TURBO MACHINE BLADE TEST DEVICE Russian patent published in 2013 - IPC G01N29/04 

Abstract RU 2490626 C1

FIELD: instrument making.

SUBSTANCE: proposed device comprises turbine bladed wheel, turbine blade butts are locked in disc annular disc. At least, one blade is a tested blade. This device comprises also transducer and electric conductors. Said conductors are secured at blade body and root surfaces and in flange hole, connected to said transducer secured at blade body and means to transmit signal to recording device. Said transducer is composed of resistive-strain sensor. Annular groove bottom has, at least, one recess and two holes communicated therewith for wiring conductors at disc face and rear. Recess length makes, at least, half the blade root thickness. Note here that connection of conductors is made at disc face side, said wires running from transducer and signal transmitter. Recess depth should make, at least, two diameters of electric conductors. Note that the number of recesses communicated with annular disc groove being equal to that of tested blades.

EFFECT: simplified design, higher accuracy of testing, better balancing and longer life of turbine.

3 cl, 2 dwg

Similar patents RU2490626C1

Title Year Author Number
STAND FOR CORROSION-STRENGTH TESTS OF GAS TURBINE ENGINE BLADE 2019
  • Andryushkin Aleksandr Yurevich
  • Levikhin Artem Alekseevich
  • Meshcheryakov Stanislav Andreevich
  • Kirshin Anton Yurevich
  • Kirshina Alena Andreevna
RU2724295C1
GAS TURBINE ENGINE LOW-PRESSURE COMPRESSOR ROTOR SECOND STAGE DISC (VERSIONS) 2015
  • Balaban Jurij Nikolaevich
  • Kuprik Viktor Viktorovich
  • Manapov Irik Usmanovich
  • Uzbekov Andrej Valerevich
  • Kuznetsov Igor Sergeevich
RU2603218C1
TURBOJET LOW-PRESSURE COMPRESSOR FIRST STAGE DISC 2014
  • Marchukov Evgenij Juvenal'Evich
  • Simonov Sergej Anatol'Evich
  • Erichev Dmitrij Jur'Evich
  • Chepkin Viktor Mikhajlovich
RU2565136C1
GAS TURBINE ENGINE LOW-PRESSURE COMPRESSOR ROTOR THIRD STAGE DISC (VERSIONS) 2015
  • Kuprik Viktor Viktorovich
  • Kondrashov Igor Aleksandrovich
  • Konovalova Tamara Petrovna
  • Marchukov Evgenij Juvenalevich
  • Poljakov Konstantin Sergeevich
  • Kuznetsov Igor Sergeevich
RU2603222C1
TURBOJET LOW-PRESSURE COMPRESSOR SECOND STAGE DISC 2014
  • Erichev Dmitrij Jur'Evich
  • Uzbekov Andrej Valer'Evich
  • Selivanov Nikolaj Pavlovich
RU2565139C1
GAS TURBINE ENGINE LOW-PRESSURE COMPRESSOR ROTOR LAST STAGE DISC 2015
  • Balaban Jurij Nikolaevich
  • Kuprik Viktor Viktorovich
  • Manapov Irik Usmanovich
  • Konovalova Tamara Petrovna
  • Shishkova Olga Vladimirovna
  • Selivanov Nikolaj Pavlovich
RU2603220C1
TURBOJET LOW-PRESSURE COMPRESSOR THIRD STAGE DISC 2014
  • Marchukov Evgenij Juvenal'Evich
  • Simonov Sergej Anatol'Evich
  • Erichev Dmitrij Jur'Evich
  • Uzbekov Andrej Valer'Evich
  • Kuznetsov Igor' Sergeevich
RU2565140C1
GAS TURBINE ENGINE LOW-PRESSURE COMPRESSOR ROTOR FIRST STAGE DISC (VERSIONS) 2015
  • Erichev Dmitrij Jurevich
  • Kuprik Viktor Viktorovich
  • Marchukov Evgenij Juvenalevich
  • Simonov Sergej Anatolevich
  • Poljakov Konstantin Sergeevich
  • Uzbekov Andrej Valerevich
  • Selivanov Nikolaj Pavlovich
RU2603304C1
TURBOMACHINE COMPRESSOR IMPELLER 2013
  • Erichev Dmitrij Jur'Evich
  • Konovalova Tamara Petrovna
  • Uzbekov Andrej Valer'Evich
RU2529279C1
UNIT FOR CONNECTING BLADES WITH ROTOR OF TURBOMACHINE (VERSIONS) 2005
  • Bakuradze Mikhail Viktorovich
  • Ivanov Vitalij Al'Bertovich
  • Koshelev Sergej Alekseevich
  • Gudkov Nikolaj Nikolaevich
  • Ermolaev Vladimir Vladimirovich
RU2296227C1

RU 2 490 626 C1

Authors

Konovalova Tamara Petrovna

Uzbekov Andrej Valer'Evich

Dates

2013-08-20Published

2011-12-22Filed