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DE69618842D1 - Schutzplatten zur Auskleidung einer Gasturbinenbrennkammer - Google Patents

Schutzplatten zur Auskleidung einer Gasturbinenbrennkammer

Info

Publication number
DE69618842D1
DE69618842D1 DE69618842T DE69618842T DE69618842D1 DE 69618842 D1 DE69618842 D1 DE 69618842D1 DE 69618842 T DE69618842 T DE 69618842T DE 69618842 T DE69618842 T DE 69618842T DE 69618842 D1 DE69618842 D1 DE 69618842D1
Authority
DE
Germany
Prior art keywords
lining
combustion chamber
gas turbine
protective plates
turbine combustion
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 - Lifetime
Application number
DE69618842T
Other languages
English (en)
Other versions
DE69618842T2 (de
Inventor
Thomas L Dubell
William T Wisinski
John R Herrin
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE69618842D1 publication Critical patent/DE69618842D1/de
Publication of DE69618842T2 publication Critical patent/DE69618842T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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

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)
  • Gas Burners (AREA)
DE69618842T 1995-05-03 1996-04-19 Schutzplatten zur Auskleidung einer Gasturbinenbrennkammer Expired - Lifetime DE69618842T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/434,077 US5758503A (en) 1995-05-03 1995-05-03 Gas turbine combustor

Publications (2)

Publication Number Publication Date
DE69618842D1 true DE69618842D1 (de) 2002-03-14
DE69618842T2 DE69618842T2 (de) 2002-10-31

Family

ID=23722730

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69618842T Expired - Lifetime DE69618842T2 (de) 1995-05-03 1996-04-19 Schutzplatten zur Auskleidung einer Gasturbinenbrennkammer

Country Status (4)

Country Link
US (1) US5758503A (de)
EP (1) EP0741268B1 (de)
JP (1) JP3911307B2 (de)
DE (1) DE69618842T2 (de)

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US6497105B1 (en) 2001-06-04 2002-12-24 Pratt & Whitney Canada Corp. Low cost combustor burner collar
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US7093439B2 (en) 2002-05-16 2006-08-22 United Technologies Corporation Heat shield panels for use in a combustor for a gas turbine engine
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US6761031B2 (en) 2002-09-18 2004-07-13 General Electric Company Double wall combustor liner segment with enhanced cooling
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US7140185B2 (en) * 2004-07-12 2006-11-28 United Technologies Corporation Heatshielded article
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DE102006040760A1 (de) * 2006-08-31 2008-03-06 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammerwand für eine mager-brennende Gasturbinenbrennkammer
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US8800290B2 (en) * 2007-12-18 2014-08-12 United Technologies Corporation Combustor
US8056342B2 (en) * 2008-06-12 2011-11-15 United Technologies Corporation Hole pattern for gas turbine combustor
US8079804B2 (en) * 2008-09-18 2011-12-20 Siemens Energy, Inc. Cooling structure for outer surface of a gas turbine case
US8092161B2 (en) * 2008-09-24 2012-01-10 Siemens Energy, Inc. Thermal shield at casing joint
US20100095679A1 (en) * 2008-10-22 2010-04-22 Honeywell International Inc. Dual wall structure for use in a combustor of a gas turbine engine
US20100095680A1 (en) * 2008-10-22 2010-04-22 Honeywell International Inc. Dual wall structure for use in a combustor of a gas turbine engine
US8448416B2 (en) * 2009-03-30 2013-05-28 General Electric Company Combustor liner
US20100242483A1 (en) * 2009-03-30 2010-09-30 United Technologies Corporation Combustor for gas turbine engine
US8695322B2 (en) * 2009-03-30 2014-04-15 General Electric Company Thermally decoupled can-annular transition piece
US20100263386A1 (en) * 2009-04-16 2010-10-21 General Electric Company Turbine engine having a liner
US8863527B2 (en) * 2009-04-30 2014-10-21 Rolls-Royce Corporation Combustor liner
US8495881B2 (en) * 2009-06-02 2013-07-30 General Electric Company System and method for thermal control in a cap of a gas turbine combustor
US8800298B2 (en) * 2009-07-17 2014-08-12 United Technologies Corporation Washer with cooling passage for a turbine engine combustor
US8739546B2 (en) * 2009-08-31 2014-06-03 United Technologies Corporation Gas turbine combustor with quench wake control
US8443610B2 (en) 2009-11-25 2013-05-21 United Technologies Corporation Low emission gas turbine combustor
US9416970B2 (en) * 2009-11-30 2016-08-16 United Technologies Corporation Combustor heat panel arrangement having holes offset from seams of a radially opposing heat panel
US9068751B2 (en) * 2010-01-29 2015-06-30 United Technologies Corporation Gas turbine combustor with staged combustion
US8966877B2 (en) 2010-01-29 2015-03-03 United Technologies Corporation Gas turbine combustor with variable airflow
US8359865B2 (en) 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
US8359866B2 (en) * 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
US9958162B2 (en) 2011-01-24 2018-05-01 United Technologies Corporation Combustor assembly for a turbine engine
US9068748B2 (en) 2011-01-24 2015-06-30 United Technologies Corporation Axial stage combustor for gas turbine engines
US8479521B2 (en) 2011-01-24 2013-07-09 United Technologies Corporation Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies
DE102012016493A1 (de) * 2012-08-21 2014-02-27 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit prallgekühlten Bolzen der Brennkammerschindeln
US10107497B2 (en) 2012-10-04 2018-10-23 United Technologies Corporation Gas turbine engine combustor liner
US9494081B2 (en) 2013-05-09 2016-11-15 Siemens Aktiengesellschaft Turbine engine shutdown temperature control system with an elongated ejector
EP3044444B1 (de) * 2013-09-13 2019-11-06 United Technologies Corporation Brennkammer für einen gasturbinenmotor mit einer abgedichten wandplatte
US10808937B2 (en) * 2013-11-04 2020-10-20 Raytheon Technologies Corporation Gas turbine engine wall assembly with offset rail
WO2015069466A1 (en) 2013-11-05 2015-05-14 United Technologies Corporation Cooled combustor floatwall panel
DE102013222932A1 (de) 2013-11-11 2015-05-28 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Schindel zur Durchführung einer Zündkerze
EP3071885B1 (de) 2013-11-21 2020-03-11 United Technologies Corporation Mehrwandige struktur eines turbinenmotors mit innenkühlelementen
