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MX2016001313A - Protector termico con separadores. - Google Patents

Protector termico con separadores.

Info

Publication number
MX2016001313A
MX2016001313A MX2016001313A MX2016001313A MX2016001313A MX 2016001313 A MX2016001313 A MX 2016001313A MX 2016001313 A MX2016001313 A MX 2016001313A MX 2016001313 A MX2016001313 A MX 2016001313A MX 2016001313 A MX2016001313 A MX 2016001313A
Authority
MX
Mexico
Prior art keywords
standoffs
plate portion
inner ring
heat shield
extends
Prior art date
Application number
MX2016001313A
Other languages
English (en)
Inventor
Daniel William Carey
Robert A Ii Corr
Crosby H Johnson
Yong W Kim
Original Assignee
Solar Turbines Inc
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 Solar Turbines Inc filed Critical Solar Turbines Inc
Publication of MX2016001313A publication Critical patent/MX2016001313A/es

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/24Heat or noise insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044Impingement cooled combustion chamber walls or subassemblies

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)
  • Supercharger (AREA)

Abstract

Se describe protector térmico para una cámara de combustión de un motor de turbina de gas. El protector térmico incluye una porción de placa, un anillo interno y una pluralidad de separadores. La porción de la placa incluye una forma de un sector anular. El anillo interno se extiende desde la parte interna de la porción de la placa. El anillo interno incluye una forma cilíndrica hueca. La pluralidad de separadores se extiende desde la porción de la placa, cercana a los extremos externos de la porción de la placa y en la misma dirección que el anillo interno. La pluralidad de separadores forma una pluralidad de festones. Cada festón se ubica entre los separadores adyacentes.
MX2016001313A 2013-08-02 2014-07-29 Protector termico con separadores. MX2016001313A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/957,735 US20150033746A1 (en) 2013-08-02 2013-08-02 Heat shield with standoffs
PCT/US2014/048652 WO2015017427A1 (en) 2013-08-02 2014-07-29 Heat shield with standoffs

Publications (1)

Publication Number Publication Date
MX2016001313A true MX2016001313A (es) 2016-05-16

Family

ID=52426403

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2016001313A MX2016001313A (es) 2013-08-02 2014-07-29 Protector termico con separadores.

Country Status (4)

Country Link
US (1) US20150033746A1 (es)
CN (1) CN105408692B (es)
MX (1) MX2016001313A (es)
WO (1) WO2015017427A1 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9534784B2 (en) * 2013-08-23 2017-01-03 Pratt & Whitney Canada Corp. Asymmetric combustor heat shield panels
US10604087B2 (en) 2015-06-02 2020-03-31 Lydall, Inc. Heat shield with sealing member
US10724740B2 (en) 2016-11-04 2020-07-28 General Electric Company Fuel nozzle assembly with impingement purge
US10634353B2 (en) * 2017-01-12 2020-04-28 General Electric Company Fuel nozzle assembly with micro channel cooling
US10837640B2 (en) * 2017-03-06 2020-11-17 General Electric Company Combustion section of a gas turbine engine
US11187412B2 (en) * 2018-08-22 2021-11-30 General Electric Company Flow control wall assembly for heat engine
US12326278B2 (en) 2022-02-28 2025-06-10 EnhancedGEO Holdings, LLC Geothermal power from superhot geothermal fluid and magma reservoirs
CN118361754A (zh) * 2023-01-19 2024-07-19 通用电气公司 用于燃气涡轮的燃烧器的圆顶-导流器组件
US11912573B1 (en) 2023-03-03 2024-02-27 EnhancedGEO Holdings, LLC Molten-salt mediated thermochemical reactions using geothermal energy

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9112324D0 (en) * 1991-06-07 1991-07-24 Rolls Royce Plc Gas turbine engine combustor
US6032457A (en) * 1996-06-27 2000-03-07 United Technologies Corporation Fuel nozzle guide
US6497105B1 (en) * 2001-06-04 2002-12-24 Pratt & Whitney Canada Corp. Low cost combustor burner collar
US7363763B2 (en) * 2003-10-23 2008-04-29 United Technologies Corporation Combustor
DE112007002152T5 (de) * 2006-09-14 2009-07-23 Solar Turbines Inc., San Diego Prallplattenkuppelanordnung für einen Turbinenmotor
US7665306B2 (en) * 2007-06-22 2010-02-23 Honeywell International Inc. Heat shields for use in combustors
EP2182285A1 (de) * 2008-10-29 2010-05-05 Siemens Aktiengesellschaft Brennereinsatz für eine Gasturbinenbrennkammer und Gasturbine
US9377198B2 (en) * 2012-01-31 2016-06-28 United Technologies Corporation Heat shield for a combustor
CN102889616B (zh) * 2012-09-29 2014-07-23 中国科学院工程热物理研究所 一种基于文丘里预混双旋喷嘴的多点直喷燃烧室

Also Published As

Publication number Publication date
CN105408692A (zh) 2016-03-16
CN105408692B (zh) 2017-07-07
WO2015017427A1 (en) 2015-02-05
US20150033746A1 (en) 2015-02-05

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