GB870988A - Improvements in or relating to a liquid fuel atomiser - Google Patents
Improvements in or relating to a liquid fuel atomiserInfo
- Publication number
- GB870988A GB870988A GB27263/57A GB2726357A GB870988A GB 870988 A GB870988 A GB 870988A GB 27263/57 A GB27263/57 A GB 27263/57A GB 2726357 A GB2726357 A GB 2726357A GB 870988 A GB870988 A GB 870988A
- Authority
- GB
- United Kingdom
- Prior art keywords
- passes
- atomizer
- fuel
- combustion chamber
- air
- 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
- 239000000446 fuel Substances 0.000 title abstract 7
- 239000007788 liquid Substances 0.000 title abstract 2
- 238000002485 combustion reaction Methods 0.000 abstract 8
- 238000007865 diluting Methods 0.000 abstract 1
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
- F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/236—Fuel delivery systems comprising two or more pumps
- F02C7/2365—Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/04—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying action being obtained by centrifugal action
-
- 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
- F23R3/005—Combined with pressure or heat exchangers
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
870,988. Rotary fuel burners. SOMMARIVA, G. B. Aug. 29, 1957 [Sept. 1, 1956], No. 27263/57. Class 75(1). [Also in 'Groups XII and XXVI] A liquid fuel burner comprises a rotary fuel atomizer 2 having radial fuel discharge ducts 45 and driven by primary air directed by stator blades 4 on to blades 43 on the atomizer. The atomizer is mounted on the end of a rotary hollow shaft 32 through which passes a stationary fuel pipe 26 having an outlet controlled by a needle valve 29. The fuel passes through apertures in the rotary shaft to an annular chamber Ch in the atomizer and thence through the ducts 45 to be discharged therefrom in a direction tangential to the atomizer blades 43. The primary air passes through orifices 3 in an annulus A to an annular chamber Ca and then to the stator blades 4. The burner is mounted at one end of a double walled combustion chamber 1 of tapering form connected to a turbine and surrounded by a heat exchanger comprising an inlet 12 and an outlet 15 for combustion products from the turbine and an inlet 16 for combustion air. The air is heated in the heat exchanger and part passes to the stator blades 4, another part passes through helical inlets 5 to the combustion chamber and the rest passes into the space between the double walls of the-combustion chamber. This latter air passes through three sets of apertures 7, 8, 9 into the combustion chamber to provide combustion and diluting air. The apertures 7, 8, 9 may be alternately inclined and perpendicular to the axis of the combustion chamber.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT350149X | 1956-09-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB870988A true GB870988A (en) | 1961-06-21 |
Family
ID=11241092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB27263/57A Expired GB870988A (en) | 1956-09-01 | 1957-08-29 | Improvements in or relating to a liquid fuel atomiser |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE560443A (en) |
| CH (1) | CH350149A (en) |
| FR (1) | FR1183106A (en) |
| GB (1) | GB870988A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1179767B (en) * | 1958-07-31 | 1964-10-15 | Power Jets Res & Dev Ltd | Combustion chamber |
| US3316955A (en) * | 1965-03-08 | 1967-05-02 | Master Cons Inc | Oil burner apparatus |
| FR2774152A1 (en) * | 1998-01-28 | 1999-07-30 | Inst Francais Du Petrole | COMBUSTION CHAMBER OF GAS TURBINE OPERATING ON LIQUID FUEL |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4702073A (en) * | 1986-03-10 | 1987-10-27 | Melconian Jerry O | Variable residence time vortex combustor |
-
0
- BE BE560443D patent/BE560443A/xx unknown
-
1957
- 1957-08-23 CH CH350149D patent/CH350149A/en unknown
- 1957-08-29 GB GB27263/57A patent/GB870988A/en not_active Expired
- 1957-08-30 FR FR1183106D patent/FR1183106A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1179767B (en) * | 1958-07-31 | 1964-10-15 | Power Jets Res & Dev Ltd | Combustion chamber |
| US3316955A (en) * | 1965-03-08 | 1967-05-02 | Master Cons Inc | Oil burner apparatus |
| FR2774152A1 (en) * | 1998-01-28 | 1999-07-30 | Inst Francais Du Petrole | COMBUSTION CHAMBER OF GAS TURBINE OPERATING ON LIQUID FUEL |
| EP0933594A1 (en) * | 1998-01-28 | 1999-08-04 | Institut Francais Du Petrole | Gas turbine combustion chamber for liquid fuel |
| US6378310B1 (en) | 1998-01-28 | 2002-04-30 | Institut Francais Du Petrole | Combustion chamber of a gas turbine working on liquid fuel |
Also Published As
| Publication number | Publication date |
|---|---|
| FR1183106A (en) | 1959-07-03 |
| BE560443A (en) | |
| CH350149A (en) | 1960-11-15 |
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