IT1090233B - Perfezionamento negli impianti a turbina a gas - Google Patents

Perfezionamento negli impianti a turbina a gas

Info

Publication number
IT1090233B
IT1090233B IT51091/77A IT5109177A IT1090233B IT 1090233 B IT1090233 B IT 1090233B IT 51091/77 A IT51091/77 A IT 51091/77A IT 5109177 A IT5109177 A IT 5109177A IT 1090233 B IT1090233 B IT 1090233B
Authority
IT
Italy
Prior art keywords
improvement
gas turbine
turbine plants
plants
gas
Prior art date
Application number
IT51091/77A
Other languages
English (en)
Original Assignee
Kronogard Sven Olof
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 Kronogard Sven Olof filed Critical Kronogard Sven Olof
Application granted granted Critical
Publication of IT1090233B publication Critical patent/IT1090233B/it

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
    • 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

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)
IT51091/77A 1976-09-24 1977-09-20 Perfezionamento negli impianti a turbina a gas IT1090233B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7610576A SE406210B (sv) 1976-09-24 1976-09-24 For en gasturbin avsedd ledapparat

Publications (1)

Publication Number Publication Date
IT1090233B true IT1090233B (it) 1985-06-26

Family

ID=20328941

Family Applications (1)

Application Number Title Priority Date Filing Date
IT51091/77A IT1090233B (it) 1976-09-24 1977-09-20 Perfezionamento negli impianti a turbina a gas

Country Status (7)

Country Link
US (1) US4183209A (it)
JP (1) JPS5352813A (it)
DE (1) DE2743110A1 (it)
FR (1) FR2365693A1 (it)
GB (1) GB1544388A (it)
IT (1) IT1090233B (it)
SE (1) SE406210B (it)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6715983B2 (en) * 2001-09-27 2004-04-06 General Electric Company Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
DE102009041027B4 (de) 2009-09-14 2012-02-09 Continental Automotive Gmbh Leitschaufel für einen Turbolader, Leitschaufelanordnung, Turbolader, Kraftfahrzeug und Verfahren
US9617868B2 (en) 2013-02-26 2017-04-11 Rolls-Royce North American Technologies, Inc. Gas turbine engine variable geometry flow component
US9500122B2 (en) * 2013-06-28 2016-11-22 General Electric Company Variable geometry nozzle and associated method of operation
DE102014213633A1 (de) * 2014-07-14 2016-01-14 Siemens Aktiengesellschaft Verstellbarer Düsenring
US10811884B2 (en) * 2018-03-16 2020-10-20 Uop Llc Consolidation and use of power recovered from a turbine in a process unit
FR3142776A1 (fr) * 2022-12-06 2024-06-07 Safran Aircraft Engines Ensemble statorique de turbomachine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR362019A (fr) * 1905-12-22 1907-02-09 Desire Bonnet Marie-Julie-Leonie Ier Distributeur à aubages mobiles pour turbines
AT34044B (de) * 1907-03-26 1908-08-10 August Oswald Pictet Turbinenleitrad mit verstellbaren Schaufeln.
GB908047A (en) * 1960-06-21 1962-10-10 Daimler Benz Ag Improvements relating to adjustable vanes for hydro-dynamic converters
US3167914A (en) * 1961-07-03 1965-02-02 Chrysler Corp Gas turbine engine housing
NL270226A (it) * 1961-10-13
GB1204321A (en) * 1966-10-13 1970-09-03 Turbokonsult Ab Improvements in or relating to gas turbine power plants

Also Published As

Publication number Publication date
GB1544388A (en) 1979-04-19
JPS5352813A (en) 1978-05-13
SE7610576L (sv) 1978-03-25
SE406210B (sv) 1979-01-29
FR2365693A1 (fr) 1978-04-21
US4183209A (en) 1980-01-15
DE2743110A1 (de) 1978-03-30

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