WO2015077600A1 (en) 2013-11-21 2015-05-28 United Technologies Corporation Cooling a multi-walled structure of a turbine engine
US10386066B2 (en) 2013-11-22 2019-08-20 United Technologies Corpoation Turbine engine multi-walled structure with cooling element(s)
WO2015077755A1 (en) 2013-11-25 2015-05-28 United Technologies Corporation Film cooled multi-walled structure with one or more indentations
US10502422B2 (en) 2013-12-05 2019-12-10 United Technologies Corporation Cooling a quench aperture body of a combustor wall
US10378768B2 (en) 2013-12-06 2019-08-13 United Technologies Corporation Combustor quench aperture cooling
US10697636B2 (en) 2013-12-06 2020-06-30 Raytheon Technologies Corporation Cooling a combustor heat shield proximate a quench aperture
WO2015085080A1 (en) 2013-12-06 2015-06-11 United Technologies Corporation Cooling an igniter aperture body of a combustor wall
US10197285B2 (en) * 2013-12-06 2019-02-05 United Technologies Corporation Gas turbine engine wall assembly interface
WO2015084963A1 (en) 2013-12-06 2015-06-11 United Technologies Corporation Cooling a quench aperture body of a combustor wall
DE102013226488A1 (de) 2013-12-18 2015-06-18 Rolls-Royce Deutschland Ltd & Co Kg Unterlegscheibe einer Brennkammerschindel einer Gasturbine
US10317079B2 (en) * 2013-12-20 2019-06-11 United Technologies Corporation Cooling an aperture body of a combustor wall
EP3090208B1 (de) 2013-12-31 2018-12-19 United Technologies Corporation Gasturbinenmotorwandanordnung mit verbesserter strömungsleitung
EP3102884B1 (de) 2014-02-03 2020-04-01 United Technologies Corporation Gestuftes hitzeschild für eine gasturbinenbrennkammer
US10533745B2 (en) 2014-02-03 2020-01-14 United Technologies Corporation Film cooling a combustor wall of a turbine engine
DE102014204481A1 (de) 2014-03-11 2015-09-17 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine
DE102014204476A1 (de) 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine
US9909761B2 (en) * 2014-04-09 2018-03-06 United Technologies Corporation Combustor wall assembly for a turbine engine
EP2977679B1 (de) 2014-07-22 2019-08-28 United Technologies Corporation Brennkammerwand für einen gasturbinenmotor und verfahren zur akustischen dämpfung
US10012385B2 (en) * 2014-08-08 2018-07-03 Pratt & Whitney Canada Corp. Combustor heat shield sealing
US9534786B2 (en) 2014-08-08 2017-01-03 Pratt & Whitney Canada Corp. Combustor heat shield
GB201418042D0 (en) 2014-10-13 2014-11-26 Rolls Royce Plc A liner element for a combustor, and a related method
US10267521B2 (en) 2015-04-13 2019-04-23 Pratt & Whitney Canada Corp. Combustor heat shield
US10935240B2 (en) 2015-04-23 2021-03-02 Raytheon Technologies Corporation Additive manufactured combustor heat shield
GB201518345D0 (en) * 2015-10-16 2015-12-02 Rolls Royce Combustor for a gas turbine engine
GB201603166D0 (en) * 2016-02-24 2016-04-06 Rolls Royce Plc A combustion chamber
US10215411B2 (en) * 2016-03-07 2019-02-26 United Technologies Corporation Combustor panels having recessed rail
GB201610122D0 (en) * 2016-06-10 2016-07-27 Rolls Royce Plc A combustion chamber
US10669939B2 (en) 2016-10-26 2020-06-02 Raytheon Technologies Corporation Combustor seal for a gas turbine engine combustor
US10823410B2 (en) 2016-10-26 2020-11-03 Raytheon Technologies Corporation Cast combustor liner panel radius for gas turbine engine combustor
US10830448B2 (en) 2016-10-26 2020-11-10 Raytheon Technologies Corporation Combustor liner panel with a multiple of heat transfer augmentors for a gas turbine engine combustor
US10670269B2 (en) 2016-10-26 2020-06-02 Raytheon Technologies Corporation Cast combustor liner panel gating feature for a gas turbine engine combustor
US10935243B2 (en) 2016-11-30 2021-03-02 Raytheon Technologies Corporation Regulated combustor liner panel for a gas turbine engine combustor
US10940530B2 (en) 2017-09-12 2021-03-09 Raytheon Technologies Corporation Method to produce jet engine combustor heat shield panels assembly
US10940529B2 (en) * 2017-09-12 2021-03-09 Raytheon Technologies Corporation Method to produce jet engine combustor heat shield panels assembly
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JP2024091028A (ja) * 2022-12-23 2024-07-04 川崎重工業株式会社 ガスタービンの燃焼器

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Also Published As

Publication number Publication date
US5758503A (en) 1998-06-02
JPH0926135A (ja) 1997-01-28
EP0741268A1 (de) 1996-11-06
DE69618842T2 (de) 2002-10-31
EP0741268B1 (de) 2002-01-30
JP3911307B2 (ja) 2007-05-09

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Legal Events

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