METHOD OF INCREASING COMPRESSOR EFFICIENCY Russian patent published in 2008 - IPC F04D29/10 

Abstract RU 2327061 C1

FIELD: compressor building; gas turbine building; engine building; electrical machinery building.

SUBSTANCE: invention allows to use an aerodynamic labyrinth-screw seal that can create a counter flow to gases leaking through gaps in running shafts. Unlike mechanical, oil, dry gas and other seals, the proposed method of aerodynamic sealing makes the only technique to completely rule out leaning through in compressors, gas turbine plants, aircraft gas turbine engines. This invention has managed to define a proper arrangement of aerodynamic labyrinth-screw seals and the conditions wherein the oil running through the front bearing assembly and oil ingress onto the blades and into the compressor setting are ruled out as well as gas leaking around inside the compressor.

EFFECT: increase in efficiency and capacity.

10 cl, 3 dwg

Similar patents RU2327061C1

Title Year Author Number
AERODYNAMIC LABYRINTH SCREW SEALING 2000
  • Bagdasarjan V.S.
  • Bagdasarjan S.V.
RU2193698C2
GAS-TURBINE PLANT AERODYNAMIC LABYRINTH SCREW SEAL 1998
  • Bagdasarjan V.S.
  • Bagdasarjan S.V.
RU2133345C1
GAS-TURBINE PLANT DELIVERING WORKING MIXTURE TO CONSUMER FOR USE IN CHEMICAL PROCESS AFTER WHICH WORKING MIXTURE IS RETURNED INTO PLANT GAS TURBINE 1997
  • Chernomordik L.I.
  • Bagdasarjan V.S.
  • Ryzhkov V.S.
  • Bagdasarjan S.V.
RU2119589C1
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE 2016
  • Marchukov Evgenij Yuvenalevich
  • Ilyasov Sergej Anatolevich
  • Kuprik Viktor Viktorovich
  • Konovalova Tamara Petrovna
  • Polyakov Konstantin Sergeevich
  • Savchenko Aleksandr Gavrilovich
  • Skaryakina Regina Yurevna
  • Selivanov Nikolaj Pavlovich
RU2614708C1
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE 2016
  • Marchukov Evgenij Yuvenalevich
  • Erichev Dmitrij Yurevich
  • Ilyasov Sergej Anatolevich
  • Kuprik Viktor Viktorovich
  • Savchenko Aleksandr Gavrilovich
  • Shishkova Olga Vladimirovna
  • Selivanov Nikolaj Pavlovich
RU2614709C1
CENTRIFUGAL COMPRESSOR 2007
  • Gorozhantsev Vladimir Vladimirovich
  • Kas'Janov Sergej Vladimirovich
  • Riznyk Roman Sergeevich
RU2338095C1
CENTRIFUGAL COMPRESSOR 2005
  • Gorozhantsev Vladimir Vladimirovich
  • Logunov Sergej Borisovich
RU2289729C1
GAS TURBINE ENGINE 2001
  • Ivanov V.V.
  • Kuznetsov V.A.
RU2211935C2
CENTRIFUGAL COMPRESSOR 1998
  • Smol'Nikov V.V.
  • Sokolovskij M.I.
  • Shcherbakov Ju.N.
  • Gorozhantsev V.V.
  • Glushkov B.K.
RU2140577C1
COMPRESSOR AND GAS-TURBINE ENGINE 1989
  • Ponomarev B.A.
  • Tikhonov A.M.
  • Shalashov N.D.
RU2110700C1

RU 2 327 061 C1

Authors

Bagdasarjan Vazgen Sergeevich

Bagdasarjan Sergej Vazgenovich

Dates

2008-06-20Published

2007-04-11Filed