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FR2126041A5 - - Google Patents

Info

Publication number
FR2126041A5
FR2126041A5 FR7205790A FR7205790A FR2126041A5 FR 2126041 A5 FR2126041 A5 FR 2126041A5 FR 7205790 A FR7205790 A FR 7205790A FR 7205790 A FR7205790 A FR 7205790A FR 2126041 A5 FR2126041 A5 FR 2126041A5
Authority
FR
France
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
FR7205790A
Other languages
French (fr)
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Application granted granted Critical
Publication of FR2126041A5 publication Critical patent/FR2126041A5/fr
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
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
FR7205790A 1971-02-19 1972-02-21 Expired FR2126041A5 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19712107949 DE2107949A1 (en) 1971-02-19 1971-02-19 Adjustable guide grille for turbo machines

Publications (1)

Publication Number Publication Date
FR2126041A5 true FR2126041A5 (en) 1972-09-29

Family

ID=5799233

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7205790A Expired FR2126041A5 (en) 1971-02-19 1972-02-21

Country Status (3)

Country Link
DE (1) DE2107949A1 (en)
FR (1) FR2126041A5 (en)
GB (1) GB1378346A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3142776A1 (en) * 2022-12-06 2024-06-07 Safran Aircraft Engines TURBOMACHINE STATOR ASSEMBLY

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3413304A1 (en) * 1984-04-09 1985-10-17 BBC Aktiengesellschaft Brown, Boveri & Cie., Baden, Aargau Adjustable guide vanes for a turbo engine
GB2258272B (en) * 1991-07-27 1994-12-07 Rolls Royce Plc Rotors for turbo machines
GB0002257D0 (en) * 2000-02-02 2000-03-22 Rolls Royce Plc Rotary apparatus for a gas turbine engine
EP2623717A1 (en) * 2012-02-02 2013-08-07 Siemens Aktiengesellschaft Blade ring for an axial turbo engine and method for adjusting the absorption characteristics of the blade ring
US9617868B2 (en) 2013-02-26 2017-04-11 Rolls-Royce North American Technologies, Inc. Gas turbine engine variable geometry flow component
DE102019201039A1 (en) * 2019-01-28 2020-07-30 Psa Automobiles Sa Guide vane grille

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3142776A1 (en) * 2022-12-06 2024-06-07 Safran Aircraft Engines TURBOMACHINE STATOR ASSEMBLY
WO2024121487A1 (en) * 2022-12-06 2024-06-13 Safran Aircraft Engines Stator assembly for turbomachine, and turbomachine

Also Published As

Publication number Publication date
DE2107949A1 (en) 1972-08-31
GB1378346A (en) 1974-12-27

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Legal Events

Date Code Title Description
ST Notification of lapse