GB2453114B - A Swirler for use in a burner of a gas turbine engine - Google Patents
A Swirler for use in a burner of a gas turbine engineInfo
- Publication number
- GB2453114B GB2453114B GB0718672A GB0718672A GB2453114B GB 2453114 B GB2453114 B GB 2453114B GB 0718672 A GB0718672 A GB 0718672A GB 0718672 A GB0718672 A GB 0718672A GB 2453114 B GB2453114 B GB 2453114B
- Authority
- GB
- United Kingdom
- Prior art keywords
- swirler
- burner
- gas turbine
- turbine engine
- engine
- 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
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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
-
- 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
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/07001—Air swirling vanes incorporating fuel injectors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0718672A GB2453114B (en) | 2007-09-25 | 2007-09-25 | A Swirler for use in a burner of a gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0718672A GB2453114B (en) | 2007-09-25 | 2007-09-25 | A Swirler for use in a burner of a gas turbine engine |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0718672D0 GB0718672D0 (en) | 2007-10-31 |
GB2453114A GB2453114A (en) | 2009-04-01 |
GB2453114B true GB2453114B (en) | 2009-08-26 |
Family
ID=38670452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0718672A Expired - Fee Related GB2453114B (en) | 2007-09-25 | 2007-09-25 | A Swirler for use in a burner of a gas turbine engine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2453114B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2246617B1 (en) * | 2009-04-29 | 2017-04-19 | Siemens Aktiengesellschaft | A burner for a gas turbine engine |
WO2015121063A1 (en) * | 2014-02-11 | 2015-08-20 | Siemens Aktiengesellschaft | Swirler for a burner of a gas turbine engine |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5319935A (en) * | 1990-10-23 | 1994-06-14 | Rolls-Royce Plc | Staged gas turbine combustion chamber with counter swirling arrays of radial vanes having interjacent fuel injection |
US5794449A (en) * | 1995-06-05 | 1998-08-18 | Allison Engine Company, Inc. | Dry low emission combustor for gas turbine engines |
EP1795807A2 (en) * | 2005-12-08 | 2007-06-13 | General Electric Company | Swirler assembly |
-
2007
- 2007-09-25 GB GB0718672A patent/GB2453114B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5319935A (en) * | 1990-10-23 | 1994-06-14 | Rolls-Royce Plc | Staged gas turbine combustion chamber with counter swirling arrays of radial vanes having interjacent fuel injection |
US5794449A (en) * | 1995-06-05 | 1998-08-18 | Allison Engine Company, Inc. | Dry low emission combustor for gas turbine engines |
EP1795807A2 (en) * | 2005-12-08 | 2007-06-13 | General Electric Company | Swirler assembly |
Also Published As
Publication number | Publication date |
---|---|
GB2453114A (en) | 2009-04-01 |
GB0718672D0 (en) | 2007-10-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20110925 |