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FR3086328B1 - Turbine a aubes retenues axialement, pour turbomachine - Google Patents

Turbine a aubes retenues axialement, pour turbomachine Download PDF

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Publication number
FR3086328B1
FR3086328B1 FR1858551A FR1858551A FR3086328B1 FR 3086328 B1 FR3086328 B1 FR 3086328B1 FR 1858551 A FR1858551 A FR 1858551A FR 1858551 A FR1858551 A FR 1858551A FR 3086328 B1 FR3086328 B1 FR 3086328B1
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FR
France
Prior art keywords
vanes
turbomachine
downstream
impeller
blades
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
FR1858551A
Other languages
English (en)
Other versions
FR3086328A1 (fr
Inventor
Nicolas Gael Julien Mallet
Remy Miled Michel Haynau
Bertrand Guillaume Robin Pellaton
Arnaud Lasantha Genilier
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 FR1858551A priority Critical patent/FR3086328B1/fr
Publication of FR3086328A1 publication Critical patent/FR3086328A1/fr
Application granted granted Critical
Publication of FR3086328B1 publication Critical patent/FR3086328B1/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
    • 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
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Abstract

L'invention concerne un rotor de turbomachine comprenant un disque (16), des aubes (14), un anneau labyrinthe (52) en aval des aubes, et un anneau (62) d'étanchéité et de retenue des aubes. D'amont vers l'aval, les pieds (24) d'aubes s'étendent, comme les parois (22a) de fond d'alvéole, suivant une direction oblique (angle α) et, engagé sensiblement radialement à l'axe (X) de rotation dans un espace (64) de retenue axiale, l'anneau (62) définit l'unique moyen, distinct des aubes et du disque, de retenue des aubes vers l'aval.
FR1858551A 2018-09-20 2018-09-20 Turbine a aubes retenues axialement, pour turbomachine Active FR3086328B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1858551A FR3086328B1 (fr) 2018-09-20 2018-09-20 Turbine a aubes retenues axialement, pour turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1858551A FR3086328B1 (fr) 2018-09-20 2018-09-20 Turbine a aubes retenues axialement, pour turbomachine

Publications (2)

Publication Number Publication Date
FR3086328A1 FR3086328A1 (fr) 2020-03-27
FR3086328B1 true FR3086328B1 (fr) 2021-01-01

Family

ID=65201564

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1858551A Active FR3086328B1 (fr) 2018-09-20 2018-09-20 Turbine a aubes retenues axialement, pour turbomachine

Country Status (1)

Country Link
FR (1) FR3086328B1 (fr)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2561307B1 (fr) 1984-03-14 1986-09-12 Snecma Dispositif de verrouillage d'aubes de soufflantes
FR2603333B1 (fr) 1986-09-03 1990-07-20 Snecma Rotor de turbomachine comportant un moyen de verrouillage axial et d'etancheite d'aubes montees dans des brochages axiaux du disque et procede de montage
FR2741666B1 (fr) 1996-10-10 1998-11-06 Snecma Dispositif de fixation axiale d'aubes de rotor de turboreacteur
FR2933442B1 (fr) 2008-07-04 2011-05-27 Snecma Flasque de maintien d'un jonc de retenue, ensemble d'un disque de rotor de turbomachine, d'un jonc de retenue et d'un flasque de maintien et turbomachine comprenant un tel ensemble
FR3020408B1 (fr) * 2014-04-24 2018-04-06 Safran Aircraft Engines Ensemble rotatif pour turbomachine
FR3022944B1 (fr) 2014-06-26 2020-02-14 Safran Aircraft Engines Ensemble rotatif pour turbomachine
FR3057300B1 (fr) * 2016-10-07 2018-10-05 Safran Aircraft Engines Assemblage d'anneau mobile de turbine de turbomachine

Also Published As

Publication number Publication date
FR3086328A1 (fr) 2020-03-27

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