BR112014027018B1 - virola de câmara de combustão de turbomáquina, e, câmara de combustão de turbomáquina - Google Patents
virola de câmara de combustão de turbomáquina, e, câmara de combustão de turbomáquina Download PDFInfo
- Publication number
- BR112014027018B1 BR112014027018B1 BR112014027018-0A BR112014027018A BR112014027018B1 BR 112014027018 B1 BR112014027018 B1 BR 112014027018B1 BR 112014027018 A BR112014027018 A BR 112014027018A BR 112014027018 B1 BR112014027018 B1 BR 112014027018B1
- Authority
- BR
- Brazil
- Prior art keywords
- ferrule
- holes
- inserts
- dilution
- combustion chamber
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 18
- 238000010790 dilution Methods 0.000 claims abstract description 35
- 239000012895 dilution Substances 0.000 claims abstract description 35
- 238000009423 ventilation Methods 0.000 claims abstract description 7
- 230000015572 biosynthetic process Effects 0.000 abstract description 2
- 238000013021 overheating Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 239000003546 flue gas Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000000112 cooling gas Substances 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Images
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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03041—Effusion cooled combustion chamber walls or domes
-
- 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
- F23R2900/03042—Film cooled combustion chamber walls or domes
-
- 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
-
- 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
- F23R3/06—Arrangement of apertures along the flame tube
-
- 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
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
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)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1254847A FR2991028B1 (fr) | 2012-05-25 | 2012-05-25 | Virole de chambre de combustion de turbomachine |
| FR1254847 | 2012-05-25 | ||
| PCT/FR2013/051117 WO2013175126A2 (fr) | 2012-05-25 | 2013-05-23 | Virole de chambre de combustion de turbomachine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BR112014027018A2 BR112014027018A2 (pt) | 2017-06-27 |
| BR112014027018B1 true BR112014027018B1 (pt) | 2021-05-25 |
Family
ID=46754628
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR112014027018-0A BR112014027018B1 (pt) | 2012-05-25 | 2013-05-23 | virola de câmara de combustão de turbomáquina, e, câmara de combustão de turbomáquina |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US9377200B2 (enExample) |
| EP (1) | EP2856036B1 (enExample) |
| CN (1) | CN104520647B (enExample) |
| BR (1) | BR112014027018B1 (enExample) |
| CA (1) | CA2871923C (enExample) |
| FR (1) | FR2991028B1 (enExample) |
| IN (1) | IN2014DN08528A (enExample) |
| RU (1) | RU2626876C2 (enExample) |
| WO (1) | WO2013175126A2 (enExample) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102012022259A1 (de) * | 2012-11-13 | 2014-05-28 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammerschindel einer Gasturbine sowie Verfahren zu deren Herstellung |
| WO2015100346A1 (en) | 2013-12-23 | 2015-07-02 | United Technologies Corporation | Multi-streamed dilution hole configuration for a gas turbine engine |
| US10451281B2 (en) * | 2014-11-04 | 2019-10-22 | United Technologies Corporation | Low lump mass combustor wall with quench aperture(s) |
| US10386072B2 (en) * | 2015-09-02 | 2019-08-20 | Pratt & Whitney Canada Corp. | Internally cooled dilution hole bosses for gas turbine engine combustors |
| US20180283689A1 (en) * | 2017-04-03 | 2018-10-04 | General Electric Company | Film starters in combustors of gas turbine engines |
| US11187412B2 (en) | 2018-08-22 | 2021-11-30 | General Electric Company | Flow control wall assembly for heat engine |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1052475A (fr) * | 1952-03-15 | 1954-01-25 | Snecma | Chambres de combustion convenant en particulier aux turbines à gaz |
| GB777782A (en) | 1955-06-24 | 1957-06-26 | Ici Ltd | Purification of terephthalic acid |
| US4132066A (en) * | 1977-09-23 | 1979-01-02 | United Technologies Corporation | Combustor liner for gas turbine engine |
| US4875339A (en) * | 1987-11-27 | 1989-10-24 | General Electric Company | Combustion chamber liner insert |
| US4887432A (en) * | 1988-10-07 | 1989-12-19 | Westinghouse Electric Corp. | Gas turbine combustion chamber with air scoops |
| FR2855249B1 (fr) * | 2003-05-20 | 2005-07-08 | Snecma Moteurs | Chambre de combustion ayant une liaison souple entre un fond de chambre et une paroi de chambre |
