GB591113A - Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus - Google Patents
Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatusInfo
- Publication number
- GB591113A GB591113A GB1354/45A GB135445A GB591113A GB 591113 A GB591113 A GB 591113A GB 1354/45 A GB1354/45 A GB 1354/45A GB 135445 A GB135445 A GB 135445A GB 591113 A GB591113 A GB 591113A
- Authority
- GB
- United Kingdom
- Prior art keywords
- burner
- fuel
- flame chamber
- inlet connection
- divides
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/062—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with aft fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Gas Burners (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
591,113. Generating combustion products under pressure. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and FEILDEN, G.B.R. Jan. 16, 1945, No. 1354. [Class 51 (i)] [Also in Groups XI and XXVI] A combustion apparatus, particularly for a gas turbine plant, in which the fuel is injected in a downstream direction into a flame chamber enclosed within an air duct, has the fuel injector burner, which supports the upstream end of the flame chamber detachably mounted on a structural member of the air duct which lies in and divides the air stream and through which pass the fuel supply connections to the burner. The flame chamber is attached to the burner by releasable locking means which allows its easy withdrawal in the axial direction. A burner 5 is mounted on the downstream edge of a structural member 7 of aerofoil form in cross-section which lies in and divides the airstream so as to be removable therefrom without disturbing the fuel supply connections. The burner, which is of the. spill controlled type, receives fuel from an inlet connection 10 through axial passages 11 each of which is fitted with a tubular liner 12. The liners 12 project from each end of the member 7 and are fitted with sealing rings 14 and 16 so as to make a fluid tight joint when the bolts attaching the inlet connection 10 and the burner 5 to the member 7 are tightened up. The burner 5 supports the upstream end of the flame chamber 4 by means of a screwed sleeve 24 engaged by a locking sleeve 25. The burner nozzle 20 is formed in a separate end plate held in position on the burner by a screwed sleeve 22. The radial passage 8 not only accommodates the fuel inlet connection but also forms a passage for cooling air for the bearings and shaft. A modification using a single duct burner is also described.
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL70888D NL70888C (en) | 1945-01-16 | ||
BE462369D BE462369A (en) | 1945-01-16 | ||
GB1354/45A GB591113A (en) | 1945-01-16 | 1945-01-16 | Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus |
CH261477D CH261477A (en) | 1945-01-16 | 1946-01-10 | Incinerator. |
FR920036D FR920036A (en) | 1945-01-16 | 1946-01-14 | Improvements to gas turbine engines or the like include a combustion apparatus |
FR920038D FR920038A (en) | 1945-01-16 | 1946-01-14 | Improvements to fuel burner vehicles, in particular turbo-propellants or similar |
US641145A US2575264A (en) | 1945-01-16 | 1946-01-14 | Construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1354/45A GB591113A (en) | 1945-01-16 | 1945-01-16 | Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
GB591113A true GB591113A (en) | 1947-08-07 |
Family
ID=29725418
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1354/45A Expired GB591113A (en) | 1945-01-16 | 1945-01-16 | Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus |
Country Status (6)
Country | Link |
---|---|
US (1) | US2575264A (en) |
BE (1) | BE462369A (en) |
CH (1) | CH261477A (en) |
FR (2) | FR920038A (en) |
GB (1) | GB591113A (en) |
NL (1) | NL70888C (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2675675A (en) * | 1954-04-20 | Muctlpefi combustion chamber jet | ||
US2670600A (en) * | 1947-06-17 | 1954-03-02 | Bristol Aeroplane Co Ltd | Air distribution system for flame tubes of gas turbine engines |
US2697032A (en) * | 1949-05-05 | 1954-12-14 | Phillips Petroleum Co | Acetylene gas producer |
US2711631A (en) * | 1949-06-21 | 1955-06-28 | Hartford Nat Bank & Trust Co | Gas turbine power plant |
US2692478A (en) * | 1951-02-24 | 1954-10-26 | Boeing Co | Turbine burner incorporating removable burner liner |
US2690648A (en) * | 1951-07-03 | 1954-10-05 | Dowty Equipment Ltd | Means for conducting the flow of liquid fuel for feeding burners of gas turbine engines |
US3062482A (en) * | 1952-08-25 | 1962-11-06 | A V Roe Canada Ltd | Gas turbine engined aircraft |
FR998079A (en) * | 1958-08-22 | 1952-01-14 | Snecma | Device for the entry of air into the primary zone of a turbo-machine combustion chamber |
US3741483A (en) * | 1971-12-10 | 1973-06-26 | Mitsubishi Heavy Ind Ltd | Combustion air supply arrangement for gas turbines |
US5630319A (en) * | 1995-05-12 | 1997-05-20 | General Electric Company | Dome assembly for a multiple annular combustor |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2439273A (en) * | 1948-04-06 | Turbo-jet engine for aircraft | ||
US2432359A (en) * | 1947-12-09 | Internal-combustion turbine power | ||
US1517422A (en) * | 1922-08-05 | 1924-12-02 | Leo G Hall | Combination land and water vehicle |
US1466006A (en) * | 1922-09-14 | 1923-08-28 | Trood Samuel | Apparatus for producing and utilizing combustible mixture |
US1950046A (en) * | 1933-05-12 | 1934-03-06 | Surface Combustion Corp | Gas burner |
US1995417A (en) * | 1933-05-12 | 1935-03-26 | Surface Combustion Corp | Gas burner |
US2072731A (en) * | 1934-12-03 | 1937-03-02 | Steam Motors Inc | Oil burner |
US2224472A (en) * | 1938-05-02 | 1940-12-10 | Chandler Evans Corp | Pressure fed carburetor |
US2360130A (en) * | 1941-03-26 | 1944-10-10 | Armstrong Siddeley Motors Ltd | High-speed propulsion plant |
US2422214A (en) * | 1944-08-17 | 1947-06-17 | Westinghouse Electric Corp | Fuel injector mounting for combustion chambers |
-
0
- BE BE462369D patent/BE462369A/xx unknown
- NL NL70888D patent/NL70888C/xx active
-
1945
- 1945-01-16 GB GB1354/45A patent/GB591113A/en not_active Expired
-
1946
- 1946-01-10 CH CH261477D patent/CH261477A/en unknown
- 1946-01-14 FR FR920038D patent/FR920038A/en not_active Expired
- 1946-01-14 US US641145A patent/US2575264A/en not_active Expired - Lifetime
- 1946-01-14 FR FR920036D patent/FR920036A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
BE462369A (en) | |
FR920036A (en) | 1947-03-25 |
NL70888C (en) | |
CH261477A (en) | 1949-05-15 |
FR920038A (en) | 1947-03-25 |
US2575264A (en) | 1951-11-13 |
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