GB0210014D0 - Fuel delivery system - Google Patents
Fuel delivery systemInfo
- Publication number
- GB0210014D0 GB0210014D0 GB0210014A GB0210014A GB0210014D0 GB 0210014 D0 GB0210014 D0 GB 0210014D0 GB 0210014 A GB0210014 A GB 0210014A GB 0210014 A GB0210014 A GB 0210014A GB 0210014 D0 GB0210014 D0 GB 0210014D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- delivery system
- fuel delivery
- fuel
- delivery
- 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.)
- Granted
Links
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02254367A EP1278014B1 (en) | 2001-07-18 | 2002-06-24 | Fuel delivery system |
DE60217768T DE60217768T2 (en) | 2001-07-18 | 2002-06-24 | Fuel delivery device |
US10/183,391 US6857272B2 (en) | 2001-07-18 | 2002-06-28 | Fuel delivery system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0117554A GB0117554D0 (en) | 2001-07-18 | 2001-07-18 | Fluid delivery system |
GB0209295A GB0209295D0 (en) | 2002-04-24 | 2002-04-24 | Fuel delivery system |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0210014D0 true GB0210014D0 (en) | 2002-06-12 |
GB2378224A GB2378224A (en) | 2003-02-05 |
GB2378224B GB2378224B (en) | 2005-10-12 |
Family
ID=26246324
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0210014A Expired - Fee Related GB2378224B (en) | 2001-07-18 | 2002-05-02 | Gas turbine engine fuel delivery system |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2378224B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115030824A (en) * | 2022-08-11 | 2022-09-09 | 成都凯天电子股份有限公司 | Self-adaptive oil supply system and method under full flight profile of helicopter |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011036205A1 (en) * | 2009-09-24 | 2011-03-31 | Siemens Aktiengesellschaft | Fuel line system, method for operating a gas turbine, and method for purging the fuel line system of a gas turbine |
GB201604379D0 (en) | 2016-03-15 | 2016-04-27 | Rolls Royce Plc | A combustion chamber system and a method of operating a combustion chamber system |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB654122A (en) * | 1948-06-11 | 1951-06-06 | Rolls Royce | Improvements in or relating to combustion equipment for gas-turbine engines |
US4417439A (en) * | 1981-07-29 | 1983-11-29 | United Technologies Corporation | Starting means for a gas turbine engine |
US4817389A (en) * | 1987-09-24 | 1989-04-04 | United Technologies Corporation | Fuel injection system |
GB2320063B (en) * | 1993-12-09 | 1998-07-15 | United Technologies Corp | Fuel staging system |
DE4429539C2 (en) * | 1994-08-19 | 2002-10-24 | Alstom | Process for speed control of a gas turbine when shedding loads |
GB2312250A (en) * | 1996-04-18 | 1997-10-22 | Rolls Royce Plc | Staged gas turbine fuel system with a single supply manifold, to which the main burners are connected through valves. |
US6405524B1 (en) * | 2000-08-16 | 2002-06-18 | General Electric Company | Apparatus for decreasing gas turbine combustor emissions |
-
2002
- 2002-05-02 GB GB0210014A patent/GB2378224B/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115030824A (en) * | 2022-08-11 | 2022-09-09 | 成都凯天电子股份有限公司 | Self-adaptive oil supply system and method under full flight profile of helicopter |
CN115030824B (en) * | 2022-08-11 | 2022-11-22 | 成都凯天电子股份有限公司 | Self-adaptive oil supply system and method under full flight profile of helicopter |
Also Published As
Publication number | Publication date |
---|---|
GB2378224A (en) | 2003-02-05 |
GB2378224B (en) | 2005-10-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20200502 |