FR3111677B1 - Compresseur de turbomachine, procédé de montage dudit compresseur - Google Patents

Compresseur de turbomachine, procédé de montage dudit compresseur Download PDF

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Publication number
FR3111677B1
FR3111677B1 FR2006534A FR2006534A FR3111677B1 FR 3111677 B1 FR3111677 B1 FR 3111677B1 FR 2006534 A FR2006534 A FR 2006534A FR 2006534 A FR2006534 A FR 2006534A FR 3111677 B1 FR3111677 B1 FR 3111677B1
Authority
FR
France
Prior art keywords
compressor
notch
sector
blades
assembling
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
FR2006534A
Other languages
English (en)
Other versions
FR3111677A1 (fr
Inventor
Kamel Benderradji
Pauline Anne Freche
Joël Robert Mathieu
Delphine Hermance Maxime Parent
Bruno Alain Mahieux
Alexandre Eric Lefebvre
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR2006534A priority Critical patent/FR3111677B1/fr
Publication of FR3111677A1 publication Critical patent/FR3111677A1/fr
Application granted granted Critical
Publication of FR3111677B1 publication Critical patent/FR3111677B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/64—Mounting; Assembling; Disassembling of axial pumps
    • F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

COMPRESSEUR DE TURBOMACHINE, PROCÉDÉ DE MONTAGE DUDIT COMPRESSEUR L’invention se rapporte à un compresseur de turbomachine comprenant : un redresseur sectorisé comprenant au moins un secteur d’aubes (31), un carter de réception (34), des moyens anti-rotation configurés pour empêcher la rotation dudit au moins un secteur d’aubes (31) par rapport au carter de réception (34), caractérisé en ce que : le carter de réception (34) comprend une première encoche (344), ledit au moins un secteur d’aubes (31) comprend une deuxième encoche (333), la première encoche (344) et la deuxième encoche (333) étant configurées pour être en vis-à-vis l’une de l’autre de manière à former une rainure de verrouillage (36), les moyens anti-rotation comportent un verrou (35) configuré pour être positionné dans la rainure de verrouillage, de manière à former une butée angulaire permettant de bloquer la rotation dudit au moins un secteur d’aubes par rapport au carter de réception. Figure à publier avec l’abrégé : 4
FR2006534A 2020-06-23 2020-06-23 Compresseur de turbomachine, procédé de montage dudit compresseur Active FR3111677B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2006534A FR3111677B1 (fr) 2020-06-23 2020-06-23 Compresseur de turbomachine, procédé de montage dudit compresseur

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2006534 2020-06-23
FR2006534A FR3111677B1 (fr) 2020-06-23 2020-06-23 Compresseur de turbomachine, procédé de montage dudit compresseur

Publications (2)

Publication Number Publication Date
FR3111677A1 FR3111677A1 (fr) 2021-12-24
FR3111677B1 true FR3111677B1 (fr) 2022-09-09

Family

ID=72801619

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2006534A Active FR3111677B1 (fr) 2020-06-23 2020-06-23 Compresseur de turbomachine, procédé de montage dudit compresseur

Country Status (1)

Country Link
FR (1) FR3111677B1 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06129205A (ja) * 1992-10-20 1994-05-10 Mitsubishi Heavy Ind Ltd ガスタービンの静翼
US8133019B2 (en) * 2009-01-21 2012-03-13 General Electric Company Discrete load fins for individual stator vanes
FR2961553B1 (fr) * 2010-06-18 2012-08-31 Snecma Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
FR3009739B1 (fr) * 2013-08-13 2015-09-11 Snecma Amelioration pour le verrouillage de pieces de support d'aubage

Also Published As

Publication number Publication date
FR3111677A1 (fr) 2021-12-24

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