SA113340835B1 - نظام مُخمّد صوتي لغرفة احتراق - Google Patents
نظام مُخمّد صوتي لغرفة احتراقInfo
- Publication number
- SA113340835B1 SA113340835B1 SA113340835A SA113340835A SA113340835B1 SA 113340835 B1 SA113340835 B1 SA 113340835B1 SA 113340835 A SA113340835 A SA 113340835A SA 113340835 A SA113340835 A SA 113340835A SA 113340835 B1 SA113340835 B1 SA 113340835B1
- Authority
- SA
- Saudi Arabia
- Prior art keywords
- damper arrangement
- acoustic damper
- combustor
- inner liner
- hollow body
- Prior art date
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
-
- 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
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
- F23M20/005—Noise absorbing means
-
- 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
- F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Sealing Devices (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
يتم الكشف عن نظام مُخمًد صوتي لغرفة احتراق ذات بطانة داخلية معدّة للاستخدام في درجة حرارة أولى أثناء التشغيل وبطانة خارجية معدّة للتشغيل في درجة حرارة ثانية أكثر انخفاضاً من درجة الحرارة الأولى أثناء التشغيل، يشتمل نظام المُخمّد الصوتي على: عددٍ من الألواح المرنة؛ وجسم مجوّف واحد على الأقل ذات حجم داخلي، يكون كل واحد من الأجسام المجوّفة على الأقل مثبتاً على واحد من الألواح المرنة، حيث يكون نظام المُخمّد الصوتي معداً لكي يثبّت على كل من البطانة الداخلية والبطانة الخارجية بحيث يكون الحجم الداخلي للجسم المجوّف الواحد على الأقل على اتصال مع حجرة مُشكلة عن طريق البطانة الداخلية، ويستوعب التعداد من الألواح المرنة توسع وتقلص البطانة الداخلية بالنسبة للبطانة الخارجية. الشكل 3
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261698958P | 2012-09-10 | 2012-09-10 | |
US13/689,926 US8684130B1 (en) | 2012-09-10 | 2012-11-30 | Damping system for combustor |
Publications (1)
Publication Number | Publication Date |
---|---|
SA113340835B1 true SA113340835B1 (ar) | 2015-09-01 |
Family
ID=49033934
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SA113340835A SA113340835B1 (ar) | 2012-09-10 | 2013-09-09 | نظام مُخمّد صوتي لغرفة احتراق |
Country Status (8)
Country | Link |
---|---|
US (1) | US8684130B1 (ar) |
EP (1) | EP2716972B1 (ar) |
JP (1) | JP5734375B2 (ar) |
KR (1) | KR101551673B1 (ar) |
CN (1) | CN103672971B (ar) |
CA (1) | CA2826099C (ar) |
RU (1) | RU2551707C2 (ar) |
SA (1) | SA113340835B1 (ar) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2516286B (en) * | 2013-07-18 | 2016-08-17 | Rolls Royce Plc | A duct and method for damping pressure waves caused by thermoacoustic instability |
US10267523B2 (en) * | 2014-09-15 | 2019-04-23 | Ansaldo Energia Ip Uk Limited | Combustor dome damper system |
WO2016089341A1 (en) * | 2014-12-01 | 2016-06-09 | Siemens Aktiengesellschaft | Resonators with interchangeable metering tubes for gas turbine engines |
EP3048370A1 (en) | 2015-01-23 | 2016-07-27 | Siemens Aktiengesellschaft | Combustion chamber for a gas turbine engine |
RU2643927C1 (ru) * | 2016-06-06 | 2018-02-06 | Акционерное общество Центральный научно-исследовательский институт специального машиностроения | Камера сгорания прямоточного воздушно-реактивного двигателя из композиционных материалов |
US10221769B2 (en) | 2016-12-02 | 2019-03-05 | General Electric Company | System and apparatus for gas turbine combustor inner cap and extended resonating tubes |
US10220474B2 (en) | 2016-12-02 | 2019-03-05 | General Electricd Company | Method and apparatus for gas turbine combustor inner cap and high frequency acoustic dampers |
US10228138B2 (en) | 2016-12-02 | 2019-03-12 | General Electric Company | System and apparatus for gas turbine combustor inner cap and resonating tubes |
US11506382B2 (en) | 2019-09-12 | 2022-11-22 | General Electric Company | System and method for acoustic dampers with multiple volumes in a combustion chamber front panel |
