AU7844301A - Transition piece for non-annular gas turbine combustion chambers - Google Patents

Transition piece for non-annular gas turbine combustion chambers

Info

Publication number
AU7844301A
AU7844301A AU78443/01A AU7844301A AU7844301A AU 7844301 A AU7844301 A AU 7844301A AU 78443/01 A AU78443/01 A AU 78443/01A AU 7844301 A AU7844301 A AU 7844301A AU 7844301 A AU7844301 A AU 7844301A
Authority
AU
Australia
Prior art keywords
gas turbine
combustion chambers
transition piece
annular gas
turbine combustion
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
AU78443/01A
Inventor
Alessandro Coppola
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nuovo Pignone Holding SpA
Original Assignee
Nuovo Pignone Holding SpA
Nuovo Pignone SpA
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 Nuovo Pignone Holding SpA, Nuovo Pignone SpA filed Critical Nuovo Pignone Holding SpA
Publication of AU7844301A publication Critical patent/AU7844301A/en
Abandoned legal-status Critical Current

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
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)
AU78443/01A 2000-06-16 2001-06-08 Transition piece for non-annular gas turbine combustion chambers Abandoned AU7844301A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ITMI00A1362 2000-06-16
IT2000MI001362A IT1317978B1 (en) 2000-06-16 2000-06-16 TRANSITION PIECE FOR COMBUSTION CHAMBERS OF NONANULAR GAS TURBINES.
PCT/EP2001/006484 WO2001096712A1 (en) 2000-06-16 2001-06-08 Transition piece for non-annular gas turbine combustion chambers

Publications (1)

Publication Number Publication Date
AU7844301A true AU7844301A (en) 2001-12-24

Family

ID=11445283

Family Applications (1)

Application Number Title Priority Date Filing Date
AU78443/01A Abandoned AU7844301A (en) 2000-06-16 2001-06-08 Transition piece for non-annular gas turbine combustion chambers

Country Status (12)

Country Link
US (1) US20030167776A1 (en)
EP (1) EP1295014B1 (en)
AR (1) AR028133A1 (en)
AT (1) ATE310896T1 (en)
AU (1) AU7844301A (en)
BR (1) BR0111577A (en)
DE (1) DE60115236T2 (en)
IT (1) IT1317978B1 (en)
MX (1) MXPA02012451A (en)
NO (1) NO330416B1 (en)
RU (1) RU2275554C2 (en)
WO (1) WO2001096712A1 (en)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7178341B2 (en) * 2004-06-17 2007-02-20 Siemens Power Generation, Inc. Multi-zone tubing assembly for a transition piece of a gas turbine
US7278254B2 (en) * 2005-01-27 2007-10-09 Siemens Power Generation, Inc. Cooling system for a transition bracket of a transition in a turbine engine
US8015818B2 (en) * 2005-02-22 2011-09-13 Siemens Energy, Inc. Cooled transition duct for a gas turbine engine
US7827801B2 (en) * 2006-02-09 2010-11-09 Siemens Energy, Inc. Gas turbine engine transitions comprising closed cooled transition cooling channels
US8151570B2 (en) * 2007-12-06 2012-04-10 Alstom Technology Ltd Transition duct cooling feed tubes
US8113003B2 (en) * 2008-08-12 2012-02-14 Siemens Energy, Inc. Transition with a linear flow path for use in a gas turbine engine
US8091365B2 (en) * 2008-08-12 2012-01-10 Siemens Energy, Inc. Canted outlet for transition in a gas turbine engine
US20120186269A1 (en) * 2011-01-25 2012-07-26 General Electric Company Support between transition piece and impingement sleeve in combustor
EP2852735B1 (en) * 2011-10-24 2016-04-27 Alstom Technology Ltd Gas turbine
US9593853B2 (en) * 2014-02-20 2017-03-14 Siemens Energy, Inc. Gas flow path for a gas turbine engine
US20180258778A1 (en) * 2015-08-28 2018-09-13 Siemens Aktiengesellschaft Non-axially symmetric transition ducts for combustors
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US10584876B2 (en) 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US10724441B2 (en) 2016-03-25 2020-07-28 General Electric Company Segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
JP6650849B2 (en) * 2016-08-25 2020-02-19 三菱日立パワーシステムズ株式会社 gas turbine
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US10837299B2 (en) 2017-03-07 2020-11-17 General Electric Company System and method for transition piece seal
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5964091A (en) * 1995-07-11 1999-10-12 Hitachi, Ltd. Gas turbine combustor and gas turbine
US6006523A (en) * 1997-04-30 1999-12-28 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor with angled tube section
US6393828B1 (en) * 1997-07-21 2002-05-28 General Electric Company Protective coatings for turbine combustion components

Also Published As

Publication number Publication date
DE60115236D1 (en) 2005-12-29
DE60115236T2 (en) 2006-07-27
US20030167776A1 (en) 2003-09-11
BR0111577A (en) 2003-03-18
ITMI20001362A0 (en) 2000-06-16
NO20025995L (en) 2003-02-13
RU2275554C2 (en) 2006-04-27
NO20025995D0 (en) 2002-12-13
MXPA02012451A (en) 2003-04-25
ITMI20001362A1 (en) 2001-12-16
EP1295014A1 (en) 2003-03-26
AR028133A1 (en) 2003-04-23
IT1317978B1 (en) 2003-07-21
ATE310896T1 (en) 2005-12-15
NO330416B1 (en) 2011-04-11
EP1295014B1 (en) 2005-11-23
WO2001096712A1 (en) 2001-12-20

Similar Documents

Publication Publication Date Title
AU7844301A (en) Transition piece for non-annular gas turbine combustion chambers
EP1271057B8 (en) Gas turbine combustor
GB2377487B (en) Improvements to gas turbine combustion chambers
EP1291581A3 (en) Gas turbine engine combustor
EP1270872A4 (en) Gas turbine engine
AU2001236532A1 (en) Low cost, low emissions natural gas combustor
AU2002235119A1 (en) Nested core gas turbine engine
EP1400756A4 (en) Gas turbine combustor
AU2003289368A1 (en) Combustor for gas turbine
AU2002366110A1 (en) Gas turbine arrangement
GB0126371D0 (en) Gas turbine engines
GB0118077D0 (en) A gas turbine engine
EG22526A (en) Combustion chamber for gas turbine
AU2001294247A1 (en) Combustion gas seal for injector
AU3698500A (en) Gas turbine engine
AUPR657901A0 (en) A miniature multifuel gas turbine engine
AU7985500A (en) Gas turbine engine
AU4662099A (en) Combustion chamber for gas turbine
AU2001295007A1 (en) Gas turbine engine having improved efficiency
AU1328201A (en) Gas turbine engine
AU3698600A (en) Gas turbine engine
AU2002952615A0 (en) Improved gas turbine combustion chambers
TW462438U (en) Turbine engine for gas burning
AU3633501A (en) Gas turbine engine
AU3698700A (en) Gas turbine engine

Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase