AU2001262304A1 - Flame-passage device for non-annular gas turbine combustion chambers - Google Patents

Flame-passage device for non-annular gas turbine combustion chambers

Info

Publication number
AU2001262304A1
AU2001262304A1 AU2001262304A AU6230401A AU2001262304A1 AU 2001262304 A1 AU2001262304 A1 AU 2001262304A1 AU 2001262304 A AU2001262304 A AU 2001262304A AU 6230401 A AU6230401 A AU 6230401A AU 2001262304 A1 AU2001262304 A1 AU 2001262304A1
Authority
AU
Australia
Prior art keywords
combustion chambers
flame
gas turbine
annular gas
passage device
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
AU2001262304A
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 AU2001262304A1 publication Critical patent/AU2001262304A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes

Abstract

A flame-passage device (10) for non-annular gas turbine combustion chambers comprises a tubular body (11), which is provided with a plurality of cooling holes (12), for cooling on the swirl-cooling type. The tubular body (11) is inserted in a flanged pipe (27), which connects the cases (31, 32) of two successive combustion chambers (17, 18), and has a first end (13) with a cylindrical shape, and a second end (14) with an oval shape, wherein the second, oval end (14) is provided with three rings (23, 24, 25), for anchorage of the corresponding combustion chamber (17) to the case (31).
AU2001262304A 2000-06-02 2001-05-18 Flame-passage device for non-annular gas turbine combustion chambers Abandoned AU2001262304A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
IT2000MI001241A IT1317775B1 (en) 2000-06-02 2000-06-02 FLAME ARROW DEVICE FOR COMBUSTION CHAMBERS OF NONANULAR GAS TURBINES
ITMI200A001241 2000-06-02
PCT/EP2001/005790 WO2001092787A1 (en) 2000-06-02 2001-05-18 Flame-passage device for non-annular gas turbine combustion chambers

Publications (1)

Publication Number Publication Date
AU2001262304A1 true AU2001262304A1 (en) 2001-12-11

Family

ID=11445183

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001262304A Abandoned AU2001262304A1 (en) 2000-06-02 2001-05-18 Flame-passage device for non-annular gas turbine combustion chambers

Country Status (12)

Country Link
US (1) US6834491B2 (en)
EP (1) EP1290377B1 (en)
AT (1) ATE344424T1 (en)
AU (1) AU2001262304A1 (en)
BR (1) BR0111269A (en)
DE (1) DE60124250T2 (en)
EG (1) EG22763A (en)
IT (1) IT1317775B1 (en)
MX (1) MXPA02011869A (en)
NO (1) NO322604B1 (en)
RU (1) RU2267711C2 (en)
WO (1) WO2001092787A1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2443839A (en) * 2006-11-17 2008-05-21 Siemens Ag Interconnected Combustion Chambers
US8623397B2 (en) * 2007-04-13 2014-01-07 The Regents Of The University Of Michigan Delivery device and method for forming the same
US8220246B2 (en) * 2009-09-21 2012-07-17 General Electric Company Impingement cooled crossfire tube assembly
US20130333389A1 (en) * 2012-06-15 2013-12-19 General Electric Company Cross fire tube retention system for a gas turbine engine
JP5911387B2 (en) * 2012-07-06 2016-04-27 三菱日立パワーシステムズ株式会社 Gas turbine combustor and gas turbine combustor operating method
US20140137536A1 (en) * 2012-11-21 2014-05-22 General Electric Company Super telescoping cross-fire tube and method of assembling a combustor structure
US9353952B2 (en) * 2012-11-29 2016-05-31 General Electric Company Crossfire tube assembly with tube bias between adjacent combustors
US10276776B2 (en) 2013-12-24 2019-04-30 Viking At, Llc Mechanically amplified smart material actuator utilizing layered web assembly
GB201410586D0 (en) 2014-06-13 2014-07-30 Rolls Royce Plc Duct
JP6521283B2 (en) * 2014-09-25 2019-05-29 三菱日立パワーシステムズ株式会社 Combustor, gas turbine
KR20170138442A (en) * 2015-03-30 2017-12-15 누보 피그노네 테크놀로지 에스알엘 Replaceable liner support for gas turbine combustors
JP6965108B2 (en) * 2017-11-08 2021-11-10 三菱パワー株式会社 Gas turbine combustor
KR102125448B1 (en) * 2018-09-11 2020-06-22 두산중공업 주식회사 Cross-fire tube, combustor and gas turbine including the same
RU194926U1 (en) * 2019-10-15 2019-12-30 Публичное Акционерное Общество "Одк-Сатурн" FLAME CONVERTER ASSEMBLY ASSEMBLY WITH HEAT PIPE COMBUSTION CHAMBER OF A GAS TURBINE ENGINE

