CH350506A - Turbomachine stator - Google Patents

Turbomachine stator

Info

Publication number
CH350506A
CH350506A CH350506DA CH350506A CH 350506 A CH350506 A CH 350506A CH 350506D A CH350506D A CH 350506DA CH 350506 A CH350506 A CH 350506A
Authority
CH
Switzerland
Prior art keywords
turbomachine stator
turbomachine
stator
Prior art date
Application number
Other languages
French (fr)
Inventor
Albert Gilbert Ronald
Original Assignee
Napier & Son Ltd
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 Napier & Son Ltd filed Critical Napier & Son Ltd
Publication of CH350506A publication Critical patent/CH350506A/en

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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
CH350506D 1957-04-04 1958-06-16 Turbomachine stator CH350506A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1099057A GB839697A (en) 1957-04-04 1957-04-04 Turbine stator blade rings

Publications (1)

Publication Number Publication Date
CH350506A true CH350506A (en) 1960-11-30

Family

ID=9978019

Family Applications (1)

Application Number Title Priority Date Filing Date
CH350506D CH350506A (en) 1957-04-04 1958-06-16 Turbomachine stator

Country Status (4)

Country Link
CH (1) CH350506A (en)
FR (1) FR1198255A (en)
GB (1) GB839697A (en)
NL (1) NL99147C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603340A1 (en) * 1986-09-03 1988-03-04 Snecma TURBOMACHINE COMPRISING A DEVICE FOR ADJUSTING THE GAMES OF A LABYRINTH JOINT BETWEEN ROTOR AND STATOR AND OF THE GAS VEIN ALIGNMENT AND METHOD OF APPLICATION

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3630633A (en) * 1970-05-07 1971-12-28 Ford Motor Co Gas turbine engine nozzle actuation system
US4767264A (en) * 1986-10-31 1988-08-30 United Technologies Corporation Vane lever arm construction
DE4446624A1 (en) * 1994-12-24 1996-06-27 Klein Schanzlin & Becker Ag Variable pitch propeller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603340A1 (en) * 1986-09-03 1988-03-04 Snecma TURBOMACHINE COMPRISING A DEVICE FOR ADJUSTING THE GAMES OF A LABYRINTH JOINT BETWEEN ROTOR AND STATOR AND OF THE GAS VEIN ALIGNMENT AND METHOD OF APPLICATION
EP0259221A1 (en) * 1986-09-03 1988-03-09 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Labyrinth clearance adjustment for a turbo machine
US4773817A (en) * 1986-09-03 1988-09-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Labyrinth seal adjustment device for incorporation in a turbomachine

Also Published As

Publication number Publication date
NL99147C (en) 1961-09-15
GB839697A (en) 1960-06-29
FR1198255A (en) 1959-12-07

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