IN2015DN00897A - - Google Patents

Info

Publication number
IN2015DN00897A
IN2015DN00897A IN897DEN2015A IN2015DN00897A IN 2015DN00897 A IN2015DN00897 A IN 2015DN00897A IN 897DEN2015 A IN897DEN2015 A IN 897DEN2015A IN 2015DN00897 A IN2015DN00897 A IN 2015DN00897A
Authority
IN
India
Prior art keywords
compressed air
receive
combustion gas
axial flow
flow
Prior art date
Application number
Other languages
English (en)
Inventor
Richard C Charron
Matthew D Montgomery
Original Assignee
Siemens Energy Inc
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 Energy Inc filed Critical Siemens Energy Inc
Publication of IN2015DN00897A publication Critical patent/IN2015DN00897A/en

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Turbine Rotor Nozzle Sealing (AREA)
IN897DEN2015 2012-09-04 2013-08-20 IN2015DN00897A (enExample)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/602,422 US9127554B2 (en) 2012-09-04 2012-09-04 Gas turbine engine with radial diffuser and shortened mid section
PCT/US2013/055792 WO2014039247A1 (en) 2012-09-04 2013-08-20 Gas turbine engine with radial diffuser and shortened mid section

Publications (1)

Publication Number Publication Date
IN2015DN00897A true IN2015DN00897A (enExample) 2015-06-12

Family

ID=49083791

Family Applications (1)

Application Number Title Priority Date Filing Date
IN897DEN2015 IN2015DN00897A (enExample) 2012-09-04 2013-08-20

Country Status (8)

Country Link
US (1) US9127554B2 (enExample)
EP (1) EP2893152A1 (enExample)
JP (1) JP6258325B2 (enExample)
CN (1) CN104619956B (enExample)
IN (1) IN2015DN00897A (enExample)
RU (1) RU2631181C2 (enExample)
SA (1) SA515360106B1 (enExample)
WO (1) WO2014039247A1 (enExample)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130081407A1 (en) * 2011-10-04 2013-04-04 David J. Wiebe Aero-derivative gas turbine engine with an advanced transition duct combustion assembly
US20140060001A1 (en) * 2012-09-04 2014-03-06 Alexander R. Beeck Gas turbine engine with shortened mid section
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
US10145251B2 (en) 2016-03-24 2018-12-04 General Electric Company Transition duct assembly
US10260752B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10260424B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10227883B2 (en) 2016-03-24 2019-03-12 General Electric Company Transition duct assembly
US10260360B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly
US11021977B2 (en) * 2018-11-02 2021-06-01 Chromalloy Gas Turbine Llc Diffuser guide vane with deflector panel having curved profile
CN113518850B (zh) * 2018-11-30 2023-08-29 西门子能源全球两合公司 燃气涡轮发动机的中间框架区段和调节径向转子间隙的相应方法
EP3845740B1 (en) * 2019-12-31 2024-04-03 ANSALDO ENERGIA S.p.A. Gas turbine assembly

