GB1303962A - - Google Patents
Info
- Publication number
- GB1303962A GB1303962A GB1970171*[A GB1970171A GB1303962A GB 1303962 A GB1303962 A GB 1303962A GB 1970171 A GB1970171 A GB 1970171A GB 1303962 A GB1303962 A GB 1303962A
- Authority
- GB
- United Kingdom
- Prior art keywords
- openings
- end wall
- array
- smaller
- diameter
- 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
Links
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 2
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 238000011144 upstream manufacturing Methods 0.000 abstract 1
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
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US5582170A | 1970-07-17 | 1970-07-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1303962A true GB1303962A (enrdf_load_stackoverflow) | 1973-01-24 |
Family
ID=22000363
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1970171*[A Expired GB1303962A (enrdf_load_stackoverflow) | 1970-07-17 | 1971-06-09 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3657883A (enrdf_load_stackoverflow) |
| JP (1) | JPS5023450B1 (enrdf_load_stackoverflow) |
| CA (1) | CA918937A (enrdf_load_stackoverflow) |
| CH (1) | CH541716A (enrdf_load_stackoverflow) |
| DE (1) | DE2133256A1 (enrdf_load_stackoverflow) |
| FR (1) | FR2099438B1 (enrdf_load_stackoverflow) |
| GB (1) | GB1303962A (enrdf_load_stackoverflow) |
| NL (1) | NL7109893A (enrdf_load_stackoverflow) |
Families Citing this family (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3742704A (en) * | 1971-07-13 | 1973-07-03 | Westinghouse Electric Corp | Combustion chamber support structure |
| US4720970A (en) * | 1982-11-05 | 1988-01-26 | The United States Of America As Represented By The Secretary Of The Air Force | Sector airflow variable geometry combustor |
| JPS61195214A (ja) * | 1985-02-22 | 1986-08-29 | Hitachi Ltd | ガスタ−ビン燃焼器の空気流量調整機構 |
| US5233822A (en) * | 1991-01-31 | 1993-08-10 | General Electric Company | Method and system for the disassembly of an annular combustor |
| US5983641A (en) * | 1997-04-30 | 1999-11-16 | Mitsubishi Heavy Industries, Ltd. | Tail pipe of gas turbine combustor and gas turbine combustor having the same tail pipe |
| US6691519B2 (en) * | 2000-02-18 | 2004-02-17 | Siemens Westinghouse Power Corporation | Adaptable modular gas turbine power plant |
| US6672073B2 (en) | 2002-05-22 | 2004-01-06 | Siemens Westinghouse Power Corporation | System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate |
| US7200987B2 (en) * | 2004-06-18 | 2007-04-10 | General Electric Company | Off-axis pulse detonation configuration for gas turbine engine |
| US7509807B2 (en) * | 2004-08-13 | 2009-03-31 | Siemens Energy, Inc. | Concentric catalytic combustor |
| US8109098B2 (en) * | 2006-05-04 | 2012-02-07 | Siemens Energy, Inc. | Combustor liner for gas turbine engine |
| EP2119966A1 (en) * | 2008-05-15 | 2009-11-18 | ALSTOM Technology Ltd | Combustor with reduced carbon monoxide emissions |
| US7874138B2 (en) * | 2008-09-11 | 2011-01-25 | Siemens Energy, Inc. | Segmented annular combustor |
| US8938976B2 (en) * | 2011-05-20 | 2015-01-27 | Siemens Energy, Inc. | Structural frame for gas turbine combustion cap assembly |
| US20140083111A1 (en) * | 2012-09-25 | 2014-03-27 | United Technologies Corporation | Gas turbine asymmetric fuel nozzle combustor |
| US9546601B2 (en) * | 2012-11-20 | 2017-01-17 | General Electric Company | Clocked combustor can array |
| EP3015770B1 (en) * | 2014-11-03 | 2020-07-01 | Ansaldo Energia Switzerland AG | Can combustion chamber |
| JP6625427B2 (ja) * | 2015-12-25 | 2019-12-25 | 川崎重工業株式会社 | ガスタービンエンジン |
| US10584880B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Mounting of integrated combustor nozzles in a segmented annular combustion system |
