FR3082231B1 - Roue de turbomachine - Google Patents

Roue de turbomachine Download PDF

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Publication number
FR3082231B1
FR3082231B1 FR1855082A FR1855082A FR3082231B1 FR 3082231 B1 FR3082231 B1 FR 3082231B1 FR 1855082 A FR1855082 A FR 1855082A FR 1855082 A FR1855082 A FR 1855082A FR 3082231 B1 FR3082231 B1 FR 3082231B1
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FR
France
Prior art keywords
stilts
platforms
wheel
sealing device
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
FR1855082A
Other languages
English (en)
Other versions
FR3082231A1 (fr
Inventor
Edouard Garreau
Jacques Andre Bassery Josserand
Elsa Maxime
Ba-Phuc TANG
Thomas Tsassis
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 FR1855082A priority Critical patent/FR3082231B1/fr
Publication of FR3082231A1 publication Critical patent/FR3082231A1/fr
Application granted granted Critical
Publication of FR3082231B1 publication Critical patent/FR3082231B1/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
    • 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
    • F05D2240/55—Seals
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L'invention concerne une roue, en particulier roue de turbine, pour turbomachine s'étendant longitudinalement selon un axe comprenant une pluralité d'aubes (14) réparties circonférentiellement autour de l'axe longitudinale présentant des échasses (20) de liaison de pieds (22) à des plates-formes (18), un dispositif d'étanchéité (56) étant monté dans chaque cavité inter-échasse délimitée circonférentiellement entre deux échasses (20) de deux aubes (14) adjacentes, caractérisée en ce que chaque plateforme (18) comprend une ouverture radiale obturée par une paroi d'obturation du dispositif d'étanchéité (56) de manière à ce que les parois des dispositifs d'étanchéité (56) et les plates-formes (18) délimitent ensemble radialement vers l'intérieur une veine annulaire d'air.
FR1855082A 2018-06-11 2018-06-11 Roue de turbomachine Active FR3082231B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1855082A FR3082231B1 (fr) 2018-06-11 2018-06-11 Roue de turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1855082 2018-06-11
FR1855082A FR3082231B1 (fr) 2018-06-11 2018-06-11 Roue de turbomachine

Publications (2)

Publication Number Publication Date
FR3082231A1 FR3082231A1 (fr) 2019-12-13
FR3082231B1 true FR3082231B1 (fr) 2020-05-22

Family

ID=62875037

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1855082A Active FR3082231B1 (fr) 2018-06-11 2018-06-11 Roue de turbomachine

Country Status (1)

Country Link
FR (1) FR3082231B1 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4936749A (en) * 1988-12-21 1990-06-26 General Electric Company Blade-to-blade vibration damper
US8282354B2 (en) * 2008-04-16 2012-10-09 United Technologies Corporation Reduced weight blade for a gas turbine engine
US9840920B2 (en) * 2012-06-15 2017-12-12 General Electric Company Methods and apparatus for sealing a gas turbine engine rotor assembly
FR3027949B1 (fr) * 2014-11-04 2019-07-26 Safran Aircraft Engines Roue de turbine pour une turbomachine

Also Published As

Publication number Publication date
FR3082231A1 (fr) 2019-12-13

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