ES318529A1 - Una turbina - Google Patents

Una turbina

Info

Publication number
ES318529A1
ES318529A1 ES0318529A ES318529A ES318529A1 ES 318529 A1 ES318529 A1 ES 318529A1 ES 0318529 A ES0318529 A ES 0318529A ES 318529 A ES318529 A ES 318529A ES 318529 A1 ES318529 A1 ES 318529A1
Authority
ES
Spain
Prior art keywords
shaped member
screws
limbs
vanes
ring
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
ES0318529A
Other languages
English (en)
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.)
English Electric Co Ltd
Original Assignee
English Electric 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 English Electric Co Ltd filed Critical English Electric Co Ltd
Publication of ES318529A1 publication Critical patent/ES318529A1/es
Expired legal-status Critical Current

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)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
ES0318529A 1964-10-16 1965-10-15 Una turbina Expired ES318529A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4228464A GB1081955A (en) 1964-10-16 1964-10-16 Improvements in or relating to turbines

Publications (1)

Publication Number Publication Date
ES318529A1 true ES318529A1 (es) 1966-06-01

Family

ID=10423742

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0318529A Expired ES318529A1 (es) 1964-10-16 1965-10-15 Una turbina

Country Status (4)

Country Link
CH (1) CH432937A (es)
DE (1) DE1928029U (es)
ES (1) ES318529A1 (es)
GB (1) GB1081955A (es)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4925364A (en) * 1988-12-21 1990-05-15 United Technologies Corporation Adjustable spacer

Also Published As

Publication number Publication date
CH432937A (fr) 1967-03-31
DE1928029U (de) 1965-12-02
GB1081955A (en) 1967-09-06

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