FR2606071B1 - Etage de stator et compresseur de turbomachine le comportant - Google Patents

Etage de stator et compresseur de turbomachine le comportant

Info

Publication number
FR2606071B1
FR2606071B1 FR8615036A FR8615036A FR2606071B1 FR 2606071 B1 FR2606071 B1 FR 2606071B1 FR 8615036 A FR8615036 A FR 8615036A FR 8615036 A FR8615036 A FR 8615036A FR 2606071 B1 FR2606071 B1 FR 2606071B1
Authority
FR
France
Prior art keywords
same
stator stage
turbomachine compressor
turbomachine
compressor
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 - Lifetime
Application number
FR8615036A
Other languages
English (en)
Other versions
FR2606071A1 (fr
Inventor
Jacques Marie Pierre Stenneler
Jean Marc Surdi
Patrick Louis Eugene Girault
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR8615036A priority Critical patent/FR2606071B1/fr
Publication of FR2606071A1 publication Critical patent/FR2606071A1/fr
Application granted granted Critical
Publication of FR2606071B1 publication Critical patent/FR2606071B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8615036A 1986-10-29 1986-10-29 Etage de stator et compresseur de turbomachine le comportant Expired - Lifetime FR2606071B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8615036A FR2606071B1 (fr) 1986-10-29 1986-10-29 Etage de stator et compresseur de turbomachine le comportant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8615036A FR2606071B1 (fr) 1986-10-29 1986-10-29 Etage de stator et compresseur de turbomachine le comportant

Publications (2)

Publication Number Publication Date
FR2606071A1 FR2606071A1 (fr) 1988-05-06
FR2606071B1 true FR2606071B1 (fr) 1990-11-30

Family

ID=9340313

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8615036A Expired - Lifetime FR2606071B1 (fr) 1986-10-29 1986-10-29 Etage de stator et compresseur de turbomachine le comportant

Country Status (1)

Country Link
FR (1) FR2606071B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5411370A (en) * 1994-08-01 1995-05-02 United Technologies Corporation Vibration damping shroud for a turbomachine vane
US6543995B1 (en) * 1999-08-09 2003-04-08 United Technologies Corporation Stator vane and stator assembly for a rotary machine
GB2427900B (en) * 2005-07-02 2007-10-10 Rolls Royce Plc Vane support in a gas turbine engine
US8206100B2 (en) * 2008-12-31 2012-06-26 General Electric Company Stator assembly for a gas turbine engine
US8966756B2 (en) * 2011-01-20 2015-03-03 United Technologies Corporation Gas turbine engine stator vane assembly
FR3021690B1 (fr) * 2014-05-28 2016-07-29 Snecma Aube directrice de sortie comprenant au moins une plateforme surmoulee

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE498668A (fr) *
FR954577A (fr) * 1947-09-02 1950-01-03
US2749026A (en) * 1951-02-27 1956-06-05 United Aircraft Corp Stator construction for compressors
GB722458A (en) * 1952-07-14 1955-01-26 Bristol Aeroplane Co Ltd Improvements in or relating to the manufacture of blades for use in axial flow compressors or the like
US2857093A (en) * 1954-12-02 1958-10-21 Cincinnati Testing & Res Lab Stator casing and blade assembly
DE1213423B (de) * 1960-06-04 1966-03-31 Maschf Augsburg Nuernberg Ag Befestigung der Schaufeln eines Leitschaufel-kranzes einer Stroemungsmaschine am Leitschaufeltraeger mittels gummielastischer Elemente
GB1053846A (fr) * 1962-10-10
GB991357A (en) * 1963-12-04 1965-05-05 Rolls Royce Axial fluid flow machine such as a compressor or turbine
GB995228A (en) * 1964-05-08 1965-06-16 Rolls Royce Bladed structure, for example, for a gas turbine engine compressor
GB1054608A (fr) * 1965-09-16
US3442442A (en) * 1966-12-02 1969-05-06 Gen Electric Mounting of blades in an axial flow compressor
GB1158238A (en) * 1968-06-27 1969-07-16 Rolls Royce Blade Assembly for a Fluid Flow Machine.
US3836282A (en) * 1973-03-28 1974-09-17 United Aircraft Corp Stator vane support and construction thereof
FR2330276A5 (fr) * 1973-12-05 1977-05-27 United Aircraft Corp Amortisseur pour aubes de turbine
GB2115883B (en) * 1982-02-26 1986-04-30 Gen Electric Turbomachine airfoil mounting assembly
FR2568953B1 (fr) * 1984-08-08 1989-02-10 Ratier Figeac Soc Aube fixe pour reacteurs

Also Published As

Publication number Publication date
FR2606071A1 (fr) 1988-05-06

Similar Documents

Publication Publication Date Title
DE3484822D1 (de) Verdichter und turbolader.
BR9001081A (pt) Compressor centrifugo
KR920701673A (ko) 스크로울 압축기
IT8948144A0 (it) Compressore con albero assialmente bilanciato
DE59006232D1 (de) Getriebe-Turboverdichter.
KR900010238A (ko) 스크롤 압축기
IT8767004A0 (it) Turbomacchina particoalrmente compressore centrifugo
BR8900003A (pt) Conjunto de compressor
BR8806951A (pt) Conjunto de compressor
DK612589D0 (da) Kompressor
IT1237846B (it) Girante di compressore
DK331989D0 (da) Kompressor
DE69002595D1 (de) Spiralverdichter und montageverfahren dafuer.
BR8906323A (pt) Conjunto compressor
BR8703244A (pt) Compressor e arranjo de compressor e gerador eletrico
DE68906667D1 (de) Keramischer turbokompressorrotor.
DK334387A (da) Kompressorsmoeresystem
DK319789A (da) Aksialt sammentrykkelig spole
DE3762147D1 (de) Gekapselter verdichter.
FR2606071B1 (fr) Etage de stator et compresseur de turbomachine le comportant
KR880019935U (ko) 베인형 압축기
KR920701674A (ko) 스크로울 압축기
BR9003818A (pt) Compressor de multiplos estagios
DE3765172D1 (de) Gasverdichter.
DE3773723D1 (de) Gasverdichter.

Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
CD Change of name or company name
ST Notification of lapse

Effective date: 20060630