MULTISTAGE COMPRESSOR Russian patent published in 2005 - IPC

Abstract RU 2265141 C1

FIELD: mechanical engineering; compressors.

SUBSTANCE: invention relates to axial-flow compressors and it can be used in different industries. According to invention, two impellers are installed for rotation in opposite directions coaxially in compressor housing. Carrying disks of impellers are made in form of coaxial rings with fitted-on blades to form coaxially arranged stages successively connected by channels.

EFFECT: provision of high efficiency, reduced overall axial dimensions and mass of compressor.

3 cl, 2 dwg

Similar patents RU2265141C1

Title Year Author Number
COMPRESSOR AND GAS-TURBINE ENGINE 1989
  • Ponomarev B.A.
  • Tikhonov A.M.
  • Shalashov N.D.
RU2110700C1
COMPRESSOR 1993
  • Joakhim Kottsur[De]
  • Frants-Arno Rikhter[De]
  • Ljubomir Turan'Skij[De]
RU2082021C1
AXIAL-CENTRIFUGAL MULTISTAGE COMPRESSOR 2017
  • Voevodin Nikolaj Nikolaevich
RU2659657C1
TURBO-COMPRESSOR 1993
  • Gel'Medov F.Sh.
  • Lokshtanov E.A.
  • Ol'Shtejn L.E.-M.
  • Sidorkin M.A.
RU2034175C1
AXIAL MULTI-STEP COMPRESSOR WITH WATER INJECTION INTO FLOW PART THEREOF 2020
  • Balashov Yurij Arkadevich
  • Berezinets Pavel Andreevich
  • Teplov Boris Dmitrievich
  • Samojlov Vladimir Leonidovich
  • Markina Veronika Nikolaevna
  • Ageev Andrej Vladimirovich
  • Tuz Natalya Evgenevna
  • Lobach Igor Anatolevich
RU2757150C1
CENTRIFUGAL COMPRESSOR DIAPHRAGM 2018
  • Nigmatulin Tagir Robertovich
  • Trushkov Vladislav Ivanovich
  • Yun Vladimir Klimentevich
RU2673650C1
METHOD OF AIRCRAFT LANDING GEAR WHEELS DRIVING AND AIRCRAFT LANDING GEAR WITH DRIVEN WHEELS 2011
  • Ivandaev Sergej Ivanovich
RU2495792C2
STAGE OF TURBOMACHINE 1989
  • Strikitsa Boris Ivanovich
RU2005890C1
ROTOR FORTH STAGE IMPELLER OF HIGH-PRESSURE COMPRESSOR (HPC) OF TURBOJET ENGINE (VERSIONS), HPC ROTOR IMPELLER DISC, HPC ROTOR IMPELLER BLADE, HPC ROTOR IMPELLER BLADE RING 2016
  • Marchukov Evgenij Yuvenalevich
  • Erichev Dmitrij Yurevich
  • Polyakov Konstantin Sergeevich
  • Syroezhkin Oleg Vasilevich
  • Selivanov Nikolaj Pavlovich
RU2630919C1
ROTOR EIGHTH STAGE IMPELLER OF HIGH-PRESSURE COMPRESSOR (HPC) OF TURBOJET ENGINE (VERSIONS), HPC ROTOR IMPELLER DISC, HPC ROTOR IMPELLER BLADE, HPC ROTOR IMPELLER BLADE RING 2016
  • Marchukov Evgenij Yuvenalevich
  • Uzbekov Andrej Valerevich
  • Syroezhkin Oleg Vasilevich
  • Shishkova Olga Vladimirovna
  • Selivanov Nikolaj Pavlovich
RU2630924C1

RU 2 265 141 C1

Authors

Kozhevin V.V.

Dates

2005-11-27Published

2004-04-12Filed