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
Links
- 235000020637 scallop Nutrition 0.000 abstract 2
- 241000237509 Patinopecten sp. Species 0.000 abstract 1
- 241000237503 Pectinidae Species 0.000 abstract 1
- 238000002485 combustion reaction Methods 0.000 abstract 1
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
- F02C7/24—Heat or noise insulation
-
- 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
- F23R3/10—Air inlet arrangements for primary air
-
- 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)
- 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.
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)
| 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)
| 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 |
-
2013
- 2013-08-02 US US13/957,735 patent/US20150033746A1/en not_active Abandoned
-
2014
- 2014-07-29 WO PCT/US2014/048652 patent/WO2015017427A1/en not_active Ceased
- 2014-07-29 CN CN201480042465.1A patent/CN105408692B/zh active Active
- 2014-07-29 MX MX2016001313A patent/MX2016001313A/es unknown
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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