| US10641491B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Cooling of integrated combustor nozzle of segmented annular combustion system |
| US10605459B2 (en) | 2016-03-25 | 2020-03-31 | General Electric Company | Integrated combustor nozzle for a segmented annular combustion system |
| US10830442B2 (en) | 2016-03-25 | 2020-11-10 | General Electric Company | Segmented annular combustion system with dual fuel capability |
| US10724441B2 (en) | 2016-03-25 | 2020-07-28 | General Electric Company | Segmented annular combustion system |
| US10563869B2 (en) | 2016-03-25 | 2020-02-18 | General Electric Company | Operation and turndown of a segmented annular combustion system |
| US10520194B2 (en) | 2016-03-25 | 2019-12-31 | General Electric Company | Radially stacked fuel injection module for a segmented annular combustion system |
| US10584876B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system |
| US11428413B2 (en) | 2016-03-25 | 2022-08-30 | General Electric Company | Fuel injection module for segmented annular combustion system |
| US11156362B2 (en) | 2016-11-28 | 2021-10-26 | General Electric Company | Combustor with axially staged fuel injection |
| US10690350B2 (en) | 2016-11-28 | 2020-06-23 | General Electric Company | Combustor with axially staged fuel injection |
| US11015812B2 (en) * | 2018-05-07 | 2021-05-25 | Rolls-Royce North American Technologies Inc. | Combustor bolted segmented architecture |
| RU2710642C1 (ru) * | 2018-11-15 | 2019-12-30 | Публичное Акционерное Общество "Одк-Сатурн" | Трубчатая камера сгорания газотурбинного двигателя |
| US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
| US11994292B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus for turbomachine |
| US11614233B2 (en) | 2020-08-31 | 2023-03-28 | General Electric Company | Impingement panel support structure and method of manufacture |
| US11371702B2 (en) | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
| US11994293B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus support structure and method of manufacture |
| US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
| US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE806613C (de) * | 1947-02-24 | 1951-06-14 | Cem Comp Electro Mec | Anordnung der Verbrennungskammern von Gasturbinen |
| US2674090A (en) * | 1950-03-21 | 1954-04-06 | United Aircraft Corp | Combustion chamber for gas turbines |
| DE1117348B (de) * | 1954-02-27 | 1961-11-16 | United Aircraft Corp | Gasturbinentriebwerk |
| US3044263A (en) * | 1959-05-21 | 1962-07-17 | Dresser Ind | Combustor with unitary liner |
| US3169367A (en) * | 1963-07-18 | 1965-02-16 | Westinghouse Electric Corp | Combustion apparatus |
-
1970
- 1970-07-17 US US55821A patent/US3657883A/en not_active Expired - Lifetime
-
1971
- 1971-05-27 CA CA114013A patent/CA918937A/en not_active Expired
- 1971-06-09 GB GB1970171*[A patent/GB1303962A/en not_active Expired
- 1971-07-05 DE DE19712133256 patent/DE2133256A1/de active Pending
- 1971-07-06 JP JP46049304A patent/JPS5023450B1/ja active Pending
- 1971-07-15 CH CH1043171A patent/CH541716A/de not_active IP Right Cessation
- 1971-07-16 NL NL7109893A patent/NL7109893A/xx unknown
- 1971-07-16 FR FR7126202A patent/FR2099438B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| CA918937A (en) | 1973-01-16 |
| NL7109893A (enrdf_load_stackoverflow) | 1972-01-19 |
| FR2099438B1 (enrdf_load_stackoverflow) | 1975-07-11 |
| JPS5023450B1 (enrdf_load_stackoverflow) | 1975-08-07 |
| DE2133256A1 (de) | 1972-01-20 |
| US3657883A (en) | 1972-04-25 |
| CH541716A (de) | 1973-09-15 |
| FR2099438A1 (enrdf_load_stackoverflow) | 1972-03-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |