BE402002A - - Google Patents
Info
- Publication number
- BE402002A BE402002A BE402002DA BE402002A BE 402002 A BE402002 A BE 402002A BE 402002D A BE402002D A BE 402002DA BE 402002 A BE402002 A BE 402002A
- Authority
- BE
- Belgium
- Prior art keywords
- air
- pipe
- auxiliary
- sprayer
- passage
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims description 6
- 239000007788 liquid Substances 0.000 claims description 4
- 230000001105 regulatory effect Effects 0.000 claims description 4
- 238000002485 combustion reaction Methods 0.000 description 5
- 239000007921 spray Substances 0.000 description 3
- 239000003595 mist Substances 0.000 description 2
- RFBVBRVVOPAAFS-UHFFFAOYSA-N 2,2-bis(hydroxymethyl)-1-azabicyclo[2.2.2]octan-3-one Chemical compound C1CC2CCN1C(CO)(CO)C2=O RFBVBRVVOPAAFS-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 239000004071 soot Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
Classifications
-
- 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
- F23D11/26—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 with provision for varying the rate at which the fuel is sprayed
- F23D11/28—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 with provision for varying the rate at which the fuel is sprayed with flow-back of fuel at the burner, e.g. using by-pass
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)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE402002A true BE402002A (en:Method) |
Family
ID=67837
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE402002D BE402002A (en:Method) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE402002A (en:Method) |
-
0
- BE BE402002D patent/BE402002A/fr unknown
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