BE499468A - - Google Patents
Info
- Publication number
- BE499468A BE499468A BE499468DA BE499468A BE 499468 A BE499468 A BE 499468A BE 499468D A BE499468D A BE 499468DA BE 499468 A BE499468 A BE 499468A
- Authority
- BE
- Belgium
- Prior art keywords
- nozzle
- fuel
- outlet
- supply duct
- pressure
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims description 26
- 238000002485 combustion reaction Methods 0.000 claims description 12
- 239000012530 fluid Substances 0.000 claims description 10
- 238000011144 upstream manufacturing Methods 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 3
- 239000007789 gas Substances 0.000 description 8
- 239000000047 product Substances 0.000 description 7
- 238000003303 reheating Methods 0.000 description 5
- 238000009834 vaporization Methods 0.000 description 3
- 230000008016 vaporization Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000006227 byproduct Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
BE499468A true BE499468A (enrdf_load_stackoverflow) |
Family
ID=141869
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE499468D BE499468A (enrdf_load_stackoverflow) |
Country Status (1)
Country | Link |
---|---|
BE (1) | BE499468A (enrdf_load_stackoverflow) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2771743A (en) * | 1951-08-10 | 1956-11-27 | Rolls Royce | Gas-turbine engine with reheat combustion equipment |
US2799991A (en) * | 1954-03-05 | 1957-07-23 | Earl W Conrad | Afterburner flame stabilization means |
US3020709A (en) * | 1952-05-21 | 1962-02-13 | Snecma | Control means of the flow of a fluid by another flow |
-
0
- BE BE499468D patent/BE499468A/fr unknown
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2771743A (en) * | 1951-08-10 | 1956-11-27 | Rolls Royce | Gas-turbine engine with reheat combustion equipment |
US3020709A (en) * | 1952-05-21 | 1962-02-13 | Snecma | Control means of the flow of a fluid by another flow |
US2799991A (en) * | 1954-03-05 | 1957-07-23 | Earl W Conrad | Afterburner flame stabilization means |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2483045A (en) | Jet engine, including a combustion chamber to which gaseous fuel is delivered under pressure | |
FR2634005A1 (fr) | Ensemble injecteur de carburant de pilotage pour un statoreacteur supersonique | |
FR2774455A1 (fr) | Systeme de combustion pour moteur a turbine a gaz et son procede de mise en oeuvre | |
FR2676511A1 (fr) | Machine soufflante radiale comportant un rotor de soufflante tournant dans un carter en spirale comme air secondaire a la veine de gaz d'echappement d'un moteur a combustion interne, notamment d'automobile. | |
JP2008502845A (ja) | 燃焼エンジンのガス流改善装置 | |
EP0933594B1 (fr) | Procédé de fonctionnement d'une chambre de combustion de turbine à gaz fonctionnant au carburant liquide | |
CA2634615C (fr) | Chambre de combustion de turbomachine a circulation helicoidale de l'air | |
EP0224397B1 (fr) | Dispositif d'injection à bol sectorisé | |
US2482394A (en) | Gas turbine | |
FR2883601A1 (fr) | Dispositif d'acceleration d'un groupe de turbocompression aux bas regimes d'un moteur alternatif et moteur alternatif comportant un tel dispositif | |
BE499468A (enrdf_load_stackoverflow) | ||
EP1577530B1 (fr) | Dispositif et méthode d'allumage d'un système de post-combustion pour turbo-réacteur à double flux | |
RU2261998C1 (ru) | Газотурбинный двигатель | |
FR2495221A1 (fr) | Structure de conduit d'admission pour moteurs a combustion interne | |
FR2932250A1 (fr) | Moteur a turbine a gaz comprenant des bouches de prelevement d'air | |
BE537785A (enrdf_load_stackoverflow) | ||
SU264656A1 (ru) | УСТРОЙСТВО дл ОТБОРА ГОРЯЧИХ ГАЗОВ, ВЫХОДЯЩИХ из СОПЛА РЕАКТИВНОГО ДВИГАТЕЛЯ | |
FR2904684A1 (fr) | Dispositif de post-combustion pour moteur a turbine a gaz | |
RU2133366C1 (ru) | Турбореактивный двигатель | |
CN2471940Y (zh) | 小型燃气轮机 | |
FR2872866A1 (fr) | Dispositif d'injection de melange carbure pour un moteur de vehicule automobile | |
FR3156508A1 (fr) | Chambre de combustion annulaire pour turbine à gaz bas-carbone. | |
BE545344A (enrdf_load_stackoverflow) | ||
BE344440A (enrdf_load_stackoverflow) | ||
CH321265A (fr) | Procédé de réglage d'un propulseur d'avion comprenant au moins un compresseur et une turbine à gaz |