FR1281702A - Adjustable guide vane bearing device for gas turbines or hot air turbines - Google Patents

Adjustable guide vane bearing device for gas turbines or hot air turbines

Info

Publication number
FR1281702A
FR1281702A FR853713A FR853713A FR1281702A FR 1281702 A FR1281702 A FR 1281702A FR 853713 A FR853713 A FR 853713A FR 853713 A FR853713 A FR 853713A FR 1281702 A FR1281702 A FR 1281702A
Authority
FR
France
Prior art keywords
turbines
hot air
bearing device
guide vane
adjustable guide
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
FR853713A
Other languages
French (fr)
Inventor
Hans Gassmann
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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 DED32864A external-priority patent/DE1120819B/en
Application filed by Daimler Benz AG filed Critical Daimler Benz AG
Priority to FR853713A priority Critical patent/FR1281702A/en
Application granted granted Critical
Publication of FR1281702A publication Critical patent/FR1281702A/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)
FR853713A 1960-03-15 1961-02-24 Adjustable guide vane bearing device for gas turbines or hot air turbines Expired FR1281702A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR853713A FR1281702A (en) 1960-03-15 1961-02-24 Adjustable guide vane bearing device for gas turbines or hot air turbines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DED32864A DE1120819B (en) 1960-03-15 1960-03-15 Storage of adjustable guide vanes for gas turbines or hot air turbines
FR853713A FR1281702A (en) 1960-03-15 1961-02-24 Adjustable guide vane bearing device for gas turbines or hot air turbines

Publications (1)

Publication Number Publication Date
FR1281702A true FR1281702A (en) 1962-01-12

Family

ID=25971062

Family Applications (1)

Application Number Title Priority Date Filing Date
FR853713A Expired FR1281702A (en) 1960-03-15 1961-02-24 Adjustable guide vane bearing device for gas turbines or hot air turbines

Country Status (1)

Country Link
FR (1) FR1281702A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1301650B (en) * 1965-01-30 1969-08-21 Rolls Royce By-pass gas turbine jet engine
US4514141A (en) * 1982-04-08 1985-04-30 S.N.E.C.M.A. Safety stop for a variable setting stator blade pivot

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1301650B (en) * 1965-01-30 1969-08-21 Rolls Royce By-pass gas turbine jet engine
US4514141A (en) * 1982-04-08 1985-04-30 S.N.E.C.M.A. Safety stop for a variable setting stator blade pivot

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