HIGH-PRESSURE TURBINE SUPPORT Russian patent published in 2017 - IPC F01D25/16 

Abstract RU 2612546 C1

FIELD: oil and gas industry.

SUBSTANCE: present invention relates to a turbine and can be used in the construction of gas turbine installations, in particular elements of support and thrust bearings. Prop high pressure turbine includes an outer casing, an inner ring connected in series, the bearing housing and roller cooperating with a turbine rotor, blade, nozzle, needle, sleeve and locking nuts. Needles are fixed on one end of the outer housing, and the other end on the inner ring. Bushings are designed as a cup with an opening in the bottom of the spokes. Sleeves are secured on the inner ring and the spokes are made beads. Each spoke is set in a hole in the bottom and the cup is provided with two pairs of washers with spherical surfaces. One pair of washers is mounted on the needle between the flange and the spokes on one side of the bottom cup and the other, between the other side of the bottom cup and the locking nut.

EFFECT: increase of the gas turbine resources of the high pressure turbine plant.

2 dwg

Similar patents RU2612546C1

Title Year Author Number
HIGH-PRESSURE TURBINE SUPPORT 2015
  • Butskij Aleksandr Anatolevich
  • Zykunov Yurij Iosifovich
  • Kanakhin Yurij Aleksandrovich
  • Maksimov Vadim Vasilevich
RU2596902C1
NOZZLE ASSEMBLY OF LOW-PRESSURE TURBINE (LPT) OF GAS TURBINE ENGINE (GTE) (VERSIONS) AND BLADE OF LPT NOZZLE ASSEMBLY (VERSIONS) 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Krylov Nikolaj Vladimirovich
  • Ryabov Evgenij Konstantinovich
  • Zolotukhin Andrej Aleksandrovich
RU2691203C1
NOZZLE APPARATUS OF A HIGH-PRESSURE TURBINE OF A GAS TURBINE ENGINE 2020
  • Kuzmin Maksim Vladimirovich
  • Khanin Aleksandr Anatolevich
RU2757245C1
TURBINE PEDESTAL OF GAS TURBINE ENGINE 2006
  • Rajkov Jurij Vasil'Evich
  • Polubojarinova Svetlana Anatol'Evna
  • Prokof'Ev Valentin Vasil'Evich
RU2326251C1
TURBINE MACHINE TURBINE SUPPORT 2019
  • Gusenko Sergej Mikhajlovich
  • Zajdullin Danis Amirovich
  • Makarychev Anton Sergeevich
RU2724074C1
METHOD FOR COOLING OF NOZZLE ASSEMBLY OF A LOW-PRESSURE TURBINE (LPT) OF A GAS TURBINE ENGINE AND A LPT NOZZLE ASSEMBLY WHICH IS COOLED BY THIS METHOD, A METHOD FOR COOLING A BLADE OF LPT NOZZLE ASSEMBLY AND A NOZZLE ASSEMBLY BLADE, COOLED BY THIS METHOD 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Krylov Nikolaj Vladimirovich
  • Selivanov Nikolaj Pavlovich
RU2691202C1
TURBOJET ENGINE CONTROL DEVICE 2008
  • Cheremushkin Oleg Vasil'Evich
RU2371595C1
ROTARY PUMP WITH GAP-FREE ATTACHMENT OF IMPELLER AND END SEALS TO ROTOR SHAFT AND METHOD OF IMPROVING PUMP PERFORMANCES 2011
  • Rjakhovskij Oleg Anatol'Evich
  • Oboznyj Jurij Sergeevich
  • Kushnarev Vladimir Ivanovich
  • Gus'Kov Aleksandr Mikhajlovich
RU2487272C1
TURBO-JET ENGINE WITH COMBINED SUPPORT OF LOW AND HIGH PRESSURE TURBINE 2009
  • Belousov Viktor Alekseevich
  • Demkin Nikolaj Borisovich
RU2414614C1
MAIN OIL ELECTRIC PUMP UNIT, AND METHOD FOR IMPROVEMENT OF UNIT CHARACTERISTICS 2011
  • Rjakhovskij Oleg Anatol'Evich
  • Oboznyj Jurij Sergeevich
  • Kushnarev Vladimir Ivanovich
  • Gus'Kov Aleksandr Mikhajlovich
  • Petrov Aleksej Igorevich
RU2484305C1

RU 2 612 546 C1

Authors

Dates

2017-03-09Published

2015-10-13Filed