BE426281A - - Google Patents
Info
- Publication number
- BE426281A BE426281A BE426281DA BE426281A BE 426281 A BE426281 A BE 426281A BE 426281D A BE426281D A BE 426281DA BE 426281 A BE426281 A BE 426281A
- Authority
- BE
- Belgium
- Prior art keywords
- turbine
- compressor
- combustion chamber
- combustion
- air
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims description 81
- 239000007789 gas Substances 0.000 claims description 44
- 239000000446 fuel Substances 0.000 claims description 37
- 238000000034 method Methods 0.000 claims description 33
- 230000006835 compression Effects 0.000 claims description 17
- 238000007906 compression Methods 0.000 claims description 17
- 230000007423 decrease Effects 0.000 claims description 10
- 238000010276 construction Methods 0.000 claims description 8
- 239000007788 liquid Substances 0.000 claims description 8
- 238000000889 atomisation Methods 0.000 claims description 6
- 238000001816 cooling Methods 0.000 claims description 5
- 230000033001 locomotion Effects 0.000 claims description 5
- 239000007921 spray Substances 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 4
- 239000003795 chemical substances by application Substances 0.000 claims description 3
- 238000005192 partition Methods 0.000 claims description 3
- 239000000567 combustion gas Substances 0.000 claims description 2
- 238000011144 upstream manufacturing Methods 0.000 claims description 2
- 230000005540 biological transmission Effects 0.000 claims 1
- 230000000149 penetrating effect Effects 0.000 claims 1
- 230000002349 favourable effect Effects 0.000 description 10
- 238000002156 mixing Methods 0.000 description 5
- 230000002093 peripheral effect Effects 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000010298 pulverizing process Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 238000000844 transformation Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000004566 building material Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 230000037213 diet Effects 0.000 description 1
- 235000005911 diet Nutrition 0.000 description 1
- 230000000694 effects 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
- 238000010438 heat treatment Methods 0.000 description 1
- 230000036540 impulse transmission Effects 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000004449 solid propellant Substances 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002918 waste heat Substances 0.000 description 1
Classifications
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/003—Gas-turbine plants with heaters between turbine stages
-
- 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)
- Engine Equipment That Uses Special Cycles (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE426281A true BE426281A (OSRAM) |
Family
ID=87100
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE426281D BE426281A (OSRAM) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE426281A (OSRAM) |
-
0
- BE BE426281D patent/BE426281A/fr unknown
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2940978C (fr) | Rotor de soufflante pour une turbomachine telle qu'un turboreacteur multiflux entraine par reducteur | |
| EP0403372B1 (fr) | Propulseur combiné turbofusée statoréacteur à réchauffe et son procédé de fonctionnement | |
| EP1445421B1 (fr) | Dispositif de ventilation d'un rotor de turbine à haute pression d'une turbomachine | |
| CA2564491C (fr) | Dispositif de ventilation de disques de turbine dans un moteur a turbine a gaz | |
| CA2774453C (fr) | Turbomoteur a arbres paralleles | |
| FR2491138A1 (fr) | Procede pour controler le jeu radial entre les ailettes et le stator dans un moteur a turbine a gaz et moteur a turbine a gaz avec dispositif pour la mise en oeuvre du procede | |
| EP2525062A1 (fr) | Turbomachine à chambre de détonation et engin volant pourvu d'une telle turbomachine | |
| CA2430143C (fr) | Refroidissement du flasque amont d'une turbine a haute pression par un systeme a double injecteurs fond de chambre | |
| FR2686654A1 (fr) | Ameliorations dans la propulsion aerospatiale. | |
| FR2892153A1 (fr) | Groupe turboreacteur | |
| FR2507680A1 (fr) | Injecteur d'air et dispositif d'injection d'air pour le refroidissement d'aubes de turbine et moteur a turbine a gaz ainsi obtenu | |
| BE1024081A1 (fr) | Refroidissement de turbomachine par evaporation | |
| FR2669680A1 (fr) | Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants. | |
| FR2875269A1 (fr) | Systeme de refroidissement pour moteur a turbine a gaz ayant un systeme central ameliore | |
| EP0301950B1 (fr) | Moteur à combustion interne suralimenté équipé d'une chambrede combustion auxiliaire | |
| BE426281A (OSRAM) | ||
| FR2605679A1 (fr) | Turboreacteur a rotor tambour, plusieurs corps et plusieurs flux | |
| FR3068075A1 (fr) | Systeme de combustion a volume constant comprenant un element d'obturation tournant a lumieres segmentees | |
| BE525244A (OSRAM) | ||
| FR2491137A1 (fr) | Mecanisme de turbines a gaz | |
| EP1359309B1 (fr) | Turbine à gaz comportant un dispositif de mélange de gaz à lobes et à tubes | |
| FR3092621A1 (fr) | Turbomachine pourvue d’un récupérateur de chaleur en sortie de turbine | |
| BE468329A (OSRAM) | ||
| FR3134146A1 (fr) | Turbomachine à chambre de combustion à gain de pression | |
| FR3052197A1 (fr) | Turbopompe, notamment pour moteur-fusee a ergols cryogeniques |