BE634363A - - Google Patents

Info

Publication number
BE634363A
BE634363A BE634363DA BE634363A BE 634363 A BE634363 A BE 634363A BE 634363D A BE634363D A BE 634363DA BE 634363 A BE634363 A BE 634363A
Authority
BE
Belgium
Prior art keywords
turbine
turbine according
rotor
fins
nozzle
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE634363A publication Critical patent/BE634363A/fr

Links

Classifications

    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
BE634363D BE634363A (en:Method)

Publications (1)

Publication Number Publication Date
BE634363A true BE634363A (en:Method)

Family

ID=201458

Family Applications (1)

Application Number Title Priority Date Filing Date
BE634363D BE634363A (en:Method)

Country Status (1)

Country Link
BE (1) BE634363A (en:Method)

Similar Documents

Publication Publication Date Title
EP2478198B1 (fr) Turbomoteur a arbres paralleles
WO2015166179A1 (fr) Turbomachine d'aeronef a prelevement de puissance mecanique ameliore
CA2947249A1 (fr) Assemblage pour turbomachine d'aeronef et son procede de montage
US3238721A (en) Engine starter
BE634363A (en:Method)
FR2777943A1 (fr) Moteur thermique a capsulismes differencies et apport de chaleur continu
EP0774572B1 (fr) Turbine à gaz compacte à cycle fermé pour la propulsion d'un véhicule
FR2944832A1 (fr) Moteur rotatif a air equipe de pales coulissantes
FR2491137A1 (fr) Mecanisme de turbines a gaz
FR3025001A1 (fr) Variante simplifiee de moteur thermique rotatif
BE892384A (fr) Moteur rotatif a combustion interne
FR3070725B1 (fr) Turbopompe cinetique avec un dispositif de variation de vitesse pour un circuit ferme, en particulier de type a cycle de rankine, notamment pour un vehicule automobile
FR3065254B1 (fr) Ensemble de turbopompe pour un circuit ferme, en particulier de type a cycle de rankine, associe a un moteur a combustion interne, notamment pour vehicule automobile
CH288545A (fr) Installation motrice.
BE411525A (en:Method)
FR2730274A1 (fr) Moteur a pistons rotatifs et combustion externe
BE335564A (en:Method)
BE490347A (en:Method)
BE534985A (en:Method)
FR2607551A1 (fr) Moteurs a distribution rotative et modules a explosion exterieurs
BE504760A (en:Method)
BE430583A (en:Method)
FR2768769A1 (fr) Moteur rotatif a engrenage
BE531079A (en:Method)
CH377588A (fr) Moteur à turbine à gaz