EP2927594A3 - Combustion chamber of a gas turbine - Google Patents

Combustion chamber of a gas turbine Download PDF

Info

Publication number
EP2927594A3
EP2927594A3 EP15158442.2A EP15158442A EP2927594A3 EP 2927594 A3 EP2927594 A3 EP 2927594A3 EP 15158442 A EP15158442 A EP 15158442A EP 2927594 A3 EP2927594 A3 EP 2927594A3
Authority
EP
European Patent Office
Prior art keywords
combustion chamber
gas turbine
wall
shingles
dividing
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.)
Granted
Application number
EP15158442.2A
Other languages
German (de)
French (fr)
Other versions
EP2927594A2 (en
EP2927594B1 (en
Inventor
Carsten Dr.-Ing. Clemen
Thomas Dr.-Ing. Dörr
Sebastian Dr.-Ing. Bake
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.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
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 Rolls Royce Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Publication of EP2927594A2 publication Critical patent/EP2927594A2/en
Publication of EP2927594A3 publication Critical patent/EP2927594A3/en
Application granted granted Critical
Publication of EP2927594B1 publication Critical patent/EP2927594B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Die Erfindung bezieht sich auf eine Brennkammer einer Gasturbine mit einer äußeren Brennkammerwand (1) und an deren Innenseite befestigten Schindeln (9) oder auf eine einwandige Brennkammer, dadurch gekennzeichnet, dass die Brennkammer in einem mittleren Bereich, bezogen auf die Durchströmungsrichtung, einen sich um den gesamten Umfang der Brennkammer erstreckenden Schlitz (18) aufweist, der die äußere Brennkammerwand (1) und die Schindeln (9) zur Zuleitung von Mischluft unterteilt.

Figure imgaf001
The invention relates to a combustion chamber of a gas turbine with an outer combustion chamber wall (1) and attached to the inside shingles (9) or to a single-wall combustion chamber, characterized in that the combustion chamber in a central region, based on the flow direction, a to having the entire circumference of the combustion chamber extending slot (18) dividing the outer combustion chamber wall (1) and the shingles (9) for supplying mixed air.
Figure imgaf001
EP15158442.2A 2014-03-11 2015-03-10 Combustion chamber of a gas turbine Active EP2927594B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102014204482.0A DE102014204482A1 (en) 2014-03-11 2014-03-11 Combustion chamber of a gas turbine

Publications (3)

Publication Number Publication Date
EP2927594A2 EP2927594A2 (en) 2015-10-07
EP2927594A3 true EP2927594A3 (en) 2016-02-17
EP2927594B1 EP2927594B1 (en) 2019-05-08

Family

ID=52633152

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15158442.2A Active EP2927594B1 (en) 2014-03-11 2015-03-10 Combustion chamber of a gas turbine

Country Status (3)

Country Link
US (1) US9366436B2 (en)
EP (1) EP2927594B1 (en)
DE (1) DE102014204482A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3045137B1 (en) * 2015-12-11 2018-05-04 Safran Aircraft Engines TURBOMACHINE COMBUSTION CHAMBER
US10655853B2 (en) * 2016-11-10 2020-05-19 United Technologies Corporation Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
US10935235B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10935236B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US11035251B2 (en) * 2019-09-26 2021-06-15 General Electric Company Stator temperature control system for a gas turbine engine
US20220390112A1 (en) * 2021-06-07 2022-12-08 General Electric Company Combustor for a gas turbine engine
US20220390111A1 (en) * 2021-06-07 2022-12-08 General Electric Company Combustor for a gas turbine engine
US11959643B2 (en) 2021-06-07 2024-04-16 General Electric Company Combustor for a gas turbine engine
US20230144971A1 (en) * 2021-11-11 2023-05-11 General Electric Company Combustion liner
CN115046226B (en) * 2022-08-11 2022-11-04 成都中科翼能科技有限公司 Gas turbine flame tube supporting and positioning structure
US11747019B1 (en) * 2022-09-02 2023-09-05 General Electric Company Aerodynamic combustor liner design for emissions reductions

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB543918A (en) * 1939-09-29 1942-03-19 Bbc Brown Boveri & Cie Improvements and relating to combustion chambers
FR1036218A (en) * 1951-04-26 1953-09-04 Lucas Ltd Joseph Improvements in the manufacture of tubular bodies
DE1179422B (en) * 1959-01-29 1964-10-08 Rolls Royce Combustion chamber, especially for jet engines
US4773227A (en) * 1982-04-07 1988-09-27 United Technologies Corporation Combustion chamber with improved liner construction

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
GB1256066A (en) 1967-11-10 1971-12-08 Lucas Industries Ltd Flame tubes for gas turbine engines
DE2416909A1 (en) 1974-04-06 1975-10-16 Daimler Benz Ag OPERATING PROCEDURE FOR A GAS TURBINE SYSTEM FOR EXHAUST GAS IMPROVEMENT AND THE CORRESPONDING GAS TURBINE SYSTEM
US4138842A (en) * 1975-11-05 1979-02-13 Zwick Eugene B Low emission combustion apparatus
FR2472082A1 (en) * 1979-12-19 1981-06-26 France Etat IMPROVEMENTS IN OR RELATING TO INTERNAL COMBUSTION ENGINES, IN PARTICULAR FOR DIESEL ENGINES
DE3209135A1 (en) * 1982-03-12 1983-09-15 Kraftwerk Union AG, 4330 Mülheim GAS TURBINE COMBUSTION CHAMBER
US4567730A (en) * 1983-10-03 1986-02-04 General Electric Company Shielded combustor
DE4034711C1 (en) * 1990-11-01 1992-02-27 Daimler-Benz Aktiengesellschaft, 7000 Stuttgart, De Secondary air feed control for gas turbine burner flame tube - has jacketed tube with spherical surface in region with air ports with throttle ring
US5461866A (en) * 1994-12-15 1995-10-31 United Technologies Corporation Gas turbine engine combustion liner float wall cooling arrangement
GB2405197B (en) * 2003-08-16 2005-09-28 Rolls Royce Plc Fuel injector
FR2897418B1 (en) * 2006-02-10 2013-03-01 Snecma ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE
DE102006042124B4 (en) 2006-09-07 2010-04-22 Man Turbo Ag Gas turbine combustor
DE102006048842B4 (en) * 2006-10-13 2019-10-10 Man Energy Solutions Se Combustion chamber for a gas turbine
RU2010101978A (en) * 2010-01-15 2011-07-20 Дженерал Электрик Компани (US) GAS TURBINE CONNECTION UNIT

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB543918A (en) * 1939-09-29 1942-03-19 Bbc Brown Boveri & Cie Improvements and relating to combustion chambers
FR1036218A (en) * 1951-04-26 1953-09-04 Lucas Ltd Joseph Improvements in the manufacture of tubular bodies
DE1179422B (en) * 1959-01-29 1964-10-08 Rolls Royce Combustion chamber, especially for jet engines
US4773227A (en) * 1982-04-07 1988-09-27 United Technologies Corporation Combustion chamber with improved liner construction

Also Published As

Publication number Publication date
US9366436B2 (en) 2016-06-14
EP2927594A2 (en) 2015-10-07
EP2927594B1 (en) 2019-05-08
DE102014204482A1 (en) 2015-09-17
US20150260403A1 (en) 2015-09-17

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