CA561070A - Turbo machines having adjustable guide blades - Google Patents

Turbo machines having adjustable guide blades

Info

Publication number
CA561070A
CA561070A CA561070A CA561070DA CA561070A CA 561070 A CA561070 A CA 561070A CA 561070 A CA561070 A CA 561070A CA 561070D A CA561070D A CA 561070DA CA 561070 A CA561070 A CA 561070A
Authority
CA
Canada
Prior art keywords
guide blades
adjustable guide
turbo machines
turbo
machines
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
CA561070A
Other languages
French (fr)
Inventor
H. A. Magin Sidney
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.)
Publication date
Application granted granted Critical
Publication of CA561070A publication Critical patent/CA561070A/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
CA561070A 1952-10-03 Turbo machines having adjustable guide blades Expired CA561070A (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
CA561070A true CA561070A (en) 1958-07-29

Family

ID=10218932

Family Applications (1)

Application Number Title Priority Date Filing Date
CA561070A Expired CA561070A (en) 1952-10-03 Turbo machines having adjustable guide blades

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
US3038697A (en) * 1960-07-05 1962-06-12 Chrysler Corp Gas turbine adjustable nozzle and interstage inner shroud suspension
US3392958A (en) * 1966-06-03 1968-07-16 Rover Co Ltd Adjustable nozzle guide vane assembly for an axial flow turbine

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE556572A (en) * 1955-08-16
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
US3630633A (en) * 1970-05-07 1971-12-28 Ford Motor Co Gas turbine engine nozzle actuation system
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
US3038697A (en) * 1960-07-05 1962-06-12 Chrysler Corp Gas turbine adjustable nozzle and interstage inner shroud suspension
US3392958A (en) * 1966-06-03 1968-07-16 Rover Co Ltd Adjustable nozzle guide vane assembly for an axial flow turbine

Also Published As

Publication number Publication date
FR1084493A (en) 1955-01-19
GB737472A (en) 1955-09-28

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