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
Application number
Other languages
English (en)
French (fr)
Publication of BE571894A publication Critical patent/BE571894A/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162Bearing supports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/20Mounting 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)
BE571894D BE571894A (ja)

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)

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