CH404841A - Turbomachinery with adjustable blades - Google Patents

Turbomachinery with adjustable blades

Info

Publication number
CH404841A
CH404841A CH1193763A CH1193763A CH404841A CH 404841 A CH404841 A CH 404841A CH 1193763 A CH1193763 A CH 1193763A CH 1193763 A CH1193763 A CH 1193763A CH 404841 A CH404841 A CH 404841A
Authority
CH
Switzerland
Prior art keywords
turbomachinery
adjustable blades
blades
adjustable
Prior art date
Application number
CH1193763A
Other languages
German (de)
Inventor
Schuerch Andreas
Pettersen Johan
Original Assignee
Bbc Brown Boveri & Cie
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 Bbc Brown Boveri & Cie filed Critical Bbc Brown Boveri & Cie
Priority to CH1193763A priority Critical patent/CH404841A/en
Priority to GB3915564A priority patent/GB1071108A/en
Publication of CH404841A publication Critical patent/CH404841A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH1193763A 1963-09-27 1963-09-27 Turbomachinery with adjustable blades CH404841A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CH1193763A CH404841A (en) 1963-09-27 1963-09-27 Turbomachinery with adjustable blades
GB3915564A GB1071108A (en) 1963-09-27 1964-09-25 Improvements in and relating to turbines and compressors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1193763A CH404841A (en) 1963-09-27 1963-09-27 Turbomachinery with adjustable blades

Publications (1)

Publication Number Publication Date
CH404841A true CH404841A (en) 1965-12-31

Family

ID=4378305

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1193763A CH404841A (en) 1963-09-27 1963-09-27 Turbomachinery with adjustable blades

Country Status (2)

Country Link
CH (1) CH404841A (en)
GB (1) GB1071108A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8297918B2 (en) * 2009-01-06 2012-10-30 General Electric Company Variable position guide vane actuation system and method
FR3082896B1 (en) 2018-06-22 2021-06-04 Safran Aircraft Engines KIT FOR THE CONTROL OF VARIABLE TIMING BLADES

Also Published As

Publication number Publication date
GB1071108A (en) 1967-06-07

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