COOLED ROTOR PERFORATED TURBINE BLADE Russian patent published in 2016 - IPC F01D5/18 

Abstract RU 2582539 C1

FIELD: manufacturing technology.

SUBSTANCE: cooled working perforated turbine blade shell comprises a perforated with small diameter cooling holes curved shape. Middle line of each of cooling holes is located in plane of vane along blade and normal to surface contour of blade profile.

EFFECT: higher cooling efficiency of turbine blade and higher reliability and service life.

1 cl, 4 dwg

Similar patents RU2582539C1

Title Year Author Number
COOLED PERFORATED TURBINE BLADE 2013
  • Trushin Vladimir Alekseevich
  • Trushin Oleg Vladimirovich
RU2544916C1
TURBINE BLADE 1993
  • Gokhshtejn Jakov Petrovich
  • Gokhshtejn Aleksandr Jakovlevich
RU2076928C1
GAS TURBINE ENGINE COOLED BLADE 2014
  • Tumakov Aleksej Grigor'Evich
  • Bajgaliev Boris Ergazovich
RU2568600C1
COOLED PERFORATED BLADE OF TURBOMACHINE WITH HEAT BARRIER COATING 2004
  • Trushin Vladimir Alekseevich
RU2286463C2
CONTINUOUS TRANSIENT CHANNEL BETWEEN HIGH-PRESSURE TURBINE AND LOW-PRESSURE TURBINE OF DOUBLE-FLOW AIRCRAFT ENGINE 2011
  • Gladkov Jurij Igorevich
  • Baranovskij Boris Viktorovich
RU2484264C2
METHOD OF REPAIRING AIRFOIL OF COOLED WORKING BLADES OF GAS TURBINE ENGINES FROM HEAT-RESISTANT ALLOYS BY LASER POWDER SURFACING 2023
  • Zadykian Grigorii Grigorovich
  • Korsmik Rudolf Sergeevich
RU2823420C1
WORKING BLADE OF THE GAS TURBINE 2017
  • Leontev Valerij Vladimirovich
RU2656052C1
GAS TURBINE BLADE WITH CONVECTIVE COOLING SYSTEM 2016
  • Balaban Yurij Nikolaevich
  • Kuprik Viktor Viktorovich
  • Marchukov Evgenij Yuvenalevich
  • Pushkin Yurij Nikolaevich
  • Chernyj Mstislav Sergeevich
RU2627879C1
TURBINE BLADE 2007
  • Kuznetsov Valerij Alekseevich
RU2346164C2
TURBINE BLADE 1993
  • Gokhshtejn Jakov Petrovich
  • Gokhshtejn Aleksandr Jakovlevich
RU2088764C1

RU 2 582 539 C1

Authors

Gishvarov Anas Saidovich

Trushin Vladimir Alekseevich

Dates

2016-04-27Published

2015-05-20Filed