PL1656497T3 - Dyfuzor umieszczony pomiędzy sprężarką i komorą spalania turbiny gazowej - Google Patents

Dyfuzor umieszczony pomiędzy sprężarką i komorą spalania turbiny gazowej

Info

Publication number
PL1656497T3
PL1656497T3 PL04741084T PL04741084T PL1656497T3 PL 1656497 T3 PL1656497 T3 PL 1656497T3 PL 04741084 T PL04741084 T PL 04741084T PL 04741084 T PL04741084 T PL 04741084T PL 1656497 T3 PL1656497 T3 PL 1656497T3
Authority
PL
Poland
Prior art keywords
gasturbine
compressor
combustion chamber
diffuser located
diffuser
Prior art date
Application number
PL04741084T
Other languages
English (en)
Inventor
Peter Tiemann
Reinhard Mönig
Christian Cornelius
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 PL1656497T3 publication Critical patent/PL1656497T3/pl

Links

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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PL04741084T 2003-08-18 2004-07-16 Dyfuzor umieszczony pomiędzy sprężarką i komorą spalania turbiny gazowej PL1656497T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP03018565A EP1508680A1 (de) 2003-08-18 2003-08-18 Diffusor zwischen Verdichter und Brennkammer einer Gasturbine angeordnet
EP04741084A EP1656497B1 (de) 2003-08-18 2004-07-16 Diffusor zwischen verdichter und brennkammer einer gasturbine angeordnet
PCT/EP2004/007946 WO2005019621A1 (de) 2003-08-18 2004-07-16 Diffusor zwischen verdichter und brennkammer einer gasturbine angeordnet

Publications (1)

Publication Number Publication Date
PL1656497T3 true PL1656497T3 (pl) 2007-03-30

Family

ID=34042857

Family Applications (1)

Application Number Title Priority Date Filing Date
PL04741084T PL1656497T3 (pl) 2003-08-18 2004-07-16 Dyfuzor umieszczony pomiędzy sprężarką i komorą spalania turbiny gazowej

Country Status (7)

Country Link
US (1) US8082738B2 (pl)
EP (2) EP1508680A1 (pl)
CN (1) CN100390387C (pl)
DE (1) DE502004001924D1 (pl)
ES (1) ES2275226T3 (pl)
PL (1) PL1656497T3 (pl)
WO (1) WO2005019621A1 (pl)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1508747A1 (de) * 2003-08-18 2005-02-23 Siemens Aktiengesellschaft Diffusor für eine Gasturbine und Gasturbine zur Energieerzeugung
US8474266B2 (en) 2009-07-24 2013-07-02 General Electric Company System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle
US8381532B2 (en) * 2010-01-27 2013-02-26 General Electric Company Bled diffuser fed secondary combustion system for gas turbines
US20110303390A1 (en) * 2010-06-14 2011-12-15 Vykson Limited Combustion Chamber Cooling Method and System
US9476429B2 (en) 2012-12-19 2016-10-25 United Technologies Corporation Flow feed diffuser
WO2014134519A1 (en) * 2013-02-28 2014-09-04 United Technologies Corporation Method and apparatus for collecting pre-diffuser airflow and routing it to combustor pre-swirlers
EP2971649A4 (en) 2013-03-14 2016-03-16 United Technologies Corp GAS TURBINE ENGINEERING DESIGN WITH NEST OF CONCENTRIC COMBUSTION CHAMBER
WO2015009449A1 (en) * 2013-07-17 2015-01-22 United Technologies Corporation Supply duct for cooling air
US11732892B2 (en) 2013-08-14 2023-08-22 General Electric Company Gas turbomachine diffuser assembly with radial flow splitters
US20150047358A1 (en) * 2013-08-14 2015-02-19 General Electric Company Inner barrel member with integrated diffuser for a gas turbomachine
WO2015031796A1 (en) 2013-08-29 2015-03-05 United Technologies Corporation Hybrid diffuser case for a gas turbine engine combustor
EP2921779B1 (en) * 2014-03-18 2017-12-06 Ansaldo Energia Switzerland AG Combustion chamber with cooling sleeve
EP3023695A1 (de) * 2014-11-20 2016-05-25 Siemens Aktiengesellschaft Thermische Energiemaschine
US10465907B2 (en) 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
JP6783054B2 (ja) * 2015-12-25 2020-11-11 川崎重工業株式会社 ガスタービンエンジン
JP6625427B2 (ja) * 2015-12-25 2019-12-25 川崎重工業株式会社 ガスタービンエンジン
JP6586389B2 (ja) * 2016-04-25 2019-10-02 三菱重工業株式会社 圧縮機ディフューザおよびガスタービン
US10598380B2 (en) 2017-09-21 2020-03-24 General Electric Company Canted combustor for gas turbine engine
US11808178B2 (en) * 2019-08-05 2023-11-07 Rtx Corporation Tangential onboard injector inlet extender
EP4033073A1 (en) * 2021-01-25 2022-07-27 Siemens Energy Global GmbH & Co. KG Combustion section with a casing shielding
US12448918B2 (en) * 2022-05-09 2025-10-21 General Electric Company Diffuser with passlets
US12359615B1 (en) * 2023-12-29 2025-07-15 Rtx Corporation Separating airflows within a turbine engine

