GB1284440A - Improvements in or relating to gas turbine engines - Google Patents
Improvements in or relating to gas turbine enginesInfo
- Publication number
- GB1284440A GB1284440A GB60035/69A GB6003569A GB1284440A GB 1284440 A GB1284440 A GB 1284440A GB 60035/69 A GB60035/69 A GB 60035/69A GB 6003569 A GB6003569 A GB 6003569A GB 1284440 A GB1284440 A GB 1284440A
- Authority
- GB
- United Kingdom
- Prior art keywords
- relating
- gas turbine
- turbine engines
- heading
- dec
- 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
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
- F23R3/36—Supply of different fuels
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Air Supply (AREA)
Abstract
1284440 Spray burners ROLLS ROYCE Ltd 9 Dec 1969 60035/69 Heading F4T The subject matter is substantially identical with that of Specification 1284439 but the claims are directed to the fact that one nozzle can be connected selectively to a fuel or air supply.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB60035/69A GB1284440A (en) | 1969-12-09 | 1969-12-09 | Improvements in or relating to gas turbine engines |
US95124A US3690093A (en) | 1969-12-09 | 1970-12-04 | Fuel injector for a gas turbine engine |
DE2060158A DE2060158C3 (en) | 1969-12-09 | 1970-12-07 | Fuel injector for a gas turbine jet engine |
FR7044353A FR2073176A5 (en) | 1969-12-09 | 1970-12-09 | FUEL INJECTOR GAS TURBINE ENGINE COMBUSTION EQUIPMENT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB60035/69A GB1284440A (en) | 1969-12-09 | 1969-12-09 | Improvements in or relating to gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1284440A true GB1284440A (en) | 1972-08-09 |
Family
ID=10484880
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB60035/69A Expired GB1284440A (en) | 1969-12-09 | 1969-12-09 | Improvements in or relating to gas turbine engines |
Country Status (4)
Country | Link |
---|---|
US (1) | US3690093A (en) |
DE (1) | DE2060158C3 (en) |
FR (1) | FR2073176A5 (en) |
GB (1) | GB1284440A (en) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1377184A (en) * | 1971-02-02 | 1974-12-11 | Secr Defence | Gas turbine engine combustion apparatus |
US3768250A (en) * | 1971-12-01 | 1973-10-30 | Mitsubishi Heavy Ind Ltd | Combustion apparatus for a gas turbine |
US4327547A (en) * | 1978-11-23 | 1982-05-04 | Rolls-Royce Limited | Fuel injectors |
GB2050592B (en) * | 1979-06-06 | 1983-03-16 | Rolls Royce | Gas turbine |
GB2055187B (en) * | 1979-08-01 | 1983-12-14 | Rolls Royce | Gaseous fuel injector for a gas turbine engine |
GB2055186B (en) * | 1979-08-01 | 1983-05-25 | Rolls Royce | Gas turbine engine dual fuel injector |
US4344280A (en) * | 1980-01-24 | 1982-08-17 | Hitachi, Ltd. | Combustor of gas turbine |
JPS5741524A (en) * | 1980-08-25 | 1982-03-08 | Hitachi Ltd | Combustion method of gas turbine and combustor for gas turbine |
US4735044A (en) * | 1980-11-25 | 1988-04-05 | General Electric Company | Dual fuel path stem for a gas turbine engine |
DE3405400A1 (en) * | 1984-01-26 | 1985-08-01 | József 8000 München Previcz | Mixture-forming valve for the introduction of a fuel-air mixture into the intake line of a combustion system |
US5564271A (en) * | 1994-06-24 | 1996-10-15 | United Technologies Corporation | Pressure vessel fuel nozzle support for an industrial gas turbine engine |
US8499739B2 (en) * | 2006-08-31 | 2013-08-06 | Caterpillar Inc. | Injector having tangentially oriented purge line |
US8215100B2 (en) * | 2007-03-02 | 2012-07-10 | Caterpillar Inc. | Regeneration device having external check valve |
US20100095649A1 (en) * | 2008-10-20 | 2010-04-22 | General Electric Company | Staged combustion systems and methods |
US10012387B2 (en) * | 2014-12-05 | 2018-07-03 | General Electric Company | Fuel supply system for a gas turbine engine |
US9791153B2 (en) * | 2015-02-27 | 2017-10-17 | United Technologies Corporation | Line replaceable fuel nozzle apparatus, system and method |
US11692488B2 (en) | 2020-11-04 | 2023-07-04 | Delavan Inc. | Torch igniter cooling system |
US11473505B2 (en) | 2020-11-04 | 2022-10-18 | Delavan Inc. | Torch igniter cooling system |
US11608783B2 (en) | 2020-11-04 | 2023-03-21 | Delavan, Inc. | Surface igniter cooling system |
US11635027B2 (en) * | 2020-11-18 | 2023-04-25 | Collins Engine Nozzles, Inc. | Fuel systems for torch ignition devices |
US11421602B2 (en) | 2020-12-16 | 2022-08-23 | Delavan Inc. | Continuous ignition device exhaust manifold |
US11635210B2 (en) | 2020-12-17 | 2023-04-25 | Collins Engine Nozzles, Inc. | Conformal and flexible woven heat shields for gas turbine engine components |
US11486309B2 (en) | 2020-12-17 | 2022-11-01 | Delavan Inc. | Axially oriented internally mounted continuous ignition device: removable hot surface igniter |
US11754289B2 (en) | 2020-12-17 | 2023-09-12 | Delavan, Inc. | Axially oriented internally mounted continuous ignition device: removable nozzle |
US12092333B2 (en) | 2020-12-17 | 2024-09-17 | Collins Engine Nozzles, Inc. | Radially oriented internally mounted continuous ignition device |
US11680528B2 (en) | 2020-12-18 | 2023-06-20 | Delavan Inc. | Internally-mounted torch igniters with removable igniter heads |
US11209164B1 (en) | 2020-12-18 | 2021-12-28 | Delavan Inc. | Fuel injector systems for torch igniters |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1877942A (en) * | 1930-05-16 | 1932-09-20 | Albert W Morse | Combination gas and oil burner |
US2595759A (en) * | 1948-11-30 | 1952-05-06 | Gen Electric | Atomizing nozzle for spraying viscous liquids |
US2635425A (en) * | 1949-09-07 | 1953-04-21 | Westinghouse Electric Corp | Dual flow fuel nozzle system having means to inject air in response to low fuel pressure |
US2907527A (en) * | 1956-04-10 | 1959-10-06 | Thompson Ramo Wooldridge Inc | Nozzle |
GB985739A (en) * | 1963-11-11 | 1965-03-10 | Rolls Royce | Fuel injector for a gas turbine engine |
-
1969
- 1969-12-09 GB GB60035/69A patent/GB1284440A/en not_active Expired
-
1970
- 1970-12-04 US US95124A patent/US3690093A/en not_active Expired - Lifetime
- 1970-12-07 DE DE2060158A patent/DE2060158C3/en not_active Expired
- 1970-12-09 FR FR7044353A patent/FR2073176A5/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2060158B2 (en) | 1980-10-16 |
DE2060158A1 (en) | 1972-06-08 |
DE2060158C3 (en) | 1981-07-23 |
US3690093A (en) | 1972-09-12 |
FR2073176A5 (en) | 1971-09-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLE | Entries relating assignments, transmissions, licences in the register of patents | ||
PCNP | Patent ceased through non-payment of renewal fee |