CN115682033A (zh) * | 2021-07-28 | 2023-02-03 | 北京航空航天大学 | 防振燃烧室以及燃烧室防振方法 |
CN113719861B (zh) * | 2021-09-10 | 2022-12-06 | 中国联合重型燃气轮机技术有限公司 | 燃烧室和具有该燃烧室的燃气轮机 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2135824C3 (de) * | 1971-07-17 | 1981-10-29 | Robert Bosch Gmbh, 7000 Stuttgart | Luftmengenmesser mit einer im Ansaugkanal einer Brennkraftmaschine im wesentlichen quer zur Ansaugluftströmung angeordnete Stauscheibe |
DE19506511C2 (de) * | 1995-02-24 | 1998-08-27 | Fraunhofer Ges Forschung | Plattenresonator |
US5685157A (en) * | 1995-05-26 | 1997-11-11 | General Electric Company | Acoustic damper for a gas turbine engine combustor |
US6334310B1 (en) | 2000-06-02 | 2002-01-01 | General Electric Company | Fracture resistant support structure for a hula seal in a turbine combustor and related method |
US6530221B1 (en) * | 2000-09-21 | 2003-03-11 | Siemens Westinghouse Power Corporation | Modular resonators for suppressing combustion instabilities in gas turbine power plants |
JP2005527761A (ja) | 2001-09-07 | 2005-09-15 | アルストム テクノロジー リミテッド | ガスタービン装置の燃焼室脈動を低減する減衰装置 |
US7010921B2 (en) * | 2004-06-01 | 2006-03-14 | General Electric Company | Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
US7334408B2 (en) * | 2004-09-21 | 2008-02-26 | Siemens Aktiengesellschaft | Combustion chamber for a gas turbine with at least two resonator devices |
US7552796B2 (en) * | 2006-04-27 | 2009-06-30 | United Technologies Corporation | Turbine engine tailcone resonator |
US8079219B2 (en) | 2008-09-30 | 2011-12-20 | General Electric Company | Impingement cooled combustor seal |
US8025122B2 (en) * | 2008-11-06 | 2011-09-27 | The Boeing Company | Acoustically treated exhaust centerbody for jet engines and associated methods |
US8490744B2 (en) * | 2009-02-27 | 2013-07-23 | Mitsubishi Heavy Industries, Ltd. | Combustor and gas turbine having the same |
US8429919B2 (en) | 2009-05-28 | 2013-04-30 | General Electric Company | Expansion hula seals |
EP2362147B1 (en) * | 2010-02-22 | 2012-12-26 | Alstom Technology Ltd | Combustion device for a gas turbine |
EP2383515B1 (de) * | 2010-04-28 | 2013-06-19 | Siemens Aktiengesellschaft | Brennersystem zur Dämpfung eines solchen Brennersystems |
US8621842B2 (en) * | 2010-05-05 | 2014-01-07 | Hamilton Sundstrand Corporation | Exhaust silencer convection cooling |
US8973365B2 (en) | 2010-10-29 | 2015-03-10 | Solar Turbines Incorporated | Gas turbine combustor with mounting for Helmholtz resonators |
US20120180500A1 (en) | 2011-01-13 | 2012-07-19 | General Electric Company | System for damping vibration in a gas turbine engine |
-
2012
- 2012-11-30 US US13/689,926 patent/US8684130B1/en active Active
-
2013
- 2013-08-26 EP EP13181701.7A patent/EP2716972B1/en active Active
- 2013-09-04 CA CA2826099A patent/CA2826099C/en not_active Expired - Fee Related
- 2013-09-09 KR KR1020130107807A patent/KR101551673B1/ko not_active IP Right Cessation
- 2013-09-09 SA SA113340835A patent/SA113340835B1/ar unknown
- 2013-09-09 RU RU2013141399/06A patent/RU2551707C2/ru active
- 2013-09-10 JP JP2013187373A patent/JP5734375B2/ja not_active Expired - Fee Related
- 2013-09-10 CN CN201310408451.4A patent/CN103672971B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
JP5734375B2 (ja) | 2015-06-17 |
EP2716972A1 (en) | 2014-04-09 |
CN103672971A (zh) | 2014-03-26 |
KR101551673B1 (ko) | 2015-09-09 |
KR20140034079A (ko) | 2014-03-19 |
CA2826099A1 (en) | 2014-03-10 |
RU2551707C2 (ru) | 2015-05-27 |
JP2014051983A (ja) | 2014-03-20 |
US20140069738A1 (en) | 2014-03-13 |
RU2013141399A (ru) | 2015-03-20 |
CA2826099C (en) | 2016-02-23 |
EP2716972B1 (en) | 2019-04-17 |
CN103672971B (zh) | 2015-10-07 |
US8684130B1 (en) | 2014-04-01 |
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