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2832195A (en) * 1956-04-16 1958-04-29 Gen Electric Cross-ignition tube assembly for gas turbine combustion system
US4249372A (en) * 1979-07-16 1981-02-10 General Electric Company Cross-ignition assembly for combustion apparatus
KR940001925B1 (en) 1990-07-10 1994-03-11 제너럴 일렉트릭 캄파니 Tube mounting apparatus including a wire retainer
US5154049A (en) * 1990-07-10 1992-10-13 General Electric Company Tube mounting apparatus including a wire retainer
US5402635A (en) * 1993-09-09 1995-04-04 Westinghouse Electric Corporation Gas turbine combustor with cooling cross-flame tube connector
US5896742A (en) * 1997-03-20 1999-04-27 General Electric Co. Tapered cross-fire tube for gas turbine combustors
US5964250A (en) 1997-12-01 1999-10-12 General Electric Company Low leakage, articulating fluid transfer tube
GB2339468B (en) * 1998-07-11 2002-04-24 Alstom Gas Turbines Ltd Gas-turbine engine combustion system

Also Published As

Publication number Publication date
WO2001092787A1 (en) 2001-12-06
ITMI20001241A0 (en) 2000-06-02
RU2267711C2 (en) 2006-01-10
US6834491B2 (en) 2004-12-28
MXPA02011869A (en) 2003-04-10
NO322604B1 (en) 2006-10-30
EP1290377B1 (en) 2006-11-02
NO20025741L (en) 2003-01-27
IT1317775B1 (en) 2003-07-15
ATE344424T1 (en) 2006-11-15
ITMI20001241A1 (en) 2001-12-02
US20040098990A1 (en) 2004-05-27
EP1290377A1 (en) 2003-03-12
BR0111269A (en) 2003-06-10
DE60124250D1 (en) 2006-12-14
NO20025741D0 (en) 2002-11-29
DE60124250T2 (en) 2007-05-24
EG22763A (en) 2003-07-30

Similar Documents

Publication Publication Date Title
AU2001262304A1 (en) Flame-passage device for non-annular gas turbine combustion chambers
WO2002035072A3 (en) Nested core gas turbine engine
HK1040758A1 (en) Tube coupling
EP1340941A3 (en) Corrugated cowl for combustor of a gas turbine engine and method for configuring the same
EP1413829A3 (en) Combustor liner with inverted turbulators
AU1736401A (en) Fluid distributor, burner device, gas turbine engine, and cogeneration system
EP1400750A3 (en) Double wall combustor liner segment with cooling channels
WO2002048533A1 (en) Stirling engine, and stirling refrigerator
AU2001235307A1 (en) Distributor for an exhaust gas turbine with an axial flow
CA2314285A1 (en) Piping support of gas turbine steam cooled combustor
ITRM940147A0 (en) GAS INSUFFLATION VALVE TO INFLATE A GASEOUS FUEL, PARTICULARLY HYDROGEN, INTO THE COMBUSTION CHAMBER OF AN INTERNAL COMBUSTION ENGINE.
EP1219900A3 (en) Gas turbine combustion device
ITRM20010435A0 (en) EXHAUST GAS TURBOCHARGER FOR A HEAT ENGINE AND PROCEDURE FOR THE PRODUCTION OF AN EXHAUST GAS TURBOCHARGER.
AU7844301A (en) Transition piece for non-annular gas turbine combustion chambers
MY141622A (en) Exhaust system for an engine
EP1365193A3 (en) Coherent jet system with single ring flame envelope
CA2413635A1 (en) Fuel injection device for a single combustion chamber gas turbine
EP1396394A4 (en) Gas generator
CA2306398A1 (en) Water-tube boiler
WO2000001931A3 (en) Exhaust component having multiple-plated outer shell
AU2002216580A1 (en) Pipe connecting device
DK1292791T3 (en) Liquid shoulder ring for tubular connection
AU693307B2 (en) Liquid ring gas pump with a silencer in the pressure chamber
CA2413637A1 (en) Improved liquid fuel injector for burners of gas turbines
AU2001290467A1 (en) A device for recovering heat energy