FR3073907B1 - Organe de retention pour plateforme de turbomachine - Google Patents

Organe de retention pour plateforme de turbomachine Download PDF

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Publication number
FR3073907B1
FR3073907B1 FR1760858A FR1760858A FR3073907B1 FR 3073907 B1 FR3073907 B1 FR 3073907B1 FR 1760858 A FR1760858 A FR 1760858A FR 1760858 A FR1760858 A FR 1760858A FR 3073907 B1 FR3073907 B1 FR 3073907B1
Authority
FR
France
Prior art keywords
platform
turbomachine
retaining body
retention
disc
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
FR1760858A
Other languages
English (en)
Other versions
FR3073907A1 (fr
Inventor
Gaillard Thomas Alain De
Alexandre Bernard Marie Boisson
Audrey Myriam Laguerre
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 FR1760858A priority Critical patent/FR3073907B1/fr
Publication of FR3073907A1 publication Critical patent/FR3073907A1/fr
Application granted granted Critical
Publication of FR3073907B1 publication Critical patent/FR3073907B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • 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

Module de turbomachine, comprenant un disque comportant une pluralité de dents (44) aptes à supporter des plateformes (30); au moins une plateforme (30) comportant une surface de rétention radiale (36d) prévue à une extrémité de la plateforme (30); au moins un organe de rétention (10) associé à ladite au moins une plateforme (30), et apte à être fixé au disque ; dans lequel l'organe de rétention (10) comporte une languette de rétention (14) apte à retenir radialement la surface de rétention radiale (36d) de la plateforme (30).
FR1760858A 2017-11-17 2017-11-17 Organe de retention pour plateforme de turbomachine Active FR3073907B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1760858A FR3073907B1 (fr) 2017-11-17 2017-11-17 Organe de retention pour plateforme de turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1760858A FR3073907B1 (fr) 2017-11-17 2017-11-17 Organe de retention pour plateforme de turbomachine
FR1760858 2017-11-17

Publications (2)

Publication Number Publication Date
FR3073907A1 FR3073907A1 (fr) 2019-05-24
FR3073907B1 true FR3073907B1 (fr) 2020-12-11

Family

ID=61132610

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1760858A Active FR3073907B1 (fr) 2017-11-17 2017-11-17 Organe de retention pour plateforme de turbomachine

Country Status (1)

Country Link
FR (1) FR3073907B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20240125242A1 (en) * 2022-10-14 2024-04-18 Rtx Corporation Platform for an airfoil of a gas turbine engine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2639402B1 (fr) * 1988-11-23 1990-12-28 Snecma Disque ailete de rotor de turbomachine
US9399922B2 (en) * 2012-12-31 2016-07-26 General Electric Company Non-integral fan blade platform
US10145268B2 (en) * 2013-03-15 2018-12-04 United Technologies Corporation Injection molded composite fan platform

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20240125242A1 (en) * 2022-10-14 2024-04-18 Rtx Corporation Platform for an airfoil of a gas turbine engine

Also Published As

Publication number Publication date
FR3073907A1 (fr) 2019-05-24

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