
RU2760412C1
METHOD OF HEAT INSULATION OF TURBINE BLADE (VERSIONS) AND DEVICE FOR OBTAINING BLADE PROFILE 1993
  • Gokhshtejn Jakov Petrovich
  • Gokhshtejn Aleksandr Jakovlevich
RU2086775C1
GAS TURBINE BLADE 2011
  • Bregman Vitalij
  • Petukhovskij Mikhail
RU2573085C2
METHOD OF COOLING THE ROTOR OF A HIGH PRESSURE TURBINE (HPT) OF GAS TURBINE ENGINE (GTE), HPT ROTOR AND HPT ROTOR BLADE COOLED BY THIS METHOD, KNOT OF THE DEVICE OF TWISTING OF AIR OF HPT ROTOR 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Selivanov Nikolaj Pavlovich
RU2684298C1
WORKING WHEEL OF AXIAL TURBO-MACHINE 1992
  • Shul'Ga Vladimir Petrovich
RU2039871C1
TURBINE COOLED BADE AND APPROPRIATE TURBINE 2011
  • Batt Stefen
  • Pehjsi Ehndi
RU2573096C2
TURBINE BLADE AND METHOD OF ASSEMBLY OF TURBINE ROTOR WITH SUCH BLADE 2009
  • Kim Khun Dong
  • Dumitrasku Marius
  • Grinspen Majkl Evgenij
  • Kang Ungmo
  • Kim Eng Veon
RU2517992C2
BLADE ROOT, CORRESPONDING BLADE, ROTOR DISC AND TURBOMACHINE UNIT 2012
RU2612675C2
TURBINE WHEEL OF AXIAL TURBOMACHINE 2000
  • Shul'Ga V.P.
RU2203428C2

RU 2 541 078 C2

Authors

Brandl' Gerbert

Tsypkajkin Igor'

Indlekofer Filipp

Dates

2015-02-10Published

2011-04-06Filed