SYSTEM TO BALANCE ROTOR OF GAS TURBINE PLANT, ROTOR DISC AND STRUCTURAL UNIT COMPRISING SUCH SYSTEM AND GAS TURBINE PLANT Russian patent published in 2012 - IPC F01D5/02 

Abstract RU 2447291 C2

FIELD: machine building.

SUBSTANCE: system to balance a gas turbine plant rotor comprises a balancing grip, including several through holes. The system also comprises several balancing weights, every of which is firmly fixed on a balancing grip by means of the first and second screw/nut pairs, comprising the first screw and the second screw, which are installed in the first and second holes that directly follow each other. Each hole has the first and second side surfaces, which are located at one and other side from the screw included into the appropriate screw/nut pair. The second side surface is displaced relative to the first side surface in the first direction, and the first through hole is displaced relative to the second through hole in the second direction, which is opposite to the first one. The first screw rests against the first side surface of the first through hole and is located at the distance from the second side surface. The second screw rests against the second side surface of the second through hole and is located at the distance from the first side surface. Other subjects of the invention are a gas turbine plant rotor disc and a structural unit, comprising the above described balancing system, and also a gas turbine plant comprising a structural unit.

EFFECT: inventions make it possible to increase time of balancing grip usage and reduce risk of its damage.

14 cl, 5 dwg

Similar patents RU2447291C2

Title Year Author Number
GAS TURBINE PLANT ROTOR BALANCING SYSTEM; ROTOR DISC AND STRUCTURAL ASSEMBLY, WHICH CONTAIN SUCH SYSTEM, AND GAS TURBINE PLANT 2007
  • Blanshar Stefan P'Er Gijom
  • Garehn Fabris
  • Zhjude Moris Gi
  • Lanzheven Toma
RU2448257C2
GAS TURBINE ENGINE COMPRESSOR ROTOR ASSEMBLY WITH BALANCING SYSTEM 2013
  • Maskat, Kori, Patrik
  • Makdonald, Laura, Elizabet
  • Miller, Dzhejms, Erik
  • Vavrek, Geri, Pol
RU2660981C2
GAS TURBINE BLOWER WITH BALANCING SYSTEM WITH DEAD HOLES TO ACCOMMODATE WEIGHTS 2009
  • Bel'Mont Oliv'E
  • Veller Lionel' Rene Anri
RU2511767C2
ROTOR DISK OF GAS-TURBINE ENGINE (VERSIONS) 2001
  • Forrester Dzhejms Majkl
  • Bolt Zhanin Ehlizabet
  • Roda Dzhejms Ehdvin
  • Stivenson Dzhozef Timoti
RU2281420C2
DEVICE FOR MECHANICAL CONTROL OF RADIAL CLEARANCE BETWEEN ENDS OF ROTOR BLADES AND STATOR OF COMPRESSOR AND GAS TURBINE ENGINE TURBINE, METHOD OF CONTROLLING RADIAL CLEARANCE BETWEEN ENDS OF ROTOR BLADES AND STATOR OF COMPRESSOR AND GAS TURBINE ENGINE TURBINE 2017
  • Eskin Izold Davidovich
  • Startsev Nikolaj Ivanovich
  • Falaleev Sergej Viktorinovich
RU2702063C2
FLANGED COMPONENT FOR GAS TURBINE ENGINE 2017
  • Struck, Bruno E.
RU2742013C2
DEVICE LOCKING RING SEAL ON TURBINE DISK OF GAS TURBINE ENGINE, RING SEAL OF BLADES COOLING CIRCUIT, TURBINE MODULE OF GAS TURBINE ENGINE AND GAS TURBINE ENGINE 2011
  • Bosko Frank Ehmmanjuehl'
RU2563411C2
GAS TURBINE ENGINE (VERSIONS) 2014
  • Finneran Dzhon U.
  • Graber Deril Dzh.
  • Ligon Dzhonatan M.
  • Munshi Mrinal
  • Porter Mettyu R.
  • Shtejman Evgenij P.
RU2639921C2
SMALL-SIZE GAS TURBINE PLANT 2024
  • Smelov Vitalij Gennadevich
  • Tkachenko Andrej Yurevich
  • Shimanov Artem Andreevich
  • Vinogradov Aleksandr Sergeevich
  • Filinov Evgenij Pavlovich
  • Baturin Oleg Vitalevich
  • Zubrilin Ivan Aleksandrovich
RU2819326C1
UNIT OF GAS TURBINE ENGINE, MODULE OF GAS TURBINE ENGINE AND GAS TURBINE ENGINE 2008
  • Drelon Godfrua Fransis Frederik
  • Pabion Filipp Zhan-P'Er
  • Prestel' Sebast'En Zhan Loran
  • Supizon Zhan-Ljuk
RU2482304C2

RU 2 447 291 C2

Authors

Blanshar Stefan P'Er Gijom

Garehn Fabris

Zhjude Moris Gi

Lanzheven Toma

Dates

2012-04-10Published

2007-10-23Filed