AXIAL MULTI-STEP COMPRESSOR WITH WATER INJECTION INTO FLOW PART THEREOF Russian patent published in 2021 - IPC F04D19/02 

Abstract RU 2757150 C1

FIELD: heat power engineering.

SUBSTANCE: invention relates to the field of heat power engineering, in particular to power gas turbine units (hereinafter referred to as GTU) with axial multi-step compressors for compressing atmospheric cyclic air. The axial multi-step compressor comprises a body with a blade apparatus with steps placed therein, wherein each step includes working and guiding blades. Each of at least two of the guiding blades thereof has therein a through longitudinal cavity and is installed with one end in the body and the other in an annular band with an intermediate seal defining the annular hollow in the rim of the carrier disk on the side of the outer side surface thereof. Connected to each through longitudinal cavity in at least two of the above guiding blades therein on the side of the body is a cooling water pipeline, and on the side of the annular band is a jet nozzle attached to the band ring, placed in the annular hollow in the rim of the carrier disk, and facing the bottom of the annular hollow at an acute angle to the radius of the rim of the carrier disk. Provided above the annular hollow in the rim of the carrier disk therein is an annular recess communicating therewith and at least two radial channels communicating the annular recess with the volume between the inner surface of the body and the outer surface of the rim of the carrier disk.

EFFECT: ensured dispersion of the cooling liquid using the factors of high-speed rotation of the compressor rotor; reduction in the gas-dynamic losses from admixing finely dispersed moisture to the compressed air; increase in the duration of stay of all formed liquid drops in the flow of the stepwise compressed air; and ensured complete evaporation of the cooling water in the flow part of the compressor of the GTU with the liquid flow rate sufficient for stabilising the power of the GTU at the nominal level when the initial temperature of the compressed air is increased from +15 to +40°C.

3 cl, 2 dwg

Similar patents RU2757150C1

Title Year Author Number
METHOD OF COOLING GAS FLOW IN MULTISTAGE COMPRESSOR 1992
  • Berkovich A.L.
  • Volkov M.P.
  • Potanin B.V.
RU2069276C1
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
METHOD TO IMPROVE EFFICIENCY OF AXIAL MULTISTAGE COMPRESSOR OPERATION 2013
  • Shigapov Ajrat Bagautdinovich
  • Shigapov Azat Ajratovich
  • Shigapov Al'Bert Ajratovich
RU2529289C1
GAS-TURBINE PLANT 2004
  • Shejndlin Aleksandr Efimovich
  • Medin Stanislav Aleksandrovich
  • Ivanov Petr Pavlovich
  • Beloglazov Aleksandr Alekseevich
RU2278286C2
METHOD OF COMBINED-CYCLE POWER PLANT EFFICIENCY INCREASING 2005
  • Kirilenko Viktor Nikolaevich
RU2334112C2
IMPROVEMENT METHOD OF EFFICIENT OPERATION OF GAS TURBINE PLANT 2013
  • Beloglazov Aleksandr Alekseevich
  • Nochevnik Mikhail Naumovich
RU2544397C2
GAS TURBINE PLANT OF RAISED EFFICIENCY 2013
  • Beloglazov Aleksandr Alekseevich
  • Nochevnik Mikhail Naumovich
RU2545261C9
METHOD OF AND DEVICE FOR INCREASING TEMPERATURE DIFFERENCE IN HEAT ENGINE 1998
  • Artamonov A.S.
RU2151310C1
WATER INJECTION SYSTEM OF AXIAL MULTISTAGE COMPRESSOR 2013
  • Shigapov Ajrat Bagautdinovich
  • Shigapov Azat Ajratovich
  • Shigapov Al'Bert Ajratovich
RU2524594C1
GAS TURBINE ENGINE OPERATING METHOD AND GAS TURBINE ENGINE 2019
  • Litvinov Vladimir Konstantinovich
RU2726861C1

RU 2 757 150 C1

Authors

Balashov Yurij Arkadevich

Berezinets Pavel Andreevich

Teplov Boris Dmitrievich

Samojlov Vladimir Leonidovich

Markina Veronika Nikolaevna

Ageev Andrej Vladimirovich

Tuz Natalya Evgenevna

Lobach Igor Anatolevich

Dates

2021-10-11Published

2020-11-03Filed