BE480530A - - Google Patents
Info
- Publication number
- BE480530A BE480530A BE480530DA BE480530A BE 480530 A BE480530 A BE 480530A BE 480530D A BE480530D A BE 480530DA BE 480530 A BE480530 A BE 480530A
- Authority
- BE
- Belgium
- Prior art keywords
- fuel
- valve
- turbine
- speed
- orifice
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims description 110
- 238000002485 combustion reaction Methods 0.000 claims description 31
- 230000001133 acceleration Effects 0.000 claims description 16
- 230000000875 corresponding Effects 0.000 claims description 16
- 239000007789 gas Substances 0.000 claims description 16
- 239000000203 mixture Substances 0.000 claims description 9
- 230000000694 effects Effects 0.000 claims description 4
- 230000001105 regulatory Effects 0.000 claims description 4
- 238000006073 displacement reaction Methods 0.000 claims description 3
- 239000003570 air Substances 0.000 claims 6
- 230000001276 controlling effect Effects 0.000 claims 2
- 239000012080 ambient air Substances 0.000 claims 1
- 238000009432 framing Methods 0.000 claims 1
- 210000000056 organs Anatomy 0.000 claims 1
- 238000005192 partition Methods 0.000 claims 1
- 210000000188 Diaphragm Anatomy 0.000 description 13
- 210000003128 Head Anatomy 0.000 description 7
- 239000002775 capsule Substances 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 241000196324 Embryophyta Species 0.000 description 3
- 238000000889 atomisation Methods 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000009792 diffusion process Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000006011 modification reaction Methods 0.000 description 2
- 230000037250 Clearance Effects 0.000 description 1
- 229920002456 HOTAIR Polymers 0.000 description 1
- 235000008694 Humulus lupulus Nutrition 0.000 description 1
- 240000006600 Humulus lupulus Species 0.000 description 1
- 210000001331 Nose Anatomy 0.000 description 1
- 241000022563 Rema Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 210000002268 Wool Anatomy 0.000 description 1
- 230000000903 blocking Effects 0.000 description 1
- 230000035512 clearance Effects 0.000 description 1
- 230000003247 decreasing Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010892 electric spark Methods 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000003546 flue gas Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- JVTAAEKCZFNVCJ-UHFFFAOYSA-N lactic acid Chemical compound CC(O)C(O)=O JVTAAEKCZFNVCJ-UHFFFAOYSA-N 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 230000002093 peripheral Effects 0.000 description 1
- 230000001141 propulsive Effects 0.000 description 1
- 230000001340 slower Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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)
- Feeding And Controlling Fuel (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
BE480530A true BE480530A (zh) |
Family
ID=127727
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE480530D BE480530A (zh) |
Country Status (1)
Country | Link |
---|---|
BE (1) | BE480530A (zh) |
-
0
- BE BE480530D patent/BE480530A/fr unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR3028888A1 (fr) | Dispositif de refroidissement pour une turbomachine alimente par un circuit de decharge | |
EP1861598A2 (fr) | Dispositif d'acceleration d'un groupe de turbocompression aux bas regimes d'un moteur alternatif et moteur alternatif comportant un tel dispositif | |
FR2669680A1 (fr) | Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants. | |
EP0307264A1 (fr) | Circuit de distribution de carburant à refroidissement accru du carburant | |
EP2333247B1 (fr) | Procédé pour augmenter la sécurité d'une installation motrice, et installation motrice apte à mettre en oeuvre ce procédé | |
EP0301950B1 (fr) | Moteur à combustion interne suralimenté équipé d'une chambrede combustion auxiliaire | |
WO2015197974A1 (fr) | Dispositif de refroidissement pour une turbomachine | |
CA2364181C (fr) | Clapet de pressurisation a deux niveaux commande par un doseur de carburant | |
FR2806446A1 (fr) | Turbocompresseur | |
BE480530A (zh) | ||
EP0806611A1 (fr) | Systéme d'injection à geometrie variable adoptant un debit d'air en fonction du regime moteur | |
FR2718190A1 (fr) | Soupape de régulation d'injection de carburant pour une turbomachine. | |
BE490787A (zh) | ||
BE480582A (zh) | ||
FR2690712A1 (fr) | Ensemble propulsif à moteurs à cycle variable et sa méthode d'utilisation. | |
BE475975A (zh) | ||
BE569711A (zh) | ||
CH321265A (fr) | Procédé de réglage d'un propulseur d'avion comprenant au moins un compresseur et une turbine à gaz | |
BE480532A (zh) | ||
CH328858A (fr) | Installation d'alimentation en combustible d'un moteur à combustion interne | |
FR3144206A1 (fr) | Procédure de rallumage de chambre de combustion | |
FR3144223A1 (fr) | Procédé de fonctionnement d'un moteur à turbine à gaz | |
BE529130A (zh) | ||
BE556686A (zh) | ||
BE497651A (zh) |