FR1198255A - Turbine stator - Google Patents

Turbine stator

Info

Publication number
FR1198255A
FR1198255A FR1198255DA FR1198255A FR 1198255 A FR1198255 A FR 1198255A FR 1198255D A FR1198255D A FR 1198255DA FR 1198255 A FR1198255 A FR 1198255A
Authority
FR
France
Prior art keywords
turbine stator
stator
turbine
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Napier Turbochargers Ltd
Original Assignee
D Napier and 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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Application granted granted Critical
Publication of FR1198255A publication Critical patent/FR1198255A/en
Expired legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
FR1198255D 1957-04-04 1958-06-16 Turbine stator Expired FR1198255A (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
FR1198255A true FR1198255A (en) 1959-12-07

Family

ID=9978019

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1198255D Expired FR1198255A (en) 1957-04-04 1958-06-16 Turbine stator

Country Status (4)

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

Families Citing this family (4)

* 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
FR2603340B1 (en) * 1986-09-03 1988-11-04 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
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

Also Published As

Publication number Publication date
NL99147C (en) 1961-09-15
GB839697A (en) 1960-06-29
CH350506A (en) 1960-11-30

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