BE498664A - - Google Patents

Info

Publication number
BE498664A
BE498664A BE498664DA BE498664A BE 498664 A BE498664 A BE 498664A BE 498664D A BE498664D A BE 498664DA BE 498664 A BE498664 A BE 498664A
Authority
BE
Belgium
Prior art keywords
compressor
turbine
rotor
shaft
reduction gear
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE498664A publication Critical patent/BE498664A/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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F02C3/103Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE498664D BE498664A (enrdf_load_html_response)

Publications (1)

Publication Number Publication Date
BE498664A true BE498664A (enrdf_load_html_response)

Family

ID=141274

Family Applications (1)

Application Number Title Priority Date Filing Date
BE498664D BE498664A (enrdf_load_html_response)

Country Status (1)

Country Link
BE (1) BE498664A (enrdf_load_html_response)

Similar Documents

Publication Publication Date Title
JP5667668B2 (ja) ガスタービンエンジン組立方法
FR2692627A1 (fr) Ensemble de carters de compresseur, installation de prélèvement d'air pour ceux-ci et procédé de régulation de la distorsion de cet ensemble de carters.
FR2605357A1 (fr) Admission pour un moteur a turbine a gaz a turbopropulseur
FR2614937A1 (fr) Turbopropulseur de type propfan a systeme de lubrification d'huile annulaire
FR2922860A1 (fr) Amelioration aux giravions equipes de turbomoteurs
FR2581423A1 (fr) Turbine de travail a contre-rotation
EP4168659B1 (fr) Turbomachine d'aeronef a cycle recupere
US20220056850A1 (en) Air turbine starter with lubricated bearing assembly
EP3861195B1 (fr) Turboréacteur à double flux comprenant un cône de sortie refroidi par son flux secondaire
US3271949A (en) Gas turbine
BE498664A (enrdf_load_html_response)
FR2899272A1 (fr) Bras de passage des servitudes dans un carter intermediaire de turboreacteur
FR3035153B1 (fr) Turbopropulseur a doublet d'helices contrarotatives dispose en amont du generateur de gaz
CH287353A (fr) Groupe moteur comprenant une turbine à gaz.
FR2491137A1 (fr) Mecanisme de turbines a gaz
FR3156490A1 (fr) Pompe pour fluide cryotechnique
WO2024246459A1 (fr) Turbomachine d'aeronef a cycle recupere
WO2024175849A1 (fr) Systeme d'echange de chaleur pour une turbomachine d'aeronef
FR3104212A1 (fr) Turbomachine a turbine contrarotative pour un aeronef
Propeller Notes on the Bristol Theseus Heat-Exchanger Propeller Turbine
BE460696A (enrdf_load_html_response)
BE534985A (enrdf_load_html_response)
BE531079A (enrdf_load_html_response)
BE462570A (enrdf_load_html_response)
BE463343A (enrdf_load_html_response)