AU2001283899A1 - Connecting system for a transition duct in a gas turbine - Google Patents

Connecting system for a transition duct in a gas turbine

Info

Publication number
AU2001283899A1
AU2001283899A1 AU2001283899A AU8389901A AU2001283899A1 AU 2001283899 A1 AU2001283899 A1 AU 2001283899A1 AU 2001283899 A AU2001283899 A AU 2001283899A AU 8389901 A AU8389901 A AU 8389901A AU 2001283899 A1 AU2001283899 A1 AU 2001283899A1
Authority
AU
Australia
Prior art keywords
gas turbine
connecting system
transition duct
duct
transition
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
AU2001283899A
Inventor
Franco Frosini
Luciano Mei
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 AU2001283899A1 publication Critical patent/AU2001283899A1/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
    • 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
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Lasers (AREA)
  • Pipeline Systems (AREA)
AU2001283899A 2000-07-03 2001-06-28 Connecting system for a transition duct in a gas turbine Abandoned AU2001283899A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
IT2000MI001492A IT1318103B1 (en) 2000-07-03 2000-07-03 CONNECTION SYSTEM BETWEEN A LOW PRESSURE NOZZLE AND UNTRANSITION DUCT IN A GAS TURBINE
ITMI200A001492 2000-07-03
PCT/EP2001/007413 WO2002002911A1 (en) 2000-07-03 2001-06-28 Connecting system for a transition duct in a gas turbine

Publications (1)

Publication Number Publication Date
AU2001283899A1 true AU2001283899A1 (en) 2002-01-14

Family

ID=11445393

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001283899A Abandoned AU2001283899A1 (en) 2000-07-03 2001-06-28 Connecting system for a transition duct in a gas turbine

Country Status (11)

Country Link
US (1) US6893209B2 (en)
EP (1) EP1299618B1 (en)
JP (1) JP4753526B2 (en)
KR (1) KR100814174B1 (en)
AU (1) AU2001283899A1 (en)
CA (1) CA2412898C (en)
DE (1) DE60130214T2 (en)
IT (1) IT1318103B1 (en)
RU (1) RU2270344C2 (en)
TW (1) TW483982B (en)
WO (1) WO2002002911A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6851264B2 (en) * 2002-10-24 2005-02-08 General Electric Company Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine
ITMI20041778A1 (en) * 2004-09-17 2004-12-17 Nuovo Pignone Spa BOTTOM SEALED BOTTOM FOR A DOUBLE SHAFT TURBINE
DK2029168T3 (en) 2006-06-02 2013-01-14 Int Aids Vaccine Initiative HIV-1 Clade A consensus sequences, antigens and transgenes.
US8151570B2 (en) * 2007-12-06 2012-04-10 Alstom Technology Ltd Transition duct cooling feed tubes
RU2480590C1 (en) * 2011-12-14 2013-04-27 Открытое акционерное общество "Авиадвигатель" Turbine of gas turbine engine
US10093720B2 (en) 2014-06-11 2018-10-09 International Aids Vaccine Initiative Broadly neutralizing antibody and uses thereof
JP6540357B2 (en) * 2015-08-11 2019-07-10 三菱日立パワーシステムズ株式会社 Static vane and gas turbine equipped with the same

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB369680A (en) 1930-01-24 1932-03-31 Asea Ab Improved device for mounting an inner casing in an outer casing
FR1003299A (en) * 1949-12-13 1952-03-17 Rateau Soc Further training in gas turbines and other axial turbo-machines
US4191011A (en) 1977-12-21 1980-03-04 General Motors Corporation Mount assembly for porous transition panel at annular combustor outlet
FR2624953B1 (en) 1987-12-16 1990-04-20 Snecma COMBUSTION CHAMBER FOR TURBOMACHINES HAVING A DOUBLE WALL CONVERGENT
DE19807247C2 (en) * 1998-02-20 2000-04-20 Mtu Muenchen Gmbh Turbomachine with rotor and stator

Also Published As

Publication number Publication date
ITMI20001492A1 (en) 2002-01-03
WO2002002911A1 (en) 2002-01-10
DE60130214D1 (en) 2007-10-11
EP1299618B1 (en) 2007-08-29
IT1318103B1 (en) 2003-07-23
JP2004502081A (en) 2004-01-22
RU2270344C2 (en) 2006-02-20
KR20030013515A (en) 2003-02-14
DE60130214T2 (en) 2008-05-21
CA2412898C (en) 2011-01-11
JP4753526B2 (en) 2011-08-24
US6893209B2 (en) 2005-05-17
TW483982B (en) 2002-04-21
US20040037699A1 (en) 2004-02-26
CA2412898A1 (en) 2002-01-10
ITMI20001492A0 (en) 2000-07-03
KR100814174B1 (en) 2008-03-14
EP1299618A1 (en) 2003-04-09

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