CH464607A - Axial flow gas turbine - Google Patents

Axial flow gas turbine

Info

Publication number
CH464607A
CH464607A CH776767A CH776767A CH464607A CH 464607 A CH464607 A CH 464607A CH 776767 A CH776767 A CH 776767A CH 776767 A CH776767 A CH 776767A CH 464607 A CH464607 A CH 464607A
Authority
CH
Switzerland
Prior art keywords
gas turbine
axial flow
flow gas
axial
turbine
Prior art date
Application number
CH776767A
Other languages
French (fr)
Inventor
Noel Penny Robert
John Poole Joseph
Original Assignee
Rover Co 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 Rover Co Ltd filed Critical Rover Co Ltd
Publication of CH464607A publication Critical patent/CH464607A/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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6033—Ceramic matrix composites [CMC]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH776767A 1966-06-03 1967-06-01 Axial flow gas turbine CH464607A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB24823/66A GB1119439A (en) 1966-06-03 1966-06-03 Adjustable nozzle guide vane assembly for an axial flow turbine

Publications (1)

Publication Number Publication Date
CH464607A true CH464607A (en) 1968-10-31

Family

ID=10217784

Family Applications (1)

Application Number Title Priority Date Filing Date
CH776767A CH464607A (en) 1966-06-03 1967-06-01 Axial flow gas turbine

Country Status (4)

Country Link
US (1) US3392958A (en)
CH (1) CH464607A (en)
DE (1) DE1601636B2 (en)
GB (1) GB1119439A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4278398A (en) * 1978-12-04 1981-07-14 General Electric Company Apparatus for maintaining variable vane clearance
US4239450A (en) * 1979-05-17 1980-12-16 Buffalo Forge Company Adjusting mechanism for variable inlet vane
US4302149A (en) * 1980-02-19 1981-11-24 General Motors Corporation Ceramic vane drive joint
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
DE4237031C1 (en) * 1992-11-03 1994-02-10 Mtu Muenchen Gmbh Adjustable guide vane
US5704762A (en) * 1993-11-08 1998-01-06 Alliedsignal Inc. Ceramic-to-metal stator vane assembly
DE102010021145A1 (en) * 2010-05-21 2011-11-24 Mtu Aero Engines Gmbh Adjustable guide vane and turbomachine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2364672A (en) * 1939-03-06 1944-12-12 Stevenson Engineering Corp Aerial propulsion
US2412365A (en) * 1943-10-26 1946-12-10 Wright Aeronautical Corp Variable turbine nozzle
US2486643A (en) * 1946-02-06 1949-11-01 Richard S Graham Reversible propeller
US2643852A (en) * 1950-01-09 1953-06-30 Us Air Force High-speed turbine
CA561070A (en) * 1952-10-03 1958-07-29 H. A. Magin Sidney Turbo machines having adjustable guide blades

Also Published As

Publication number Publication date
DE1601636B2 (en) 1970-11-05
GB1119439A (en) 1968-07-10
DE1601636A1 (en) 1970-06-18
US3392958A (en) 1968-07-16

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