FR1084493A - Turbo-machine with adjustable guide vanes - Google Patents

Turbo-machine with adjustable guide vanes

Info

Publication number
FR1084493A
FR1084493A FR1084493DA FR1084493A FR 1084493 A FR1084493 A FR 1084493A FR 1084493D A FR1084493D A FR 1084493DA FR 1084493 A FR1084493 A FR 1084493A
Authority
FR
France
Prior art keywords
turbo
machine
guide vanes
adjustable guide
adjustable
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 FR1084493A publication Critical patent/FR1084493A/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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1084493D 1952-10-03 1953-09-30 Turbo-machine with adjustable guide vanes Expired FR1084493A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2489452A GB737472A (en) 1952-10-03 1952-10-03 Turbines and like machines having adjustable guide blades

Publications (1)

Publication Number Publication Date
FR1084493A true FR1084493A (en) 1955-01-19

Family

ID=10218932

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1084493D Expired FR1084493A (en) 1952-10-03 1953-09-30 Turbo-machine with adjustable guide vanes

Country Status (3)

Country Link
CA (1) CA561070A (en)
FR (1) FR1084493A (en)
GB (1) GB737472A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2862357A (en) * 1955-08-16 1958-12-02 Rolls Royce Turbines
US3630633A (en) * 1970-05-07 1971-12-28 Ford Motor Co Gas turbine engine nozzle actuation system

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2854211A (en) * 1955-11-25 1958-09-30 Gen Electric Adjustable vane arrangement for fluid flow machinery
NL251063A (en) * 1959-04-30 1900-01-01
US3038697A (en) * 1960-07-05 1962-06-12 Chrysler Corp Gas turbine adjustable nozzle and interstage inner shroud suspension
GB1119439A (en) * 1966-06-03 1968-07-10 Rover Co Ltd Adjustable nozzle guide vane assembly for an axial flow turbine
DE3427528C1 (en) * 1984-07-26 1985-08-22 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8500 Nürnberg Device for regulating the extraction pressure of a extraction condensation turbine
FR2681640B1 (en) * 1991-09-25 1993-11-19 Snecma VARIABLE TIMING STATOR BLADE TURBOMACHINE.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2862357A (en) * 1955-08-16 1958-12-02 Rolls Royce Turbines
US3630633A (en) * 1970-05-07 1971-12-28 Ford Motor Co Gas turbine engine nozzle actuation system

Also Published As

Publication number Publication date
CA561070A (en) 1958-07-29
GB737472A (en) 1955-09-28

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