GB2091409B - Variable area means for air systems of air blast type fuel nozzle assemblies - Google Patents
Variable area means for air systems of air blast type fuel nozzle assembliesInfo
- Publication number
- GB2091409B GB2091409B GB8132583A GB8132583A GB2091409B GB 2091409 B GB2091409 B GB 2091409B GB 8132583 A GB8132583 A GB 8132583A GB 8132583 A GB8132583 A GB 8132583A GB 2091409 B GB2091409 B GB 2091409B
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- fuel nozzle
- type fuel
- variable area
- nozzle assemblies
- 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
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/008—Flow control devices
-
- 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
- F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US21228180A | 1980-12-02 | 1980-12-02 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2091409A GB2091409A (en) | 1982-07-28 |
GB2091409B true GB2091409B (en) | 1985-03-20 |
Family
ID=22790361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8132583A Expired GB2091409B (en) | 1980-12-02 | 1981-10-29 | Variable area means for air systems of air blast type fuel nozzle assemblies |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS57120018A (en) |
CA (1) | CA1188111A (en) |
FR (1) | FR2495285A1 (en) |
GB (1) | GB2091409B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3317035A1 (en) * | 1983-05-10 | 1984-11-15 | BBC Aktiengesellschaft Brown, Boveri & Cie., Baden, Aargau | MULTIPLE BURNER |
DE3737247C1 (en) * | 1987-11-03 | 1989-03-02 | Zettner Michael L | Burner |
DE4220060C2 (en) * | 1992-06-19 | 1996-10-17 | Mtu Muenchen Gmbh | Device for actuating a swirl device of a burner for gas turbine engines that controls the throughput of combustion air |
US5505045A (en) * | 1992-11-09 | 1996-04-09 | Fuel Systems Textron, Inc. | Fuel injector assembly with first and second fuel injectors and inner, outer, and intermediate air discharge chambers |
DE4424599A1 (en) * | 1994-07-13 | 1996-01-18 | Abb Research Ltd | Method and device for operating a combined burner for liquid and gaseous fuels |
DE4424597B4 (en) * | 1994-07-13 | 2006-03-23 | Alstom | incinerator |
DE19618856B4 (en) * | 1996-05-10 | 2006-04-13 | Alstom | Device for operating an annular combustion chamber equipped with combined burners for liquid and gaseous fuels |
EP3018410B1 (en) | 2014-11-10 | 2017-05-17 | Valli Zabban S.p.A. | Plant and method for reducing bitumen fumes |
CN117948610B (en) * | 2024-03-21 | 2024-06-18 | 大同知了科技有限公司 | Shock wave device, shock wave gasification burner and combustion method |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2655787A (en) * | 1949-11-21 | 1953-10-20 | United Aircraft Corp | Gas turbine combustion chamber with variable area primary air inlet |
FR1053386A (en) * | 1952-04-03 | 1954-02-02 | Liquid fuel burner and apparatus for its implementation | |
DE952857C (en) * | 1953-09-30 | 1956-11-22 | Max Adolf Mueller Dipl Ing | Device for heating the secondary circuits of twin-circuit jet engines |
US3827638A (en) * | 1973-05-23 | 1974-08-06 | Ex Cell O Corp | Fuel spray nozzle |
FR2265979B1 (en) * | 1974-03-29 | 1977-10-14 | France Etat | |
GB1601218A (en) * | 1978-03-20 | 1981-10-28 | Rolls Royce | Combustion equipment for gas turbine engines |
US4216652A (en) * | 1978-06-08 | 1980-08-12 | General Motors Corporation | Integrated, replaceable combustor swirler and fuel injector |
-
1981
- 1981-10-28 CA CA000388912A patent/CA1188111A/en not_active Expired
- 1981-10-29 GB GB8132583A patent/GB2091409B/en not_active Expired
- 1981-12-01 FR FR8122482A patent/FR2495285A1/en active Pending
- 1981-12-01 JP JP19188981A patent/JPS57120018A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
GB2091409A (en) | 1982-07-28 |
JPS57120018A (en) | 1982-07-26 |
FR2495285A1 (en) | 1982-06-04 |
CA1188111A (en) | 1985-06-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19921029 |