SA518391117B1 - حقن ماء على ثلاث مراحل يتم التحكم فيه بشكل مستقل في حارق انتشار - Google Patents
حقن ماء على ثلاث مراحل يتم التحكم فيه بشكل مستقل في حارق انتشارInfo
- Publication number
- SA518391117B1 SA518391117B1 SA518391117A SA518391117A SA518391117B1 SA 518391117 B1 SA518391117 B1 SA 518391117B1 SA 518391117 A SA518391117 A SA 518391117A SA 518391117 A SA518391117 A SA 518391117A SA 518391117 B1 SA518391117 B1 SA 518391117B1
- Authority
- SA
- Saudi Arabia
- Prior art keywords
- water
- nozzle
- water injection
- fuel
- injected
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
يتعلق الاختراع الحالي بنظام احتراق combustion system لمحرك تربيني turbine engine ، حيث يتضمن تجميعة فوهة وقود fuel nozzle assembly لها ثلاث مراحل من حقن الماء يتم التحكم فيها بشكل مستقل. تتضمن المرحلة الأولى ماء مختلط بوقود غازي gaseous fuel عند الدخول إلى الفوهة، حيث يختلط ماء المرحلة الأولى وينتقل مع الوقود الغازي المراد حقنه داخل الحارق . وتتضمن المرحلة الثنية ماء تم حقنه داخل الحارق عن طريق فوهة سائل ثانوية secondary liquid nozzle يتم استخدامها لزيت الوقود أثناء عملية الوقود السائل، ولكن يمكن استخدامها للماء الثانوي أثناء عملية الوقود الغازي gaseous fuel . تتضمن المرحلة الثلاثية ماء تم حقنه داخل الحارق عن طريق مجموعة من ثقوب الفوهة المعروفة بغطاء الهواء الرذاذ. يتم أيضاً تحديد طريقة القياس والمعيار للتحكم في المراحل الثلاثة لحقن الماء لتحقيق توازن أمثل للمعيار التشغيلي للتربين بما في ذلك انبعاثات أكاسيد النيتروجين oxides of nitrogen (NOx) ، ديناميكيات الاحتراق combustion dynamics واصطدام الماء أسفل الفوهة . شكل 3.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/856,973 US20170082024A1 (en) | 2015-09-17 | 2015-09-17 | Independently controlled three stage water injection in a diffusion burner |
PCT/US2016/047685 WO2017048455A1 (en) | 2015-09-17 | 2016-08-19 | Independently controlled three stage water injection in a diffusion burner |
Publications (1)
Publication Number | Publication Date |
---|---|
SA518391117B1 true SA518391117B1 (ar) | 2022-04-13 |
Family
ID=58276866
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SA518391117A SA518391117B1 (ar) | 2015-09-17 | 2018-03-14 | حقن ماء على ثلاث مراحل يتم التحكم فيه بشكل مستقل في حارق انتشار |
Country Status (4)
Country | Link |
---|---|
US (2) | US20170082024A1 (ar) |
JP (1) | JP6615328B2 (ar) |
SA (1) | SA518391117B1 (ar) |
WO (1) | WO2017048455A1 (ar) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3121179B1 (fr) * | 2021-03-24 | 2023-02-17 | Airbus Helicopters | véhicule muni d’une installation motrice comprenant au moins un moteur thermique coopérant avec un système de conditionnement d’air |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4110973A (en) * | 1977-01-24 | 1978-09-05 | Energy Services Inc. | Water injection system for industrial gas turbine engine |
US4580910A (en) * | 1985-01-24 | 1986-04-08 | National Flight Services, Inc. | Engine exhaust gas test harness |
US5228283A (en) * | 1990-05-01 | 1993-07-20 | General Electric Company | Method of reducing nox emissions in a gas turbine engine |
US5175994A (en) * | 1991-05-03 | 1993-01-05 | United Technologies Corporation | Combustion section supply system having fuel and water injection for a rotary machine |
US6595003B2 (en) * | 2000-08-31 | 2003-07-22 | Ralph A. Dalla Betta | Process and apparatus for control of NOx in catalytic combustion systems |
US6938425B2 (en) * | 2003-08-11 | 2005-09-06 | Siemens Westinghouse Power Corporation | System and method for controlling water injection in a turbine engine |
US9927818B2 (en) * | 2010-05-24 | 2018-03-27 | Ansaldo Energia Ip Uk Limited | Stabilizing a gas turbine engine via incremental tuning during transients |
US20110314831A1 (en) * | 2010-06-23 | 2011-12-29 | Abou-Jaoude Khalil F | Secondary water injection for diffusion combustion systems |
US9243804B2 (en) * | 2011-10-24 | 2016-01-26 | General Electric Company | System for turbine combustor fuel mixing |
US9422869B2 (en) * | 2013-03-13 | 2016-08-23 | General Electric Company | Systems and methods for gas turbine tuning and control |
CN106574774A (zh) * | 2014-08-14 | 2017-04-19 | 西门子公司 | 具有雾化器阵列的多功能燃料喷嘴 |
US9784183B2 (en) * | 2014-11-18 | 2017-10-10 | General Electric Company | Power outlet, emissions, fuel flow and water flow based probabilistic control in liquid-fueled gas turbine tuning, related control systems, computer program products and methods |
-
2015
- 2015-09-17 US US14/856,973 patent/US20170082024A1/en not_active Abandoned
-
2016
- 2016-08-19 JP JP2018514358A patent/JP6615328B2/ja active Active
- 2016-08-19 WO PCT/US2016/047685 patent/WO2017048455A1/en active Application Filing
-
2018
- 2018-03-14 SA SA518391117A patent/SA518391117B1/ar unknown
-
2019
- 2019-09-06 US US16/563,186 patent/US20200018232A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US20200018232A1 (en) | 2020-01-16 |
WO2017048455A1 (en) | 2017-03-23 |
JP2018527514A (ja) | 2018-09-20 |
US20170082024A1 (en) | 2017-03-23 |
JP6615328B2 (ja) | 2019-12-04 |
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