STEAM TURBINES HIGH-TEMPERATURE STUD PINS REFRIGERATION METHOD AND DEVICE FOR ITS ACTUALIZATION Russian patent published in 2018 - IPC F01D5/08 

Abstract RU 2641782 C2

FIELD: electricity-producing industry.

SUBSTANCE: invention relates to the method and device for the case high-temperature stud pins refrigeration and the flanged joints of the steam turbines of the thermal power stations (TPS, CHP), more specifically for the high-temperature stud pin of the flange connectors of the high-pressure cylinder (HPC) seal, and can be used in the stud pins refrigerating systems of the turbines of a ST-type. The assigned technical problem in the steam turbines high-temperature stud pins refrigeration method, which includes the cooling steam supply along the cooling line from the flowing channel on one side and the cooling steam removal along the outlet line on the other side is achieved by means of the fact that the steam extraction is carried out from the medium or low-pressure stage of the steam turbine with subsequent direction of the extracted steam for the steam turbines high-temperature stud pins refrigeration. Upon that, the extracted steam flow velocity control is effected on account of the isolation valve adjustment on the extraction steam line from the low or medium pressure stage of the steam turbine, and the extracted steam temperature control is effected on account of the steam extraction from the low or medium pressure stage of the steam turbine. Further, the extracted steam is transferred through the cylindrical connecting leg into the cylindrical metal tube of a minor diameter and then after the distribution in a volume the extracted steam runs into the cooling cylindrical conduit, where the extracted steam is supplied through the perforation hole in the cylindrical metal tube of a minor diameter into the cooling cylindrical conduit, where it removes a part of the heat from the internal surface of the external cylindrical tube of a greater diameter and the steam heats up as consequence of the heat loss. At this time, the extracted steam cools down the external cylindrical metal tube walls of a greater diameter, and further, the steam is forced out into the outlet cylindrical connecting leg and further either goes back into the steam turbine plant cycle or to the atmosphere. The cooling cylindrical conduit is formed by two cylindrical metal tubes with bases that have the common normal axis. Along with this, the cylindrical metal tube of a minor diameter has the perforation hole and is linked to the cylindrical connecting leg, and the external cylindrical metal tube of a greater diameter is linked to the outlet cylindrical connecting leg.

EFFECT: reduction in expenditure, thermal efficiency increase.

4 cl, 3 dwg

Similar patents RU2641782C2

Title Year Author Number
GAS-DRIVEN TURBINES HIGH-TEMPERATURE STUD PINS REFRIGERATION METHOD AND DEVICE FOR ITS ACTUALIZATION 2016
  • Kantyukov Rafael Rafkatovich
  • Takhaviev Marat Safautdinovich
  • Lebedev Ruslan Vladimirovich
  • Shenkarenko Sergej Viktorovich
  • Avzalov Razil Kamilevich
RU2641787C2
LAST STAGE OF STEAM TURBINE 2016
  • Lisyanskij Aleksandr Stepanovich
  • Usachev Konstantin Mikhajlovich
  • Ananina Svetlana Borisovna
RU2614316C1
METHOD FOR REMOVAL OF MOISTURE FROM PERIPHERAL ZONE OF STEAM TURBINE AND LABYRINTH SHROUD SEAL FOR STAGES OF STEAM TURBINES OPERATING IN WET STEAM MEDIUM 2021
  • Lisianskii Aleksandr Stepanovich
  • Smyslov Anatolii Mikhailovich
  • Galiakbarov Ruslan Fanilevich
  • Bolshakov Boris Olegovich
  • Mingazhev Askar Dzhamilevich
RU2784635C1
STEAM TURBINE 2006
  • Vigkhardt Kaj
RU2410545C2
METHOD OF COOLING AND REGULATING RADIAL CLEARANCES OF TURBINE OF DOUBLE-FLOW GAS TURBINE ENGINE AND DEVICE FOR IMPLEMENTATION THEREOF 2020
  • Bolotin Nikolaj Borisovich
RU2732653C1
CONTROL METHOD OF RADIAL CLEARANCES OF TURBINE OF DOUBLE-FLOW GAS TURBINE ENGINE AND DEVICE FOR IMPLEMENTATION THEREOF 2020
  • Bolotin Nikolaj Borisovich
RU2738523C1
SYSTEM OF LIQUID COOLING OF POWER GAS TURBINE HIGH-TEMPERATURE STAGE BLADES 2012
  • Balashov Jurij Arkad'Evich
  • Beljakov Anatolij Vasil'Evich
  • Berezinets Pavel Andreevich
  • Taradaj Dmitrij Vadimovich
RU2500893C1
COOLED NOZZLE BLADE OF A HIGH-PRESSURE TURBINE OF A TURBOJET ENGINE 2021
  • Ponosova Natalya Vasilevna
  • Popov Denis Andreevich
  • Serebrich Georgij Petrovich
  • Sychev Vladimir Konstantinovich
  • Faskhutdinov Rustam Nailevich
RU2767580C1
GAS TURBINE ENGINE TURBINE ROTOR 2010
  • Sychev Vladimir Konstantinovich
  • Jazev Vladimir Mikhajlovich
  • Kuznetsov Valerij Alekseevich
RU2453709C1

RU 2 641 782 C2

Authors

Kantyukov Rafael Rafkatovich

Takhaviev Marat Safautdinovich

Lebedev Ruslan Vladimirovich

Shenkarenko Sergej Viktorovich

Avzalov Razil Kamilevich

Dates

2018-01-22Published

2016-05-30Filed