AU2003296634A1 - Heat shield element, combustion chamber and gas turbine - Google Patents

Heat shield element, combustion chamber and gas turbine

Info

Publication number
AU2003296634A1
AU2003296634A1 AU2003296634A AU2003296634A AU2003296634A1 AU 2003296634 A1 AU2003296634 A1 AU 2003296634A1 AU 2003296634 A AU2003296634 A AU 2003296634A AU 2003296634 A AU2003296634 A AU 2003296634A AU 2003296634 A1 AU2003296634 A1 AU 2003296634A1
Authority
AU
Australia
Prior art keywords
combustion chamber
gas turbine
heat shield
shield element
heat
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
AU2003296634A
Other versions
AU2003296634A8 (en
Inventor
John Carl Glessner
Michael Huth
Peter Tiemann
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.)
Siemens AG
Original Assignee
Siemens AG
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 AG filed Critical Siemens AG
Publication of AU2003296634A8 publication Critical patent/AU2003296634A8/en
Publication of AU2003296634A1 publication Critical patent/AU2003296634A1/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
    • F23R3/007—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
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • F23M20/005—Noise absorbing 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
AU2003296634A 2003-01-27 2003-12-10 Heat shield element, combustion chamber and gas turbine Abandoned AU2003296634A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP03001727A EP1441180A1 (en) 2003-01-27 2003-01-27 Heatshield, combustion chamber and gas turbine
EP03001727.1 2003-01-27
PCT/EP2003/014008 WO2004068035A2 (en) 2003-01-27 2003-12-10 Heat shield element, combustion chamber and gas turbine

Publications (2)

Publication Number Publication Date
AU2003296634A8 AU2003296634A8 (en) 2004-08-23
AU2003296634A1 true AU2003296634A1 (en) 2004-08-23

Family

ID=32524211

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003296634A Abandoned AU2003296634A1 (en) 2003-01-27 2003-12-10 Heat shield element, combustion chamber and gas turbine

Country Status (5)

Country Link
EP (2) EP1441180A1 (en)
AU (1) AU2003296634A1 (en)
DE (1) DE50310791D1 (en)
ES (1) ES2314294T3 (en)
WO (1) WO2004068035A2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2929689B1 (en) * 2008-04-03 2013-04-12 Snecma Propulsion Solide GAS TURBINE COMBUSTION CHAMBER WITH SECTORIZED INTERNAL AND EXTERNAL WALLS
DE102015215207A1 (en) * 2015-08-10 2017-02-16 Siemens Aktiengesellschaft Combustion chamber for a gas turbine and heat shield element for lining such a combustion chamber
US10465907B2 (en) 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
US10598380B2 (en) 2017-09-21 2020-03-24 General Electric Company Canted combustor for gas turbine engine
CN112832928B (en) * 2021-03-05 2022-04-22 中国科学院力学研究所 Method for designing cooling structure with equal inner wall strength for rocket engine
CN112832929B (en) * 2021-03-05 2022-05-24 中国科学院力学研究所 Method for designing cooling structure for equal inner wall surface temperature of rocket engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2794319A (en) * 1953-03-02 1957-06-04 Westinghouse Electric Corp Afterburner shell construction
DE1000188C2 (en) * 1955-06-16 1957-06-13 Gen Electric Device to prevent the howl of a jet engine with a burner in the exhaust pipe
US2938333A (en) * 1957-03-18 1960-05-31 Gen Motors Corp Combustion chamber liner construction
US3918255A (en) * 1973-07-06 1975-11-11 Westinghouse Electric Corp Ceramic-lined combustion chamber and means for support of a liner with combustion air penetrations
FR2716933B1 (en) * 1994-03-03 1996-04-05 Snecma Thermal protection jacket element for a turbomachine and its manufacturing processes.
GB2361302A (en) * 2000-04-13 2001-10-17 Rolls Royce Plc Discharge nozzle for a gas turbine engine combustion chamber
DE60135436D1 (en) * 2001-01-09 2008-10-02 Mitsubishi Heavy Ind Ltd Gas turbine combustor
JP2004524479A (en) * 2001-04-27 2004-08-12 シーメンス　アクチエンゲゼルシヤフト Especially for gas turbine combustion chambers

Also Published As

Publication number Publication date
EP1588102A2 (en) 2005-10-26
WO2004068035A2 (en) 2004-08-12
ES2314294T3 (en) 2009-03-16
AU2003296634A8 (en) 2004-08-23
EP1588102B1 (en) 2008-11-12
EP1441180A1 (en) 2004-07-28
DE50310791D1 (en) 2008-12-24
WO2004068035A3 (en) 2004-09-23

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Legal Events

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