BE571894A - - Google Patents
Info
- Publication number
- BE571894A BE571894A BE571894DA BE571894A BE 571894 A BE571894 A BE 571894A BE 571894D A BE571894D A BE 571894DA BE 571894 A BE571894 A BE 571894A
- Authority
- BE
- Belgium
- Prior art keywords
- turbine
- housing
- bearing
- gearbox
- shaft
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims description 12
- 239000000969 carrier Substances 0.000 claims description 9
- 230000005540 biological transmission Effects 0.000 claims description 7
- 210000001503 Joints Anatomy 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 230000000875 corresponding Effects 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 239000003638 reducing agent Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000001808 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000003466 welding Methods 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
BE571894A true BE571894A (ja) |
Family
ID=189919
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE571894D BE571894A (ja) |
Country Status (1)
Country | Link |
---|---|
BE (1) | BE571894A (ja) |
-
0
- BE BE571894D patent/BE571894A/fr unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10519871B2 (en) | Support assembly for a propeller shaft | |
US10151249B2 (en) | Gas turbine architecture | |
US6855089B2 (en) | Reduced twist carrier | |
US11174916B2 (en) | Aircraft engine reduction gearbox | |
EP3283747B1 (fr) | Turbomoteur a doublet d'helices contrarotatives dispose en amont du generateur de gaz | |
KR20070095773A (ko) | 유성 기어 열 일체형 태양 기어 커플링 설계 | |
US11268453B1 (en) | Lubrication system for aircraft engine reduction gearbox | |
FR2641333A1 (fr) | Turboreacteur a double flux comportant une turbine contrarotative pour l'entrainement de la soufflante | |
US20180306121A1 (en) | Turbine engine with fan and reduction of speed on the shaft of the power turbine | |
US2968922A (en) | Combustion turbine power units | |
US3271949A (en) | Gas turbine | |
FR3021296A1 (fr) | Ensemble de propulsion a doublet d'helices pour aeronef | |
BE571894A (ja) | ||
FR3035153B1 (fr) | Turbopropulseur a doublet d'helices contrarotatives dispose en amont du generateur de gaz | |
EP4073354B1 (fr) | Pressurisation d'enceintes de lubrification dans une turbomachine a turbine contrarotative | |
FR3041990A1 (fr) | Ensemble de propulsion d'un aeronef | |
US3363413A (en) | Gas turbine | |
US11773771B2 (en) | Turbomachine with counter-rotating turbine for an aircraft | |
FR2573816A1 (fr) | Turboreacteur multiflux multicorps a mecanisme de transmission perfectionne | |
FR3042011B1 (fr) | Ensemble de propulsion d'un aeronef equipe d'une soufflante principale et d'au moins une soufflante deportee | |
EP4033086B1 (fr) | Turbomachine d'aeronef a triple flux equipe d'un module de transmission de puissance | |
FR3042008A1 (fr) | Ensemble de propulsion avec soufflante d'axe decale et reducteur de vitesse sur l'arbre d'entrainement de la soufflante | |
CH355990A (fr) | Installation à turbine à gaz | |
FR3035156A1 (fr) | Turbomoteur a doublet d'helices contrarotatives dispose en amont du generateur de gaz | |
GB856347A (en) | Combustion turbine power units |