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Publication number Priority date Publication date Assignee Title
US2541170A (en) * 1946-07-08 1951-02-13 Kellogg M W Co Air intake arrangement for air jacketed combustion chambers
US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine
US4796429A (en) * 1976-11-15 1989-01-10 General Motors Corporation Combustor diffuser
US4194359A (en) * 1977-12-12 1980-03-25 United Technologies Corporation Means for improving the performance of burner shroud diffusers
US4297842A (en) * 1980-01-21 1981-11-03 General Electric Company NOx suppressant stationary gas turbine combustor
GB8928378D0 (en) * 1989-12-15 1990-02-21 Rolls Royce Plc A diffuser
US5077967A (en) * 1990-11-09 1992-01-07 General Electric Company Profile matched diffuser
US5197289A (en) * 1990-11-26 1993-03-30 General Electric Company Double dome combustor
US5269133A (en) * 1991-06-18 1993-12-14 General Electric Company Heat exchanger for cooling a gas turbine
FR2706534B1 (fr) * 1993-06-10 1995-07-21 Snecma Diffuseur-séparateur multiflux avec redresseur intégré pour turboréacteur.
DE4415315A1 (de) * 1994-05-02 1995-11-09 Abb Management Ag Kraftwerksanlage
US5555721A (en) * 1994-09-28 1996-09-17 General Electric Company Gas turbine engine cooling supply circuit
DE19544927A1 (de) * 1995-12-01 1997-04-17 Siemens Ag Gasturbine
DE19639623A1 (de) * 1996-09-26 1998-04-09 Siemens Ag Mischung von zwei Fluidströmen an einem Verdichter
GB9917957D0 (en) * 1999-07-31 1999-09-29 Rolls Royce Plc A combustor arrangement
ES2261288T3 (es) * 2001-03-26 2006-11-16 Siemens Aktiengesellschaft Turbina de gas.
DE50107283D1 (de) * 2001-06-18 2005-10-06 Siemens Ag Gasturbine mit einem Verdichter für Luft
EP1400751A1 (de) * 2002-09-17 2004-03-24 Siemens Aktiengesellschaft Brennkammer für eine Gasturbine
GB0229307D0 (en) * 2002-12-17 2003-01-22 Rolls Royce Plc A diffuser arrangement

Also Published As

Publication number Publication date
EP1508680A1 (de) 2005-02-23
CN100390387C (zh) 2008-05-28
WO2005019621A1 (de) 2005-03-03
CN1836097A (zh) 2006-09-20
EP1656497B1 (de) 2006-11-02
EP1656497A1 (de) 2006-05-17
ES2275226T3 (es) 2007-06-01
US20100257869A1 (en) 2010-10-14
US8082738B2 (en) 2011-12-27
DE502004001924D1 (de) 2006-12-14

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