FR2136773A5 - - Google Patents

Info

Publication number
FR2136773A5
FR2136773A5 FR7215207A FR7215207A FR2136773A5 FR 2136773 A5 FR2136773 A5 FR 2136773A5 FR 7215207 A FR7215207 A FR 7215207A FR 7215207 A FR7215207 A FR 7215207A FR 2136773 A5 FR2136773 A5 FR 2136773A5
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
FR7215207A
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 FR2136773A5 publication Critical patent/FR2136773A5/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
FR7215207A 1971-05-03 1972-04-28 Expired FR2136773A5 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2121707A DE2121707C3 (de) 1971-05-03 1971-05-03 Leitschaufelkranz

Publications (1)

Publication Number Publication Date
FR2136773A5 true FR2136773A5 (de) 1972-12-22

Family

ID=5806680

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7215207A Expired FR2136773A5 (de) 1971-05-03 1972-04-28

Country Status (9)

Country Link
US (1) US3824034A (de)
JP (1) JPS5218850B1 (de)
AT (1) AT311737B (de)
CH (1) CH538045A (de)
DE (1) DE2121707C3 (de)
ES (1) ES402257A1 (de)
FR (1) FR2136773A5 (de)
GB (1) GB1344221A (de)
IT (1) IT952754B (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010023205A1 (fr) * 2008-08-26 2010-03-04 Snecma Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe
WO2017089677A1 (fr) 2015-11-27 2017-06-01 Safran Aircraft Engines Module de turbomachine ou de banc d'essai de chambre de combustion

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1385666A (en) * 1973-07-06 1975-02-26 Rolls Royce Sealing of vaned assemblies of gas turbine engines
US4194869A (en) * 1978-06-29 1980-03-25 United Technologies Corporation Stator vane cluster
CH664191A5 (de) * 1984-01-09 1988-02-15 Bbc Brown Boveri & Cie Von aussen zustellbare axialfixierung eines schaufeltraegers in einer turbine.
US4566851A (en) * 1984-05-11 1986-01-28 United Technologies Corporation First stage turbine vane support structure
US4643636A (en) * 1985-07-22 1987-02-17 Avco Corporation Ceramic nozzle assembly for gas turbine engine
US4721434A (en) * 1986-12-03 1988-01-26 United Technologies Corporation Damping means for a stator
FR2624914B1 (fr) * 1987-12-16 1990-04-20 Snecma Dispositif de fixation a vis d'une piece de revolution sur une bride annulaire de turbomachine
US4890978A (en) * 1988-10-19 1990-01-02 Westinghouse Electric Corp. Method and apparatus for vane segment support and alignment in combustion turbines
US5149250A (en) * 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
SE500743C2 (sv) * 1992-04-01 1994-08-22 Abb Carbon Ab Sätt och anordning för montering av axialströmningsmaskin
US5392513A (en) * 1993-12-21 1995-02-28 General Electric Co. Steampath and process of retrofitting a nozzle thereof
US5618161A (en) * 1995-10-17 1997-04-08 Westinghouse Electric Corporation Apparatus for restraining motion of a turbo-machine stationary vane
US6234750B1 (en) * 1999-03-12 2001-05-22 General Electric Company Interlocked compressor stator
DE10161292A1 (de) 2001-12-13 2003-06-26 Rolls Royce Deutschland Lagerring zur Lagerung von Schaufelfüßen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine
JP4247214B2 (ja) * 2004-10-29 2009-04-02 三菱重工業株式会社 排気タービン過給機
EP1724443A1 (de) * 2005-05-20 2006-11-22 ABB Turbo Systems AG Düsenring
US8328512B2 (en) * 2009-06-05 2012-12-11 United Technologies Corporation Inner diameter shroud assembly for variable inlet guide vane structure in a gas turbine engine
DE102010064047A1 (de) * 2010-12-23 2012-06-28 Man Diesel & Turbo Se Strömungsmaschine
US9181855B2 (en) * 2013-01-31 2015-11-10 Electro-Motive Diesel, Inc. Turbocharger with axial turbine stage
DE102013017713B4 (de) 2013-10-24 2022-10-27 Man Energy Solutions Se Turbomaschine
US10294808B2 (en) * 2016-04-21 2019-05-21 United Technologies Corporation Fastener retention mechanism

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2905434A (en) * 1954-07-08 1959-09-22 Westinghouse Electric Corp Turbine apparatus
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US3542483A (en) * 1968-07-17 1970-11-24 Westinghouse Electric Corp Turbine stator structure

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010023205A1 (fr) * 2008-08-26 2010-03-04 Snecma Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe
FR2935428A1 (fr) * 2008-08-26 2010-03-05 Snecma Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe
CN102132011A (zh) * 2008-08-26 2011-07-20 斯奈克玛 涡轮发动机的轻质固定翼片组件和包括至少一个这种固定翼片组件的涡轮发动机
US8757966B2 (en) 2008-08-26 2014-06-24 Snecma Stationary vane assembly for a turbine engine having a reduced weight, and turbine engine comprising at least one such stationary vane assembly
CN102132011B (zh) * 2008-08-26 2014-11-05 斯奈克玛 涡轮发动机的轻质固定翼片组件和包括至少一个这种固定翼片组件的涡轮发动机
WO2017089677A1 (fr) 2015-11-27 2017-06-01 Safran Aircraft Engines Module de turbomachine ou de banc d'essai de chambre de combustion
FR3044411A1 (fr) * 2015-11-27 2017-06-02 Snecma Module de turbumachine ou de banc d'essai de chambre de combustion
US10914196B2 (en) 2015-11-27 2021-02-09 Safran Aircraft Engines Module of a turbomachine or of a combustion chamber test bench

Also Published As

Publication number Publication date
GB1344221A (en) 1974-01-16
CH538045A (de) 1973-06-15
DE2121707A1 (de) 1972-11-16
DE2121707C3 (de) 1974-06-20
DE2121707B2 (de) 1973-11-22
AT311737B (de) 1973-11-26
JPS5218850B1 (de) 1977-05-24
IT952754B (it) 1973-07-30
ES402257A1 (es) 1975-11-01
US3824034A (en) 1974-07-16

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Legal Events

Date Code Title Description
ST Notification of lapse