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FR2599081B1 - Redresseur de soufflante de turboreacteur multiflux - Google Patents

Redresseur de soufflante de turboreacteur multiflux

Info

Publication number
FR2599081B1
FR2599081B1 FR8607368A FR8607368A FR2599081B1 FR 2599081 B1 FR2599081 B1 FR 2599081B1 FR 8607368 A FR8607368 A FR 8607368A FR 8607368 A FR8607368 A FR 8607368A FR 2599081 B1 FR2599081 B1 FR 2599081B1
Authority
FR
France
Prior art keywords
multiflux
blower rectifier
turbojet blower
turbojet
rectifier
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
FR8607368A
Other languages
English (en)
Other versions
FR2599081A1 (fr
Inventor
Thierry Feuvrier
Alexandre Forestier
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 FR8607368A priority Critical patent/FR2599081B1/fr
Publication of FR2599081A1 publication Critical patent/FR2599081A1/fr
Application granted granted Critical
Publication of FR2599081B1 publication Critical patent/FR2599081B1/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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8607368A 1986-05-23 1986-05-23 Redresseur de soufflante de turboreacteur multiflux Expired FR2599081B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8607368A FR2599081B1 (fr) 1986-05-23 1986-05-23 Redresseur de soufflante de turboreacteur multiflux

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8607368A FR2599081B1 (fr) 1986-05-23 1986-05-23 Redresseur de soufflante de turboreacteur multiflux

Publications (2)

Publication Number Publication Date
FR2599081A1 FR2599081A1 (fr) 1987-11-27
FR2599081B1 true FR2599081B1 (fr) 1988-07-29

Family

ID=9335535

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8607368A Expired FR2599081B1 (fr) 1986-05-23 1986-05-23 Redresseur de soufflante de turboreacteur multiflux

Country Status (1)

Country Link
FR (1) FR2599081B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2654463A1 (fr) * 1989-11-15 1991-05-17 Snecma Element de stator de turbomachine.
US5494404A (en) * 1993-12-22 1996-02-27 Alliedsignal Inc. Insertable stator vane assembly
FR2817283B1 (fr) * 2000-11-27 2003-06-13 Alstom Power Nv Composant hydraulique et procede de fabrication d'un tel composant
FR2958980B1 (fr) * 2010-04-14 2013-03-15 Snecma Dispositif redresseur pour turbomachine
JP6221544B2 (ja) * 2013-09-18 2017-11-01 株式会社Ihi ターボファンエンジンのためのシール
FR3132126B1 (fr) * 2022-01-24 2025-02-21 Safran Aircraft Engines Moteur d'aéronef comprenant des aubes fixées au carter

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US3442442A (en) * 1966-12-02 1969-05-06 Gen Electric Mounting of blades in an axial flow compressor
FR2321616A1 (fr) * 1975-08-21 1977-03-18 Snecma Perfectionnements a la fixation des aubes statoriques d'une soufflante ou d'un compresseur a flux axial
GB2084261A (en) * 1980-09-30 1982-04-07 Rolls Royce Mounting compressor stator blades
GB2115883B (en) * 1982-02-26 1986-04-30 Gen Electric Turbomachine airfoil mounting assembly

Also Published As

Publication number Publication date
FR2599081A1 (fr) 1987-11-27

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Legal Events

Date Code Title Description
ST Notification of lapse