CH306452A - Turbomaschine mit verstellbaren Leitschaufeln. - Google Patents

Turbomaschine mit verstellbaren Leitschaufeln.

Info

Publication number
CH306452A
CH306452A CH306452DA CH306452A CH 306452 A CH306452 A CH 306452A CH 306452D A CH306452D A CH 306452DA CH 306452 A CH306452 A CH 306452A
Authority
CH
Switzerland
Prior art keywords
turbomachine
guide vanes
adjustable guide
adjustable
vanes
Prior art date
Application number
Other languages
English (en)
Inventor
Featonby Joseph
Original Assignee
Nat Research Council
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
Priority claimed from US223673A external-priority patent/US2697326A/en
Application filed by Nat Research Council filed Critical Nat Research Council
Publication of CH306452A publication Critical patent/CH306452A/de

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162Final 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)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH306452D 1951-04-30 1952-04-29 Turbomaschine mit verstellbaren Leitschaufeln. CH306452A (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US223673A US2697326A (en) 1951-04-30 1951-04-30 Reactor with adjustable stator blades
US468955A US2809803A (en) 1951-04-30 1954-11-15 Turbine with adjustable stator blades

Publications (1)

Publication Number Publication Date
CH306452A true CH306452A (de) 1955-04-15

Family

ID=26918018

Family Applications (1)

Application Number Title Priority Date Filing Date
CH306452D CH306452A (de) 1951-04-30 1952-04-29 Turbomaschine mit verstellbaren Leitschaufeln.

Country Status (6)

Country Link
US (1) US2809803A (de)
CH (1) CH306452A (de)
DE (1) DE952141C (de)
FR (1) FR1055261A (de)
GB (1) GB732788A (de)
NL (1) NL81035C (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603340A1 (fr) * 1986-09-03 1988-03-04 Snecma Turbomachine comportant un dispositif d'ajustement des jeux d'un joint a labyrinthe entre rotor et stator et de l'alignement de veine des gaz et methode d'application

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2919890A (en) * 1955-09-16 1960-01-05 Gen Electric Adjustable gas turbine nozzle assembly
US4302149A (en) * 1980-02-19 1981-11-24 General Motors Corporation Ceramic vane drive joint
US4395195A (en) * 1980-05-16 1983-07-26 United Technologies Corporation Shroud ring for use in a gas turbine engine
DE3913102C1 (de) * 1989-04-21 1990-05-31 Mtu Muenchen Gmbh
GB2410066A (en) * 2004-01-13 2005-07-20 Rolls Royce Plc A stator vane arrangement
DE102008033560A1 (de) * 2008-07-17 2010-01-21 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk mit verstellbaren Leitschaufeln

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE559674C (de) * 1931-03-24 1932-09-23 Aeg Regelungsvorrichtung zur Veraenderung der Steigung eines Propellers, insbesondere zum Ansaugen der Kuehlluft fuer Kraftfahrzeuge
CH244431A (de) * 1944-11-10 1946-09-15 Bbc Brown Boveri & Cie Einrichtung zur Regelung von Verbrennungsturbinenanlagen.
GB617173A (en) * 1946-02-27 1949-02-02 Power Jets Res & Dev Ltd Improvements in internal combustion turbine engines
NL75411C (de) * 1946-03-20

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603340A1 (fr) * 1986-09-03 1988-03-04 Snecma Turbomachine comportant un dispositif d'ajustement des jeux d'un joint a labyrinthe entre rotor et stator et de l'alignement de veine des gaz et methode d'application
EP0259221A1 (de) * 1986-09-03 1988-03-09 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Labyrinthspielanpassung für eine Turbomaschine
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
FR1055261A (fr) 1954-02-17
US2809803A (en) 1957-10-15
DE952141C (de) 1956-11-08
GB732788A (en) 1955-06-29
NL81035C (de)

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