GB1127637A - Supports for fuel burners - Google Patents
Supports for fuel burnersInfo
- Publication number
- GB1127637A GB1127637A GB37035/66A GB3703566A GB1127637A GB 1127637 A GB1127637 A GB 1127637A GB 37035/66 A GB37035/66 A GB 37035/66A GB 3703566 A GB3703566 A GB 3703566A GB 1127637 A GB1127637 A GB 1127637A
- Authority
- GB
- United Kingdom
- Prior art keywords
- burner
- lengthwise
- aug
- supports
- swirler
- 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
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- 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)
- Spray-Type Burners (AREA)
- Superconductor Devices And Manufacturing Methods Thereof (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
1,127,637. Mounting burners. JOSEPH LUCAS (INDUSTRIES) Ltd. 14 Aug., 1967 [18 Aug., 1966], No. 37035/66. Heading F4T. A burner, of a gas turbine engine, having an air swirler 8, liquid fuel supply pipe 10, and inner and outer concentric parts 11, 12 between which gaseous fuel can be supplied is supported at two spaced positions lengthwise thereof by part-spherical bearings 24, 25 which permit lengthwise movement of the front part of the burner through the swirler 8 to accommodate lengthwise expansion of the burner.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB37035/66A GB1127637A (en) | 1966-08-18 | 1966-08-18 | Supports for fuel burners |
DE19671601598 DE1601598A1 (en) | 1966-08-18 | 1967-08-16 | Storage of a burner for gas turbines |
US661268A US3458997A (en) | 1966-08-18 | 1967-08-17 | Supports for fuel burners |
NL6711357A NL6711357A (en) | 1966-08-18 | 1967-08-17 | |
FR118197A FR1535882A (en) | 1966-08-18 | 1967-08-18 | Fuel burner, especially for gas turbine engine |
BE702833D BE702833A (en) | 1966-08-18 | 1967-08-18 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB37035/66A GB1127637A (en) | 1966-08-18 | 1966-08-18 | Supports for fuel burners |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1127637A true GB1127637A (en) | 1968-09-18 |
Family
ID=10393213
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB37035/66A Expired GB1127637A (en) | 1966-08-18 | 1966-08-18 | Supports for fuel burners |
Country Status (5)
Country | Link |
---|---|
US (1) | US3458997A (en) |
BE (1) | BE702833A (en) |
DE (1) | DE1601598A1 (en) |
GB (1) | GB1127637A (en) |
NL (1) | NL6711357A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0078630A2 (en) * | 1981-10-29 | 1983-05-11 | Avco Corporation | Fuel nozzle assembly for a gas turbine engine |
EP0376442A1 (en) * | 1988-12-27 | 1990-07-04 | General Electric Company | Gas turbine igniter with balljoint support |
EP0687865A1 (en) * | 1994-06-13 | 1995-12-20 | Westinghouse Electric Corporation | Low NOx combustor retro-fit system for gas turbines |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3854285A (en) * | 1973-02-26 | 1974-12-17 | Gen Electric | Combustor dome assembly |
US3879940A (en) * | 1973-07-30 | 1975-04-29 | Gen Electric | Gas turbine engine fuel delivery tube assembly |
US4082499A (en) * | 1976-11-12 | 1978-04-04 | Allis-Chalmers Corporation | Multipurpose kiln shell gas burner |
DE2710618C2 (en) * | 1977-03-11 | 1982-11-11 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Fuel injector for gas turbine engines |
US4258544A (en) * | 1978-09-15 | 1981-03-31 | Caterpillar Tractor Co. | Dual fluid fuel nozzle |
IT1133435B (en) * | 1980-06-06 | 1986-07-09 | Italimpianti | Vaulting radiant burner |
US5240409A (en) * | 1992-04-10 | 1993-08-31 | Institute Of Gas Technology | Premixed fuel/air burners |
US7356994B2 (en) * | 2004-04-09 | 2008-04-15 | Delavan Inc | Alignment and positioning system for installing a fuel injector in a gas turbine engine |
US7628019B2 (en) * | 2005-03-21 | 2009-12-08 | United Technologies Corporation | Fuel injector bearing plate assembly and swirler assembly |
US8166763B2 (en) * | 2006-09-14 | 2012-05-01 | Solar Turbines Inc. | Gas turbine fuel injector with a removable pilot assembly |
US8286433B2 (en) | 2007-10-26 | 2012-10-16 | Solar Turbines Inc. | Gas turbine fuel injector with removable pilot liquid tube |
US8661823B2 (en) * | 2010-01-05 | 2014-03-04 | General Electric Company | Integral flange connection fuel nozzle body for gas turbine |
GB2543803B (en) * | 2015-10-29 | 2019-10-30 | Rolls Royce Plc | A combustion chamber assembly |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2675864A (en) * | 1950-03-15 | 1954-04-20 | Jay J Seaver | Burner for open-hearth furnaces |
US2907527A (en) * | 1956-04-10 | 1959-10-06 | Thompson Ramo Wooldridge Inc | Nozzle |
US2965303A (en) * | 1959-03-30 | 1960-12-20 | United Aircraft Corp | Coolant injection in a fuel nozzle |
US3159971A (en) * | 1961-02-24 | 1964-12-08 | Parker Hannifin Corp | Resilient nozzle mount |
US3320744A (en) * | 1965-11-15 | 1967-05-23 | Sonic Dev Corp | Gas turbine engine burner |
-
1966
- 1966-08-18 GB GB37035/66A patent/GB1127637A/en not_active Expired
-
1967
- 1967-08-16 DE DE19671601598 patent/DE1601598A1/en active Pending
- 1967-08-17 US US661268A patent/US3458997A/en not_active Expired - Lifetime
- 1967-08-17 NL NL6711357A patent/NL6711357A/xx unknown
- 1967-08-18 BE BE702833D patent/BE702833A/xx unknown
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0078630A2 (en) * | 1981-10-29 | 1983-05-11 | Avco Corporation | Fuel nozzle assembly for a gas turbine engine |
EP0078630A3 (en) * | 1981-10-29 | 1983-08-10 | Avco Corporation | Fuel nozzle assembly for a gas turbine engine |
EP0376442A1 (en) * | 1988-12-27 | 1990-07-04 | General Electric Company | Gas turbine igniter with balljoint support |
EP0687865A1 (en) * | 1994-06-13 | 1995-12-20 | Westinghouse Electric Corporation | Low NOx combustor retro-fit system for gas turbines |
Also Published As
Publication number | Publication date |
---|---|
BE702833A (en) | 1968-01-15 |
NL6711357A (en) | 1968-02-19 |
US3458997A (en) | 1969-08-05 |
DE1601598A1 (en) | 1970-08-27 |
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