FR2896019B1 - Redresseur de compresseur de turbomachine - Google Patents

Redresseur de compresseur de turbomachine

Info

Publication number
FR2896019B1
FR2896019B1 FR0650110A FR0650110A FR2896019B1 FR 2896019 B1 FR2896019 B1 FR 2896019B1 FR 0650110 A FR0650110 A FR 0650110A FR 0650110 A FR0650110 A FR 0650110A FR 2896019 B1 FR2896019 B1 FR 2896019B1
Authority
FR
France
Prior art keywords
turbomachine compressor
compressor rectifier
rectifier
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.)
Active
Application number
FR0650110A
Other languages
English (en)
Other versions
FR2896019A1 (fr
Inventor
Guy Guerin
Jean Marc Sasseigne
Bernard Sontot
Guy Vieillefond
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 FR0650110A priority Critical patent/FR2896019B1/fr
Publication of FR2896019A1 publication Critical patent/FR2896019A1/fr
Application granted granted Critical
Publication of FR2896019B1 publication Critical patent/FR2896019B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00Manufacture
    • F05B2230/20Manufacture essentially without removing material
    • F05B2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05B2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • F05B2230/237Brazing

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0650110A 2006-01-12 2006-01-12 Redresseur de compresseur de turbomachine Active FR2896019B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0650110A FR2896019B1 (fr) 2006-01-12 2006-01-12 Redresseur de compresseur de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0650110A FR2896019B1 (fr) 2006-01-12 2006-01-12 Redresseur de compresseur de turbomachine

Publications (2)

Publication Number Publication Date
FR2896019A1 FR2896019A1 (fr) 2007-07-13
FR2896019B1 true FR2896019B1 (fr) 2011-11-25

Family

ID=37199083

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0650110A Active FR2896019B1 (fr) 2006-01-12 2006-01-12 Redresseur de compresseur de turbomachine

Country Status (1)

Country Link
FR (1) FR2896019B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106425142A (zh) * 2016-09-30 2017-02-22 中国南方航空工业(集团)有限公司 一种航空发动机轴向扩压器焊接方法

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2336572B1 (fr) * 2009-12-14 2012-07-25 Techspace Aero S.A. Virole en deux parties pour étage à aubes d'un compresseur axial
FR2960604B1 (fr) 2010-05-26 2013-09-20 Snecma Ensemble a aubes de compresseur de turbomachine
FR2976634B1 (fr) 2011-06-14 2013-07-05 Snecma Element de turbomachine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1304001A (fr) * 1969-02-10 1973-01-24
US5332360A (en) * 1993-09-08 1994-07-26 General Electric Company Stator vane having reinforced braze joint
FR2860740B1 (fr) * 2003-10-10 2007-03-02 Snecma Moteurs Procede de brasage d'un redresseur de compresseur de turbomachine.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106425142A (zh) * 2016-09-30 2017-02-22 中国南方航空工业(集团)有限公司 一种航空发动机轴向扩压器焊接方法
CN106425142B (zh) * 2016-09-30 2019-04-16 中国南方航空工业(集团)有限公司 一种航空发动机轴向扩压器焊接方法

Also Published As

Publication number Publication date
FR2896019A1 (fr) 2007-07-13

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