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3088279A (en) * 1960-08-26 1963-05-07 Gen Electric Radial flow gas turbine power plant
US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine
US4896499A (en) * 1978-10-26 1990-01-30 Rice Ivan G Compression intercooled gas turbine combined cycle
SU1311332A1 (ru) * 1984-03-01 1995-11-20 В.Е. Беляев Осарадиальный диффузор компрессора
US5252860A (en) * 1989-12-11 1993-10-12 Westinghouse Electric Corp. Gas turbine control system having maximum instantaneous load-pickup limiter
KR940011861A (ko) * 1992-11-09 1994-06-22 한스 요트. 헤쩨르, 하아. 카이저 가스 터빈 연소실
JP2904701B2 (ja) * 1993-12-15 1999-06-14 株式会社日立製作所 ガスタービン及びガスタービンの燃焼装置
US5737915A (en) 1996-02-09 1998-04-14 General Electric Co. Tri-passage diffuser for a gas turbine
EP1270874B1 (de) * 2001-06-18 2005-08-31 Siemens Aktiengesellschaft Gasturbine mit einem Verdichter für Luft
US6796130B2 (en) * 2002-11-07 2004-09-28 Siemens Westinghouse Power Corporation Integrated combustor and nozzle for a gas turbine combustion system
RU2235921C1 (ru) * 2002-12-30 2004-09-10 Журавлев Юрий Иванович Напорный диффузор осевого компрессора
JP2005042973A (ja) * 2003-07-22 2005-02-17 Kawasaki Heavy Ind Ltd 旋回流型燃焼器を備えたガスタービン
US7721547B2 (en) * 2005-06-27 2010-05-25 Siemens Energy, Inc. Combustion transition duct providing stage 1 tangential turning for turbine engines
US7870739B2 (en) * 2006-02-02 2011-01-18 Siemens Energy, Inc. Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions
US7600370B2 (en) * 2006-05-25 2009-10-13 Siemens Energy, Inc. Fluid flow distributor apparatus for gas turbine engine mid-frame section
JP5072278B2 (ja) * 2006-07-18 2012-11-14 三菱重工業株式会社 油圧着脱式カップリング
US7631499B2 (en) * 2006-08-03 2009-12-15 Siemens Energy, Inc. Axially staged combustion system for a gas turbine engine
US20090139199A1 (en) 2007-11-15 2009-06-04 General Electric Company Pulse detonation combustor valve for high temperature and high pressure operation
CN101275750B (zh) * 2008-04-25 2010-12-08 北京航空航天大学 一种径向旋流器拐弯区直接喷射预混预蒸发低污染燃烧室
US8276389B2 (en) 2008-09-29 2012-10-02 Siemens Energy, Inc. Assembly for directing combustion gas
US8230688B2 (en) 2008-09-29 2012-07-31 Siemens Energy, Inc. Modular transvane assembly
US9822649B2 (en) * 2008-11-12 2017-11-21 General Electric Company Integrated combustor and stage 1 nozzle in a gas turbine and method
US8616007B2 (en) * 2009-01-22 2013-12-31 Siemens Energy, Inc. Structural attachment system for transition duct outlet
US20140060001A1 (en) * 2012-09-04 2014-03-06 Alexander R. Beeck Gas turbine engine with shortened mid section

Also Published As

Publication number Publication date
WO2014039247A1 (en) 2014-03-13
EP2893152A1 (en) 2015-07-15
RU2631181C2 (ru) 2017-09-19
US9127554B2 (en) 2015-09-08
RU2015107382A (ru) 2016-10-27
JP2015532699A (ja) 2015-11-12
SA515360106B1 (ar) 2016-06-16
CN104619956B (zh) 2017-06-09
CN104619956A (zh) 2015-05-13
JP6258325B2 (ja) 2018-01-10
US20140060000A1 (en) 2014-03-06

Similar Documents

Publication Publication Date Title
IN2015DN00897A (enExample)
EP2784267A3 (en) A gas turbine engine cooling arrangement
EP2618060A3 (en) Axial flow fuel nozzle with a stepped center body
JP6769714B2 (ja) ガスタービン燃焼器用の燃料供給システム
SA515360558B1 (ar) نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغاز
EP1959197A3 (en) Combustor of a gas turbine
EP2617980A3 (en) Gas turbine engines
EP2163819A3 (en) Combustor, method of supplying fuel to same, and method of modifying same
WO2013009636A3 (en) Gas turbine engine with supersonic compressor
EP2481986A3 (en) Gas turbine combustor
EP2290289A3 (en) Gas turbine combustor with improved quench holes arrangement
EP3109557A3 (en) Combustion systems
EP2584142A3 (en) Gas turbine engine cooling systems having hub-bleed impellers and methods for the production thereof
EP2236930A3 (en) Combustor for gas turbine engine
EP2527742A3 (en) System and method for flow control in gas turbine engine
EP2538138A3 (en) Combustor assembly for use in a turbine engine and methods of assembling same
WO2013126125A3 (en) Radial inflow gas turbine engine with advanced transition duct
IN2014DN06201A (enExample)
EP2559858A3 (en) Compressors with integrated secondary air flow systems
EP2554793A3 (en) Inter-turbine ducts with guide vanes of a gas turbine engine
EP2385219A3 (en) Diffuser for gas turbine system between compressor exit and combustor inlet
EP2144002A3 (en) Flow sleeve with tabbed direct combustion liner cooling air
WO2015126489A3 (en) Exhaust section for an aircraft gas turbine engine
EP2762683A3 (en) Axial turbine with sector-divided turbine housing
GB201212384D0 (en) A gas turbine engine