| RU2260748C2 (ru) * | 2003-12-02 | 2005-09-20 | Открытое акционерное общество "Авиадвигатель" | Камера сгорания газотурбинного двигателя |
| FR2881813B1 (fr) * | 2005-02-09 | 2011-04-08 | Snecma Moteurs | Carenage de chambre de combustion de turbomachine |
| FR2892180B1 (fr) * | 2005-10-18 | 2008-02-01 | Snecma Sa | Amelioration des perfomances d'une chambre de combustion par multiperforation des parois |
| FR2899315B1 (fr) | 2006-03-30 | 2012-09-28 | Snecma | Configuration d'ouvertures de dilution dans une paroi de chambre de combustion de turbomachine |
| US8171634B2 (en) * | 2007-07-09 | 2012-05-08 | Pratt & Whitney Canada Corp. | Method of producing effusion holes |
| US8789372B2 (en) * | 2009-07-08 | 2014-07-29 | General Electric Company | Injector with integrated resonator |
-
2012
- 2012-05-25 FR FR1254847A patent/FR2991028B1/fr active Active
-
2013
- 2013-05-23 EP EP13728462.6A patent/EP2856036B1/fr active Active
- 2013-05-23 CN CN201380023683.6A patent/CN104520647B/zh active Active
- 2013-05-23 BR BR112014027018-0A patent/BR112014027018B1/pt active IP Right Grant
- 2013-05-23 WO PCT/FR2013/051117 patent/WO2013175126A2/fr not_active Ceased
- 2013-05-23 RU RU2014152849A patent/RU2626876C2/ru active
- 2013-05-23 IN IN8528DEN2014 patent/IN2014DN08528A/en unknown
- 2013-05-23 US US14/394,214 patent/US9377200B2/en active Active
- 2013-05-23 CA CA2871923A patent/CA2871923C/fr active Active
Also Published As
| Publication number | Publication date |
|---|---|
| FR2991028A1 (fr) | 2013-11-29 |
| RU2014152849A (ru) | 2016-07-20 |
| EP2856036A2 (fr) | 2015-04-08 |
| IN2014DN08528A (enExample) | 2015-05-15 |
| WO2013175126A2 (fr) | 2013-11-28 |
| WO2013175126A3 (fr) | 2014-04-24 |
| CN104520647B (zh) | 2016-02-24 |
| FR2991028B1 (fr) | 2014-07-04 |
| US9377200B2 (en) | 2016-06-28 |
| US20150059344A1 (en) | 2015-03-05 |
| CA2871923A1 (fr) | 2013-11-28 |
| CA2871923C (fr) | 2020-02-11 |
| RU2626876C2 (ru) | 2017-08-02 |
| BR112014027018A2 (pt) | 2017-06-27 |
| EP2856036B1 (fr) | 2018-09-12 |
| CN104520647A (zh) | 2015-04-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| BR112014027018B1 (pt) | virola de câmara de combustão de turbomáquina, e, câmara de combustão de turbomáquina | |
| CN101737103B (zh) | 关于护罩冷却的方法及设备 | |
| BR112016027042B1 (pt) | Pá de turbina de turbomáquina, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina | |
| JP5715331B2 (ja) | ターボ機械用のタービンバケット及びタービンバケットにおける頭部波作用を減少させる方法 | |
| BR112016027014B1 (pt) | Pá de turbina de turbomotor, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina | |
| BRPI1011134B1 (pt) | Turbomáquina com duplo corpo | |
| JP3940377B2 (ja) | 燃焼室の端の二重インジェクタシステムによる高圧タービンの上流端プレートの冷却 | |
| JP2011513638A (ja) | 端部の冷却を備えているタービン翼ならびに関連のタービンおよびターボエンジン | |
| BR112013021367B1 (pt) | parede anular para câmara de combustão de turbomáquina, câmara anular de combustão de turbomáquina e turbomáquina | |
| CN105626160A (zh) | 涡轮叶片及用于冷却涡轮叶片与叶轮柱之间的轮缘间隙的方法 | |
| BR112012028640B1 (pt) | Conjunto de pás para compressor de turbomáquina, compressor de turbomáquina e turbomáquina | |
| BR102016025774A2 (pt) | combustor para um motor de turbina a gás | |
| BR102016002632A2 (pt) | motor elétrico | |
| CN102798151A (zh) | 用于将燃料供应到燃烧室的燃烧室喷嘴和方法 | |
| CN104884741B (zh) | 用于涡轮机的叶片 | |
| BR102016005720A2 (pt) | sistema para resfriamento de um envoltório de turbina | |
| US20160102562A1 (en) | Cooling arrangement for gas turbine blade platform | |
| JP2018505339A (ja) | フィルム冷却されるガスタービン構成部品 | |
| BR112012008509B1 (pt) | Dispositivo de injeção de combustível para uma câmara anular de combustão de turbomáquina, e, câmara anular de combustão de turbomáquina | |
| CN106536858B (zh) | 具有顺翼展延伸流阻断器的涡轮翼型件冷却系统 | |
| CN101900132B (zh) | 涡轮机压缩机叶轮部件 | |
| ES2402886T3 (es) | Motor de turbina de gas | |
| BR112016006688B1 (pt) | Câmara de combustão anular para turbomáquina com admissão de ar homogêneo através de sistemas de injeção de carburante, módulo de câmara de combustão e turbomáquina para aeronave | |
| BR112016006421B1 (pt) | Injetor de combustível, câmara de combustão e turbomáquina | |
| JP2018538473A (ja) | 冷却システムが装備されたブレード、付随するガイドベーンアセンブリおよび付随するターボ機械 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
| B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
| B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
| B16A | Patent or certificate of addition of invention granted |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 23/05/2013, OBSERVADAS AS CONDICOES LEGAIS. |