KR100760560B1 - 화염 튜브 - Google Patents
화염 튜브 Download PDFInfo
- Publication number
- KR100760560B1 KR100760560B1 KR1020020081808A KR20020081808A KR100760560B1 KR 100760560 B1 KR100760560 B1 KR 100760560B1 KR 1020020081808 A KR1020020081808 A KR 1020020081808A KR 20020081808 A KR20020081808 A KR 20020081808A KR 100760560 B1 KR100760560 B1 KR 100760560B1
- Authority
- KR
- South Korea
- Prior art keywords
- flame tube
- cylindrical
- holes
- hole
- cylindrical region
- 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 - Fee Related
Links
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
- 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
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
-
- 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)
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ITMI2001A002785 | 2001-12-21 | ||
| IT2001MI002785A ITMI20012785A1 (it) | 2001-12-21 | 2001-12-21 | Tubo di fianna o "liner" migliorato per una camera di combustione di una turbina a gas a basse emissioni inquinanti |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| KR20030053436A KR20030053436A (ko) | 2003-06-28 |
| KR100760560B1 true KR100760560B1 (ko) | 2007-09-20 |
Family
ID=11448750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR1020020081808A Expired - Fee Related KR100760560B1 (ko) | 2001-12-21 | 2002-12-20 | 화염 튜브 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US6966187B2 (enExample) |
| EP (1) | EP1321713B1 (enExample) |
| JP (1) | JP4362283B2 (enExample) |
| KR (1) | KR100760560B1 (enExample) |
| CA (1) | CA2413655C (enExample) |
| DE (1) | DE60225411T2 (enExample) |
| IT (1) | ITMI20012785A1 (enExample) |
| RU (1) | RU2302586C2 (enExample) |
| TW (1) | TWI312851B (enExample) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ITMI20012781A1 (it) * | 2001-12-21 | 2003-06-21 | Nuovo Pignone Spa | Assieme migliorato di camera di pre miscelamento e di camera di combustione, a basse emissioni inquinanti per turbine a gas con combustibile |
| ITMI20032621A1 (it) * | 2003-12-30 | 2005-06-30 | Nuovo Pignone Spa | Sistema di combustione a basse emissioni inquinanti |
| CA2457609A1 (en) * | 2004-02-13 | 2005-08-13 | Alberta Research Council Inc. | Heating solid oxide fuel cell stack |
| US7350619B2 (en) * | 2004-09-23 | 2008-04-01 | Honeywell International, Inc. | Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner |
| EP1832812A3 (de) * | 2006-03-10 | 2012-01-04 | Rolls-Royce Deutschland Ltd & Co KG | Gasturbinenbrennkammerwand mit Dämpfung von Brennkammerschwingungen |
| US8156743B2 (en) * | 2006-05-04 | 2012-04-17 | General Electric Company | Method and arrangement for expanding a primary and secondary flame in a combustor |
| EP2245374B1 (de) * | 2008-02-20 | 2017-11-15 | General Electric Technology GmbH | Thermische maschine |
| EP2187125A1 (de) * | 2008-09-24 | 2010-05-19 | Siemens Aktiengesellschaft | Vorrichtung und Verfahren zur Dämpfung von Verbrennungsschwingungen |
| US8863525B2 (en) | 2011-01-03 | 2014-10-21 | General Electric Company | Combustor with fuel staggering for flame holding mitigation |
| US20120208141A1 (en) * | 2011-02-14 | 2012-08-16 | General Electric Company | Combustor |
| EP2644995A1 (en) | 2012-03-27 | 2013-10-02 | Siemens Aktiengesellschaft | An improved hole arrangement of liners of a combustion chamber of a gas turbine engine with low combustion dynamics and emissions |
| US20140033726A1 (en) * | 2012-08-06 | 2014-02-06 | Wei Chen | Liner cooling assembly for a gas turbine system |
| US10533750B2 (en) | 2014-09-05 | 2020-01-14 | Siemens Aktiengesellschaft | Cross ignition flame duct |
| US10753610B2 (en) * | 2015-03-30 | 2020-08-25 | Nuovo Pignone Srl | Interchangeable liner support for gas turbine combusters |
