CH708646A2 - Innengekühlter Übergangskanalhinterrahmen. - Google Patents

Innengekühlter Übergangskanalhinterrahmen. Download PDF

Info

Publication number
CH708646A2
CH708646A2 CH01421/14A CH14212014A CH708646A2 CH 708646 A2 CH708646 A2 CH 708646A2 CH 01421/14 A CH01421/14 A CH 01421/14A CH 14212014 A CH14212014 A CH 14212014A CH 708646 A2 CH708646 A2 CH 708646A2
Authority
CH
Switzerland
Prior art keywords
rear frame
channel
cooling
transition
main body
Prior art date
Application number
CH01421/14A
Other languages
German (de)
English (en)
Inventor
Elizabeth Angelyn Fadde
Patrick Benedict Melton
David William Cihlar
Richard Martin Dicintio
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH708646A2 publication Critical patent/CH708646A2/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/04—Air inlet arrangements
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • 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
    • F23R2900/03043—Convection cooled combustion chamber walls with means for guiding the cooling air flow
    • 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
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH01421/14A 2013-09-25 2014-09-19 Innengekühlter Übergangskanalhinterrahmen. CH708646A2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/036,101 US9574498B2 (en) 2013-09-25 2013-09-25 Internally cooled transition duct aft frame with serpentine cooling passage and conduit

Publications (1)

Publication Number Publication Date
CH708646A2 true CH708646A2 (de) 2015-03-31

Family

ID=52623741

Family Applications (1)

Application Number Title Priority Date Filing Date
CH01421/14A CH708646A2 (de) 2013-09-25 2014-09-19 Innengekühlter Übergangskanalhinterrahmen.

Country Status (5)

Country Link
US (1) US9574498B2 (enExample)
JP (1) JP6431730B2 (enExample)
CN (1) CN104515146B (enExample)
CH (1) CH708646A2 (enExample)
DE (1) DE102014113326A1 (enExample)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6289887B1 (en) 1998-08-07 2001-09-18 Portafire, Inc. Artificial campfire device
EP3325887A1 (en) * 2015-07-24 2018-05-30 Siemens Aktiengesellschaft Gas turbine transition duct with late lean injection having reduced combustion residence time
US9989260B2 (en) * 2015-12-22 2018-06-05 General Electric Company Staged fuel and air injection in combustion systems of gas turbines
US11493066B2 (en) * 2016-01-20 2022-11-08 Soliton Holdings Generalized jet-effect and enhanced devices
JP6584687B2 (ja) 2016-03-01 2019-10-02 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ ガスタービンエンジン内の圧縮機組立体の下流側のミッドフレームトルクディスク用の圧縮機ブリード冷却システム
US10830142B2 (en) * 2016-10-10 2020-11-10 General Electric Company Combustor aft frame cooling
US10577957B2 (en) * 2017-10-13 2020-03-03 General Electric Company Aft frame assembly for gas turbine transition piece
US11215072B2 (en) 2017-10-13 2022-01-04 General Electric Company Aft frame assembly for gas turbine transition piece
US10684016B2 (en) 2017-10-13 2020-06-16 General Electric Company Aft frame assembly for gas turbine transition piece
US10718224B2 (en) * 2017-10-13 2020-07-21 General Electric Company AFT frame assembly for gas turbine transition piece
US11092339B2 (en) * 2018-01-12 2021-08-17 Raytheon Technologies Corporation Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages
CA3222070A1 (en) * 2022-12-14 2024-06-14 Cenovus Energy Inc. Modified allam cycle system and method for hydrocarbon recovery steam generation

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4195474A (en) * 1977-10-17 1980-04-01 General Electric Company Liquid-cooled transition member to turbine inlet
JPS62150453U (enExample) * 1986-03-14 1987-09-24
US5414999A (en) 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
US5906093A (en) * 1997-02-21 1999-05-25 Siemens Westinghouse Power Corporation Gas turbine combustor transition
JP3310900B2 (ja) * 1997-04-15 2002-08-05 三菱重工業株式会社 燃焼器尾筒の冷却構造
US6412268B1 (en) * 2000-04-06 2002-07-02 General Electric Company Cooling air recycling for gas turbine transition duct end frame and related method
EP1146289B1 (en) * 2000-04-13 2008-12-24 Mitsubishi Heavy Industries, Ltd. Cooling structure of combustor tail tube
JP2002243154A (ja) * 2001-02-16 2002-08-28 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器
US6568187B1 (en) * 2001-12-10 2003-05-27 Power Systems Mfg, Llc Effusion cooled transition duct
US6619915B1 (en) 2002-08-06 2003-09-16 Power Systems Mfg, Llc Thermally free aft frame for a transition duct
US6662567B1 (en) 2002-08-14 2003-12-16 Power Systems Mfg, Llc Transition duct mounting system
US7178340B2 (en) 2003-09-24 2007-02-20 Power Systems Mfg., Llc Transition duct honeycomb seal
US7178341B2 (en) * 2004-06-17 2007-02-20 Siemens Power Generation, Inc. Multi-zone tubing assembly for a transition piece of a gas turbine
US8015818B2 (en) * 2005-02-22 2011-09-13 Siemens Energy, Inc. Cooled transition duct for a gas turbine engine
US7789626B1 (en) * 2007-05-31 2010-09-07 Florida Turbine Technologies, Inc. Turbine blade with showerhead film cooling holes
US8418474B2 (en) 2008-01-29 2013-04-16 Alstom Technology Ltd. Altering a natural frequency of a gas turbine transition duct
US8186167B2 (en) 2008-07-07 2012-05-29 General Electric Company Combustor transition piece aft end cooling and related method
US8245515B2 (en) 2008-08-06 2012-08-21 General Electric Company Transition duct aft end frame cooling and related method
US8707705B2 (en) * 2009-09-03 2014-04-29 General Electric Company Impingement cooled transition piece aft frame
JP2012145098A (ja) * 2010-12-21 2012-08-02 Toshiba Corp トランジションピースおよびガスタービン
US20120186260A1 (en) 2011-01-25 2012-07-26 General Electric Company Transition piece impingement sleeve for a gas turbine
US9255484B2 (en) * 2011-03-16 2016-02-09 General Electric Company Aft frame and method for cooling aft frame

Also Published As

Publication number Publication date
US9574498B2 (en) 2017-02-21
DE102014113326A1 (de) 2015-03-26
US20150082795A1 (en) 2015-03-26
JP2015063994A (ja) 2015-04-09
CN104515146A (zh) 2015-04-15
JP6431730B2 (ja) 2018-11-28
CN104515146B (zh) 2019-04-09

Similar Documents

Publication Publication Date Title
CH708646A2 (de) Innengekühlter Übergangskanalhinterrahmen.
DE102014103022B4 (de) Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine
DE102014103082A1 (de) Strömungshülse für ein Brennkammermodul für eine Gasturbine
DE102014110166A1 (de) System zur Belieferung einer Brennkammer mit Brennstoff
DE102014108829B4 (de) Mantelringblocksegment für eine Gasturbine
DE102014103081A1 (de) Strömungshülsenanordnung für ein Verbrennungsmodul eines Gasturbinenbrenners
DE102014103088A1 (de) System zur Steuerung der Flussrate eines komprimierten Arbeitsfluids zu einem Brennstoffinjektor eines Brenners
DE102011000225A1 (de) Über einen Anzapfdiffusor gespeistes sekundäres Verbrennungssystem für Gasturbinen
CH710574B1 (de) System und Verfahren zur Nutzung von Kühlluft in einem Brenner.
CH707852A2 (de) System zur Zuführung von Brennstoff zu einer Brennkammer.
DE102015113006A1 (de) Brennkammerkappenanordnung
DE102008037385A1 (de) Auskleidungsanordnung mit Turbulatoren am hinteren Ende und Kühlverfahren
DE102012100373A1 (de) System und Verfahren für einen Gasturbinenauslassdiffusor
DE102013114973A1 (de) Brennstoffinjektor zur Zuführung von Brennstoff zu einer Brennkammer
DE102015119750A1 (de) Bündelrohr-Brennstoffdüse
DE102016106491A1 (de) Brennstoffdüsenanordnung mit einer Pilotdüse
DE102015120448A1 (de) Vormischbrennstoffdüsenanordnung
DE102014115402A1 (de) Übergangskanalanordnung mit modifizierter Hinterkante in einem Turbinensystem
DE102014109288A1 (de) Gasturbinen-Deckbandkühlung
EP2719869A1 (de) Axiale Abdichtung in einer Gehäusestruktur für eine Strömungsmaschine
DE102015113146A1 (de) Systeme und Vorrichtungen im Zusammenhang mit Gasturbinenbrennkammern
CH710425A2 (de) Vormischbrennstoffdüsenanordnung.
DE102015105578A1 (de) Brennstoffzufuhrsystem
DE102015113009A1 (de) Brennkammerkappenanordnung
CH702543A2 (de) Turbomaschine mit einer Einspritzdüsenanordnung.

Legal Events

Date Code Title Description
NV New agent

Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH

AZW Rejection (application)