FR3109604B1 - Roue aubagee a performances d’etancheite et de retention des aubes ameliorees - Google Patents

Roue aubagee a performances d’etancheite et de retention des aubes ameliorees Download PDF

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Publication number
FR3109604B1
FR3109604B1 FR2004178A FR2004178A FR3109604B1 FR 3109604 B1 FR3109604 B1 FR 3109604B1 FR 2004178 A FR2004178 A FR 2004178A FR 2004178 A FR2004178 A FR 2004178A FR 3109604 B1 FR3109604 B1 FR 3109604B1
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FR
France
Prior art keywords
blade
improved sealing
impeller
retention performances
crown
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
FR2004178A
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English (en)
Other versions
FR3109604A1 (fr
Inventor
Pierre-Alain Francis Claude Sebrecht
Lauriane Charlotte Morgane Pucheu
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 FR2004178A priority Critical patent/FR3109604B1/fr
Publication of FR3109604A1 publication Critical patent/FR3109604A1/fr
Application granted granted Critical
Publication of FR3109604B1 publication Critical patent/FR3109604B1/fr
Active legal-status Critical Current
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00Products made by additive manufacturing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/18Two-dimensional patterned
    • F05D2250/182Two-dimensional patterned crenellated, notched

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L’invention concerne un disque (48) de roue aubagée (38) pour turbomachine, s’étendant radialement autour d’un axe (AX) de direction axiale et comprenant en périphérie une pluralité de dents (56) s’étendant radialement et délimitant deux à deux des alvéoles (57) adaptées chacune pour loger un pied (59) d’une aube (49). Les alévoles (57) s’étendent chacune suivant une composante axiale depuis une ouverture (57a) d’introduction du pied (59) de l’aube (49), jusqu’à un fond axial d’alvéole (57b) qui est défini par une couronne (58), cette couronne étant centrée sur l’axe (AX) de direction axiale et formée d’un seul tenant avec les dents (56). Figure pour l’abrégé : Fig . 5
FR2004178A 2020-04-27 2020-04-27 Roue aubagee a performances d’etancheite et de retention des aubes ameliorees Active FR3109604B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2004178A FR3109604B1 (fr) 2020-04-27 2020-04-27 Roue aubagee a performances d’etancheite et de retention des aubes ameliorees

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2004178 2020-04-27
FR2004178A FR3109604B1 (fr) 2020-04-27 2020-04-27 Roue aubagee a performances d’etancheite et de retention des aubes ameliorees

Publications (2)

Publication Number Publication Date
FR3109604A1 FR3109604A1 (fr) 2021-10-29
FR3109604B1 true FR3109604B1 (fr) 2022-08-26

Family

ID=71094601

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2004178A Active FR3109604B1 (fr) 2020-04-27 2020-04-27 Roue aubagee a performances d’etancheite et de retention des aubes ameliorees

Country Status (1)

Country Link
FR (1) FR3109604B1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE794573A (fr) * 1972-02-02 1973-05-16 Gen Electric Dispositif de fixation d'aubes
FR2561307B1 (fr) * 1984-03-14 1986-09-12 Snecma Dispositif de verrouillage d'aubes de soufflantes
FR2905139B1 (fr) 2006-08-25 2012-09-28 Snecma Aube de rotor d'une turbomachine
FR3051827B1 (fr) 2016-05-31 2020-03-06 Safran Aircraft Engines Ensemble rotatif pour turbomachine, equipe de moyens de verrouillage mutuel jonc-flasque d'etancheite
US10428661B2 (en) * 2016-10-26 2019-10-01 Roll-Royce North American Technologies Inc. Turbine wheel assembly with ceramic matrix composite components

Also Published As

Publication number Publication date
FR3109604A1 (fr) 2021-10-29

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