| JP7262364B2 (ja) | 2019-10-17 | 2023-04-21 | 三菱重工業株式会社 | ガスタービン燃焼器 |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4833881A (en) | 1984-12-17 | 1989-05-30 | General Electric Company | Gas turbine engine augmentor |
| US5417056A (en) | 1992-01-02 | 1995-05-23 | General Electric Company | Axially translating screen suppressor for a gas turbine engine augmentor |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5129726A (enExample) * | 1974-09-06 | 1976-03-13 | Mitsubishi Heavy Ind Ltd | |
| US4201047A (en) * | 1976-06-10 | 1980-05-06 | Morgan J Randolph | Low emission combustors |
| FR2381911A1 (fr) * | 1977-02-25 | 1978-09-22 | Guidas | Chambre de combustion perfectionnee notamment pour une turbine a gaz |
| GB1570875A (en) * | 1977-03-16 | 1980-07-09 | Lucas Industries Ltd | Combustion equipment |
| US4498288A (en) * | 1978-10-13 | 1985-02-12 | General Electric Company | Fuel injection staged sectoral combustor for burning low-BTU fuel gas |
| RU2062406C1 (ru) * | 1994-04-28 | 1996-06-20 | Акционерное общество "Авиадвигатель" | Камера сгорания газотурбинного двигателя |
| GB2309296B (en) * | 1995-10-11 | 2000-02-09 | Europ Gas Turbines Ltd | Gas turbine engine combuster |
| GB2328011A (en) * | 1997-08-05 | 1999-02-10 | Europ Gas Turbines Ltd | Combustor for gas or liquid fuelled turbine |
| US6098397A (en) * | 1998-06-08 | 2000-08-08 | Caterpillar Inc. | Combustor for a low-emissions gas turbine engine |
| RU2162988C2 (ru) * | 1999-02-22 | 2001-02-10 | Открытое акционерное общество "Авиадвигатель" | Камера сгорания газотурбинной установки |
| GB9926257D0 (en) * | 1999-11-06 | 2000-01-12 | Rolls Royce Plc | Wall elements for gas turbine engine combustors |
| US6446438B1 (en) * | 2000-06-28 | 2002-09-10 | Power Systems Mfg., Llc | Combustion chamber/venturi cooling for a low NOx emission combustor |
| US6427446B1 (en) * | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
| JP4610800B2 (ja) * | 2001-06-29 | 2011-01-12 | 三菱重工業株式会社 | ガスタービン燃焼器 |
-
2001
- 2001-12-21 IT IT2001MI002785A patent/ITMI20012785A1/it unknown
-
2002
- 2002-12-05 CA CA002413655A patent/CA2413655C/en not_active Expired - Lifetime
- 2002-12-10 TW TW091135661A patent/TWI312851B/zh not_active IP Right Cessation
- 2002-12-17 US US10/320,726 patent/US6966187B2/en not_active Expired - Lifetime
- 2002-12-18 EP EP02258733A patent/EP1321713B1/en not_active Revoked
- 2002-12-18 DE DE60225411T patent/DE60225411T2/de not_active Expired - Lifetime
- 2002-12-20 JP JP2002369154A patent/JP4362283B2/ja not_active Expired - Fee Related
- 2002-12-20 KR KR1020020081808A patent/KR100760560B1/ko not_active Expired - Fee Related
- 2002-12-20 RU RU2002134607/06A patent/RU2302586C2/ru active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4833881A (en) | 1984-12-17 | 1989-05-30 | General Electric Company | Gas turbine engine augmentor |
| US5417056A (en) | 1992-01-02 | 1995-05-23 | General Electric Company | Axially translating screen suppressor for a gas turbine engine augmentor |
Also Published As
| Publication number | Publication date |
|---|---|
| CA2413655C (en) | 2009-11-17 |
| JP2003207133A (ja) | 2003-07-25 |
| US20030118963A1 (en) | 2003-06-26 |
| RU2302586C2 (ru) | 2007-07-10 |
| CA2413655A1 (en) | 2003-06-21 |
| EP1321713A2 (en) | 2003-06-25 |
| ITMI20012785A1 (it) | 2003-06-21 |
| TW200409886A (en) | 2004-06-16 |
| US6966187B2 (en) | 2005-11-22 |
| DE60225411D1 (de) | 2008-04-17 |
| EP1321713B1 (en) | 2008-03-05 |
| KR20030053436A (ko) | 2003-06-28 |
| JP4362283B2 (ja) | 2009-11-11 |
| EP1321713A3 (en) | 2004-07-14 |
| DE60225411T2 (de) | 2009-03-19 |
| TWI312851B (en) | 2009-08-01 |
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| JP2002168134A (ja) | プレートフィン及びそれを用いた燃焼器 |
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