[go: up one dir, main page]

FR2599081B1 - MULTIFLUX TURBOJET BLOWER RECTIFIER - Google Patents

MULTIFLUX TURBOJET BLOWER RECTIFIER

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
French (fr)
Other versions
FR2599081A1 (en
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/en
Publication of FR2599081A1 publication Critical patent/FR2599081A1/en
Application granted granted Critical
Publication of FR2599081B1 publication Critical patent/FR2599081B1/en
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 MULTIFLUX TURBOJET BLOWER RECTIFIER Expired FR2599081B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8607368A FR2599081B1 (en) 1986-05-23 1986-05-23 MULTIFLUX TURBOJET BLOWER RECTIFIER

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8607368A FR2599081B1 (en) 1986-05-23 1986-05-23 MULTIFLUX TURBOJET BLOWER RECTIFIER

Publications (2)

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

Family

ID=9335535

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8607368A Expired FR2599081B1 (en) 1986-05-23 1986-05-23 MULTIFLUX TURBOJET BLOWER RECTIFIER

Country Status (1)

Country Link
FR (1) FR2599081B1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2654463A1 (en) * 1989-11-15 1991-05-17 Snecma TURBOMACHINE STATOR ELEMENT.
US5494404A (en) * 1993-12-22 1996-02-27 Alliedsignal Inc. Insertable stator vane assembly
FR2817283B1 (en) * 2000-11-27 2003-06-13 Alstom Power Nv HYDRAULIC COMPONENT AND METHOD FOR MANUFACTURING SUCH COMPONENT
FR2958980B1 (en) * 2010-04-14 2013-03-15 Snecma RECTIFIER DEVICE FOR TURBOMACHINE
JP6221544B2 (en) * 2013-09-18 2017-11-01 株式会社Ihi Seal for turbofan engine
FR3132126B1 (en) * 2022-01-24 2025-02-21 Safran Aircraft Engines Aircraft engine comprising blades fixed to the casing

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1213423B (en) * 1960-06-04 1966-03-31 Maschf Augsburg Nuernberg Ag Attachment of the vanes of a guide vane ring of a flow machine to the guide vane carrier by means of rubber-elastic elements
US3442442A (en) * 1966-12-02 1969-05-06 Gen Electric Mounting of blades in an axial flow compressor
FR2321616A1 (en) * 1975-08-21 1977-03-18 Snecma Axial flow compressor stator blade fixing - uses U section seal around slot across carrier ring and fitting rectangular blade base
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 (en) 1987-11-27

Similar Documents

Publication Publication Date Title
FR2600379B1 (en) MULTIFLUX TURBOJET BLOWER RECTIFIER
AT399804B (en) SPORTSHOE
DK126388D0 (en) reference
KR880004025U (en) Improvement
BR8904999A (en) FAN SET
ATA290587A (en) ARRANGEMENT ARRANGEMENT
KR870012563U (en) duct
BR8704813A (en) FAN NOZZLE
BR8705932A (en) FAN
FR2599081B1 (en) MULTIFLUX TURBOJET BLOWER RECTIFIER
DD264274A1 (en) SMOKE DUCT
FI882238L (en) FOERBAETTRINGAR I SAMBAND MED ORGANISKA FOERENINGAR
AT386436B (en) SHAFTSYSTEM
ATA48386A (en) CRANEWAY
KR880002655U (en) fan
KR880000938U (en) fan
KR880002020U (en) Improvement
KR870012940U (en) Improvement
SE457329B (en) aircraft
ATA179487A (en) MAISHAECKSLER
BR8603727A (en) FAN
SE8602189D0 (en) FAN UNIT
DK301086D0 (en) FAN UNIT
DK301186D0 (en) FAN UNIT
KR870012456U (en) Blower

Legal Events

Date Code Title Description
ST Notification of lapse