IN2014DN06201A - - Google Patents

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Publication number
IN2014DN06201A
IN2014DN06201A IN6201DEN2014A IN2014DN06201A IN 2014DN06201 A IN2014DN06201 A IN 2014DN06201A IN 6201DEN2014 A IN6201DEN2014 A IN 6201DEN2014A IN 2014DN06201 A IN2014DN06201 A IN 2014DN06201A
Authority
IN
India
Prior art keywords
diffuser
blow
gas diffuser
exhaust gas
channel
Prior art date
Application number
Inventor
Marc Bröker
Tobias Buchal
Original Assignee
Siemens Ag
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens Ag filed Critical Siemens Ag
Publication of IN2014DN06201A publication Critical patent/IN2014DN06201A/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

The invention relates to a gas turbine (10) having an exhaust gas diffuser (21) connected to a turbine unit (24) wherein the gas diffuser channel (33) of the gas diffuser is delimited on the outside by a channel wall (40) and is provided with a plurality of hollow supporting fins (35) extending inward for fastening a radial bearing (51) of the gas turbine (10) wherein at least one blow off line (47) for blow off air comprising at least one pipeline ends at the outlet side on the exhaust gas diffuser (21) and the end of the exhaust gas diffuser on the inlet side is connected to a compressor (18) of the gas turbine (10). In order to at least partially compensate for the incorrect incident flow of the supporting fins (35) more particularly in partial load operation it is proposed that the supporting fins (35) have a hub (48) on the inner end thereof the axial end of said hub being provided with additional openings (49) for blowing out the blow off air in the diffuser channel.
IN6201DEN2014 2012-02-28 2013-01-15 IN2014DN06201A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP12157273.9A EP2634381A1 (en) 2012-02-28 2012-02-28 Gas turbine with an exhaust gas diffuser and support ribs
PCT/EP2013/050610 WO2013127553A1 (en) 2012-02-28 2013-01-15 Gas turbine having an exhaust gas diffuser and supporting fins

Publications (1)

Publication Number Publication Date
IN2014DN06201A true IN2014DN06201A (en) 2015-10-23

Family

ID=47594704

Family Applications (1)

Application Number Title Priority Date Filing Date
IN6201DEN2014 IN2014DN06201A (en) 2012-02-28 2013-01-15

Country Status (7)

Country Link
US (1) US20140373504A1 (en)
EP (2) EP2634381A1 (en)
JP (1) JP2015508860A (en)
KR (1) KR20140127291A (en)
CN (1) CN104145089B (en)
IN (1) IN2014DN06201A (en)
WO (1) WO2013127553A1 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9488191B2 (en) * 2013-10-30 2016-11-08 Siemens Aktiengesellschaft Gas turbine diffuser strut including coanda flow injection
EP2896793B1 (en) * 2014-01-21 2024-08-28 Ansaldo Energia Switzerland AG Method of operating a gas turbine assembly and the gas turbine assembly
EP3147465A1 (en) * 2015-09-24 2017-03-29 Siemens Aktiengesellschaft Support of a machine, rotating machine engine and a method for assembling of such a rotating machine
JP6563312B2 (en) * 2015-11-05 2019-08-21 川崎重工業株式会社 Extraction structure of gas turbine engine
US9976479B2 (en) * 2015-12-15 2018-05-22 General Electric Company Power plant including a static mixer and steam generating system via turbine extraction and compressor extraction
US9890710B2 (en) * 2015-12-15 2018-02-13 General Electric Company Power plant with steam generation via combustor gas extraction
US10072573B2 (en) * 2015-12-15 2018-09-11 General Electric Company Power plant including an ejector and steam generating system via turbine extraction
US9964035B2 (en) * 2015-12-15 2018-05-08 General Electric Company Power plant including exhaust gas coolant injection system and steam generating system via turbine extraction
US9970354B2 (en) * 2015-12-15 2018-05-15 General Electric Company Power plant including an ejector and steam generating system via turbine extraction and compressor extraction
US10883387B2 (en) * 2016-03-07 2021-01-05 General Electric Company Gas turbine exhaust diffuser with air injection
CN108180045A (en) * 2018-02-07 2018-06-19 上海电气电站设备有限公司 Gas-steam Combined Cycle peak regulation phase modulation shaft system of unit support construction
DE102018217824A1 (en) 2018-10-18 2020-04-23 Siemens Aktiengesellschaft Method for assembling a gas turbine arrangement on a foundation of a power plant and gas turbine arrangement
CN111927581B (en) * 2020-09-08 2022-07-12 杭州汽轮机股份有限公司 Multi-surface supported welding exhaust cylinder of industrial steam turbine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744722A (en) * 1951-04-06 1956-05-08 Gen Motors Corp Turbine bearing support
US4989406A (en) * 1988-12-29 1991-02-05 General Electric Company Turbine engine assembly with aft mounted outlet guide vanes
US6266954B1 (en) * 1999-12-15 2001-07-31 General Electric Co. Double wall bearing cone
JP4040556B2 (en) * 2003-09-04 2008-01-30 株式会社日立製作所 Gas turbine equipment and cooling air supply method
US6983608B2 (en) * 2003-12-22 2006-01-10 General Electric Company Methods and apparatus for assembling gas turbine engines
US8257025B2 (en) * 2008-04-21 2012-09-04 Siemens Energy, Inc. Combustion turbine including a diffuser section with cooling fluid passageways and associated methods
US8647057B2 (en) * 2009-06-02 2014-02-11 Siemens Energy, Inc. Turbine exhaust diffuser with a gas jet producing a coanda effect flow control
US8668449B2 (en) * 2009-06-02 2014-03-11 Siemens Energy, Inc. Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow
US8328518B2 (en) * 2009-08-13 2012-12-11 Siemens Energy, Inc. Turbine vane for a gas turbine engine having serpentine cooling channels
JP4958967B2 (en) * 2009-12-15 2012-06-20 川崎重工業株式会社 Gas turbine engine with improved ventilation structure
US20130174534A1 (en) * 2012-01-05 2013-07-11 General Electric Company System and device for controlling fluid flow through a gas turbine exhaust

Also Published As

Publication number Publication date
EP2634381A1 (en) 2013-09-04
US20140373504A1 (en) 2014-12-25
CN104145089B (en) 2016-03-02
JP2015508860A (en) 2015-03-23
EP2791478A1 (en) 2014-10-22
WO2013127553A1 (en) 2013-09-06
CN104145089A (en) 2014-11-12
KR20140127291A (en) 2014-11-03

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