AU4840172A - Flame-tube fora combustionchamber ofa gas turbine engine - Google Patents

Flame-tube fora combustionchamber ofa gas turbine engine

Info

Publication number
AU4840172A
AU4840172A AU48401/72A AU4840172A AU4840172A AU 4840172 A AU4840172 A AU 4840172A AU 48401/72 A AU48401/72 A AU 48401/72A AU 4840172 A AU4840172 A AU 4840172A AU 4840172 A AU4840172 A AU 4840172A
Authority
AU
Australia
Prior art keywords
combustionchamber
flame
gas turbine
turbine engine
ofa gas
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.)
Expired
Application number
AU48401/72A
Other versions
AU463411B2 (en
Inventor
Noel Penny Robert
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.)
Penny R N
Original Assignee
Penny R N
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 Penny R N filed Critical Penny R N
Publication of AU4840172A publication Critical patent/AU4840172A/en
Application granted granted Critical
Publication of AU463411B2 publication Critical patent/AU463411B2/en
Expired 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/203—Heat transfer, e.g. cooling by transpiration cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
AU48401/72A 1971-11-05 1972-11-01 Flame-tube fora combustionchamber ofa gas turbine engine Expired AU463411B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB51450/71 1971-11-05
GB5145071A GB1377648A (en) 1971-11-05 1971-11-05 Flame-tube for a combustion chamber of a gas turbine engine

Publications (2)

Publication Number Publication Date
AU4840172A true AU4840172A (en) 1974-05-02
AU463411B2 AU463411B2 (en) 1975-07-24

Family

ID=10460079

Family Applications (1)

Application Number Title Priority Date Filing Date
AU48401/72A Expired AU463411B2 (en) 1971-11-05 1972-11-01 Flame-tube fora combustionchamber ofa gas turbine engine

Country Status (10)

Country Link
JP (1) JPS4854308A (en)
AU (1) AU463411B2 (en)
BE (1) BE790956A (en)
CA (1) CA959661A (en)
CH (2) CH559883A5 (en)
DE (1) DE2253843A1 (en)
FR (1) FR2158572B3 (en)
GB (1) GB1377648A (en)
IT (1) IT975453B (en)
NL (1) NL7214895A (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2842410A1 (en) * 1978-09-29 1980-04-17 Daimler Benz Ag GAS TURBINE SYSTEM
JPS57154856U (en) * 1981-03-19 1982-09-29
CA1231240A (en) * 1983-08-26 1988-01-12 Westinghouse Electric Corporation Varying thickness thermal barrier for combustion turbine baskets
FR2647533B1 (en) * 1989-05-29 1993-03-19 Europ Propulsion SUPERSONIC COMBUSTION STATOREACTOR CHAMBER
FR2699963B1 (en) * 1992-12-24 1995-03-17 Europ Propulsion Close combustion gas generator.
FR2710968B1 (en) * 1993-10-06 1995-11-03 Snecma Double wall combustion chamber.
JPH09511321A (en) * 1994-03-04 1997-11-11 ボルボ エアロ コーポレイション Flame stabilizer
WO1999046540A1 (en) * 1998-03-10 1999-09-16 Siemens Aktiengesellschaft Combustion chamber and method for operating a combustion chamber
EP0943867B1 (en) * 1998-03-17 2002-12-18 ALSTOM (Switzerland) Ltd Ceramic lining for a combustor
US6182436B1 (en) * 1998-07-09 2001-02-06 Pratt & Whitney Canada Corp. Porus material torch igniter
DE10024302A1 (en) * 2000-05-17 2001-11-22 Alstom Power Nv Process for producing a thermally stressed casting
EP1286112A1 (en) * 2001-08-09 2003-02-26 Siemens Aktiengesellschaft Premix burner and method of operating the same
EP1475567A1 (en) * 2003-05-08 2004-11-10 Siemens Aktiengesellschaft Layered structure and method to produce such a layered structure
EP1847696A1 (en) * 2006-04-21 2007-10-24 Siemens Aktiengesellschaft Component for a secondary combustion system in a gas turbine and corresponding gas turbine.
US9310079B2 (en) * 2010-12-30 2016-04-12 Rolls-Royce North American Technologies, Inc. Combustion liner with open cell foam and acoustic damping layers
US11248795B2 (en) 2018-03-09 2022-02-15 Siemens Energy Global Gmbh & Co Kg Finely distributed combustion system for a gas turbine engine
CN112902229A (en) * 2021-03-12 2021-06-04 西北工业大学 Combustion chamber evaporating pipe structure

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1626032A1 (en) * 1967-08-31 1971-01-14 Daimler Benz Ag Part of a gas turbine engine that is exposed to thermal stress and is to be cooled with a gas

Also Published As

Publication number Publication date
IT975453B (en) 1974-07-20
FR2158572A1 (en) 1973-06-15
CH559883A5 (en) 1975-03-14
GB1377648A (en) 1974-12-18
BE790956A (en) 1973-03-01
FR2158572B3 (en) 1975-11-28
DE2253843A1 (en) 1973-05-10
CH559882A5 (en) 1975-03-14
CA959661A (en) 1974-12-24
JPS4854308A (en) 1973-07-31
NL7214895A (en) 1973-05-08
AU463411B2 (en) 1975-07-24

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