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.)
Raytheon Technologies 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
Publication of DE69618842D1 publication Critical patent/DE69618842D1/de
Application granted granted Critical
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)
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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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
US8966877B2 (en) 2010-01-29 2015-03-03 United Technologies Corporation Gas turbine combustor with variable airflow
US9068751B2 (en) * 2010-01-29 2015-06-30 United Technologies Corporation Gas turbine combustor with staged combustion
US8359866B2 (en) * 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
US8359865B2 (en) 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
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
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
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
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EP3066390B1 (de) * 2013-11-04 2020-10-21 United Technologies Corporation Wandanordnung eines gasturbinenmotors mit versetzter schiene
EP3066391B1 (de) 2013-11-05 2019-01-16 United Technologies Corporation Gekühlte brennkammerschwebewandplatte
DE102013222932A1 (de) 2013-11-11 2015-05-28 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Schindel zur Durchführung einer Zündkerze
US10317078B2 (en) 2013-11-21 2019-06-11 United Technologies Corporation Cooling a multi-walled structure of a turbine engine
US10753608B2 (en) 2013-11-21 2020-08-25 Raytheon Technologies Corporation Turbine engine multi-walled structure with internal cooling element(s)
EP3071887B1 (de) 2013-11-22 2020-03-11 United Technologies Corporation Mehrwandige struktur eines turbinenmotors mit kühlelementen
US10598379B2 (en) 2013-11-25 2020-03-24 United Technologies Corporation Film cooled multi-walled structure with one or more indentations
EP3077724B1 (de) 2013-12-05 2021-04-28 Raytheon Technologies Corporation Kühlung eines löschöffnungskörpers einer brennkammerwand
EP3077641B1 (de) 2013-12-06 2020-02-12 United Technologies Corporation Kühlung einer zünderdurchführung einer brennkammerwand
US10697636B2 (en) 2013-12-06 2020-06-30 Raytheon Technologies Corporation Cooling a combustor heat shield proximate a quench aperture
EP3077729B1 (de) * 2013-12-06 2020-07-15 United Technologies Corporation Schnittstelle für gasturbinen wandanordnung
US10386068B2 (en) 2013-12-06 2019-08-20 United Technologies Corporation Cooling a quench aperture body of a combustor wall
EP3077640B1 (de) 2013-12-06 2021-06-02 Raytheon Technologies Corporation Brennkammerlöschöffnungskühlung
DE102013226488A1 (de) 2013-12-18 2015-06-18 Rolls-Royce Deutschland Ltd & Co Kg Unterlegscheibe einer Brennkammerschindel einer Gasturbine
WO2015147929A2 (en) * 2013-12-20 2015-10-01 United Technologies Corporation Cooling an aperture body of a combustor wall
US10234140B2 (en) 2013-12-31 2019-03-19 United Technologies Corporation Gas turbine engine wall assembly with enhanced flow architecture
US10533745B2 (en) 2014-02-03 2020-01-14 United Technologies Corporation Film cooling a combustor wall of a turbine engine
WO2015117139A1 (en) 2014-02-03 2015-08-06 United Technologies Corporation Stepped heat shield for a turbine engine combustor
DE102014204476A1 (de) 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine
DE102014204481A1 (de) 2014-03-11 2015-09-17 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
US9534786B2 (en) 2014-08-08 2017-01-03 Pratt & Whitney Canada Corp. Combustor heat shield
US10012385B2 (en) * 2014-08-08 2018-07-03 Pratt & Whitney Canada Corp. Combustor heat shield sealing
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
US10823410B2 (en) 2016-10-26 2020-11-03 Raytheon Technologies Corporation Cast combustor liner panel radius for 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
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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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Also Published As

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

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