SYSTEMS AND METHODS FOR CONTROLLING FLOW OF EXHAUST GAS IN GAS TURBINE SYSTEMS WITH RECIRCULATION OF EXHAUST GAS Russian patent published in 2018 - IPC F02C3/34 

Abstract RU 2645392 C2

FIELD: engines and pumps.

SUBSTANCE: method of controlling a gas turbine system with exhaust gas recirculation (EGR) in which the angle of plurality of inlet guide blades of the exhaust gas compressor of the gas turbine system with EGR is adjusted. The plurality of inlet guide blades has a first range of motion limited by a minimum angle and a maximum angle, at that, the angle is adjusted based on one or more monitored or modelled parameters of the gas turbine system with EGR. The pitch of plurality of blades of the supercharger of the recirculation blower arranged upstream of the exhaust gas compressor is adjusted. The plurality of supercharger blades has a second range of motion limited by a minimum pitch and a maximum pitch, and the pitch of the plurality of supercharger blades is adjusted based on at least the angle of the plurality of inlet guide blades. The gas turbine system comprises an exhaust gas compressor disposed along the EGR path and configured to compress recirculated exhaust gas. A recirculation supercharger comprising a plurality of supercharger blades and an electric motor and located along the EGR path and upstream of the exhaust gas compressor. The controller is connected to the flow control element and the recirculation supercharger. The controller is arranged to control the position of the flow control element based on the measured or modulated parameter of the gas turbine system with EGR, and is configured to control one or more operational parameters of the recirculation blower for controlling the flow of recirculated exhaust gas to the inlet section based on the position of the flow control element. Said one or more operation parameter includes a rotational speed of a supercharger controlled by said electric motor, a pitch of a plurality of supercharger blades, or any combination thereof.

EFFECT: improved responsiveness for controlling gas turbine systems with exhaust gas recirculation.

25 cl, 10 dwg, 2 tbl

Similar patents RU2645392C2

Title Year Author Number
SYSTEM AND METHOD FOR COMPRESSION OF OXIDIZER IN GAS TURBINE SYSTEM BASED ON STOICHIOMETRIC RECYCLING OF EXHAUST GAS 2013
  • Khantington Richard E.
  • Mittriker Franklin F.
  • Uest Dzhejms A.
  • Starcher Loren K.
  • Dkhanuka Sulabkh K.
  • O'Di Dennis M.
  • Drejper Semyuel D.
  • Khansen Kristian M.
  • Denman Todd
RU2655896C2
SYSTEM AND METHOD FOR STOICHIOMETRIC EXHAUST GAS RECIRCULATION GAS TURBINE SYSTEM 2014
  • Khantington Richard E.
  • Minto Karl Din
  • Syuj Bin
  • Tetcher Dzhonatan Karl
  • Vorel Aaron Lejven
RU2678608C2
EXHAUST GAS RECYCLING SYSTEM WITH FIXED CONTENT 2011
  • Stajls Deniel Dzhozef
  • Khildich Dzhejms
  • Ruona Uiljam Charlz
RU2581684C2
EXHAUST GASES RECIRCULATION CONTROL METHOD AND SYSTEM 2014
  • Ulri Dzhozef Norman
  • Makkonvill Greg Patrik
  • Stajls Deniel Dzhozef
  • Persifull Ross Dikstra
  • Shelbi Majkl Khovard
RU2647262C2
THRESHOLD BASED ON EXHAUST GAS TEMPERATURE FOR TURBINE CONTROL METHOD, AND TURBINE 2010
  • Botarelli Claudio
RU2542617C2
DIRECT EXHAUST GASES RECIRCULATION SYSTEM 2014
  • Milvord Filip K.
RU2665010C2
ENGINE OPERATION WITH TURBO SUPERCHARGING AND ENGINE SYSTEM 2013
  • Rollinger, Dzhon Erik
  • Gibson, Aleks O'Konnor
  • Baklend, Dzhulija Khelen
  • Vejd, Robert Endrju
RU2576564C2
CONTROL METHOD OF OPERATING MODE OF GAS TURBINE BASED ON EXHAUST GAS TEMPERATURE, AND GAS TURBINE 2010
  • Botarelli Claudio
RU2539930C2
GAS TURBINE OPERATION CONTROL METHOD BASED ON TEMPERATURE OF EXHAUST GAS AND GAS TURBINE 2010
  • Botarelli Claudio
RU2540210C2
INTERNAL COMBUSTION ENGINE CONTROL SYSTEM 2019
  • Nakada, Hayato
  • Sano, Takeshi
RU2719095C1

RU 2 645 392 C2

Authors

Tatcher Dzhonatan Karl

Uest Dzhejms A.

Vorel Aaron Lejven

Dates

2018-02-21Published

2014-06-24Filed