CH332966A - Turbine à écoulement axial - Google Patents

Turbine à écoulement axial

Info

Publication number
CH332966A
CH332966A CH332966DA CH332966A CH 332966 A CH332966 A CH 332966A CH 332966D A CH332966D A CH 332966DA CH 332966 A CH332966 A CH 332966A
Authority
CH
Switzerland
Prior art keywords
axial flow
flow turbine
turbine
axial
flow
Prior art date
Application number
Other languages
English (en)
Inventor
Bernard Halford Frank
Bennett Gay Arnold Roydon
Original Assignee
Havilland Engine Company Limit
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Havilland Engine Company Limit filed Critical Havilland Engine Company Limit
Publication of CH332966A publication Critical patent/CH332966A/fr

Links

Classifications

    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CH332966D 1953-07-29 1954-07-29 Turbine à écoulement axial CH332966A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB332966X 1953-07-29

Publications (1)

Publication Number Publication Date
CH332966A true CH332966A (fr) 1958-09-30

Family

ID=10351087

Family Applications (1)

Application Number Title Priority Date Filing Date
CH332966D CH332966A (fr) 1953-07-29 1954-07-29 Turbine à écoulement axial

Country Status (2)

Country Link
CH (1) CH332966A (fr)
FR (1) FR1110874A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2540939A1 (fr) * 1983-02-10 1984-08-17 Snecma Anneau d'etancheite pour un rotor de turbine d'une turbomachine et installation de turbomachine munie de tels anneaux

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2043798B (en) * 1979-03-14 1983-01-12 Rolls Royce Gas turbine stator vane assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2540939A1 (fr) * 1983-02-10 1984-08-17 Snecma Anneau d'etancheite pour un rotor de turbine d'une turbomachine et installation de turbomachine munie de tels anneaux
EP0119881A1 (fr) * 1983-02-10 1984-09-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Anneau d'étanchéité pour un rotor de turbine d'une turbomachine et installation de turbomachine munie de tels anneaux

Also Published As

Publication number Publication date
FR1110874A (fr) 1956-02-17

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