FR3030613B1 - Aube mobile pour organe de turbomachine comprenant une nervure de rigidification - Google Patents

Aube mobile pour organe de turbomachine comprenant une nervure de rigidification Download PDF

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Publication number
FR3030613B1
FR3030613B1 FR1462814A FR1462814A FR3030613B1 FR 3030613 B1 FR3030613 B1 FR 3030613B1 FR 1462814 A FR1462814 A FR 1462814A FR 1462814 A FR1462814 A FR 1462814A FR 3030613 B1 FR3030613 B1 FR 3030613B1
Authority
FR
France
Prior art keywords
platform
rib
blade
rigidification
body including
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
FR1462814A
Other languages
English (en)
Other versions
FR3030613A1 (fr
Inventor
Peter Jeanty
Vincent Francois Boulay
Christophe Damour
Raphael Dupeyre
Jonathan Yvetot
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
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1462814A priority Critical patent/FR3030613B1/fr
Publication of FR3030613A1 publication Critical patent/FR3030613A1/fr
Application granted granted Critical
Publication of FR3030613B1 publication Critical patent/FR3030613B1/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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • 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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • 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
    • 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
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/11—Two-dimensional triangular

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Il est proposé une aube (1) mobile pour organe de turbomachine, l'aube (1) comprenant : - une pale (4), - un pied comprenant : ○ une plate-forme (2) de support depuis laquelle s'étend radialement la pale (4), et ○ une échasse (3) s'étendant radialement depuis une portion de surface (20) de la plate-forme (2) vers un axe de rotation (X) de l'aube (1), la plate-forme comportant en outre une portion de surface libre disposée à une extrémité de la plateforme (2) en regard de l'axe de rotation de l'aube (X), l'aube (1) étant caractérisée en ce que le pied comprend en outre une nervure (5) de rigidification de la plateforme (2) s'étendant entre la portion de surface libre (21) de la plate-forme (2) et l'échasse (3).
FR1462814A 2014-12-18 2014-12-18 Aube mobile pour organe de turbomachine comprenant une nervure de rigidification Active FR3030613B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1462814A FR3030613B1 (fr) 2014-12-18 2014-12-18 Aube mobile pour organe de turbomachine comprenant une nervure de rigidification

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1462814A FR3030613B1 (fr) 2014-12-18 2014-12-18 Aube mobile pour organe de turbomachine comprenant une nervure de rigidification

Publications (2)

Publication Number Publication Date
FR3030613A1 FR3030613A1 (fr) 2016-06-24
FR3030613B1 true FR3030613B1 (fr) 2021-05-21

Family

ID=52477982

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1462814A Active FR3030613B1 (fr) 2014-12-18 2014-12-18 Aube mobile pour organe de turbomachine comprenant une nervure de rigidification

Country Status (1)

Country Link
FR (1) FR3030613B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU174793U1 (ru) * 2016-09-13 2017-11-02 Общество с ограниченной ответственностью "Инжиниринговый центр "Газотурбинные технологии" Рабочая лопатка турбомашины
FR3090032B1 (fr) * 2018-12-12 2021-01-29 Safran Aircraft Engines Aube pour roue de turbomachine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6158962A (en) * 1999-04-30 2000-12-12 General Electric Company Turbine blade with ribbed platform
FR2825748B1 (fr) * 2001-06-07 2003-11-07 Snecma Moteurs Agencement de rotor de turbomachine a deux disques aubages separes par une entretoise
JP2011089438A (ja) * 2009-10-21 2011-05-06 Toshiba Corp 蒸気タービンおよび蒸気タービンロータ並びに蒸気タービン用動翼
FR2995343B1 (fr) * 2012-09-11 2018-05-25 Safran Aircraft Engines Aube de turbine, turbine, et procede de fabrication
FR3003893B1 (fr) * 2013-04-02 2017-12-29 Snecma Aube de turbomachine

Also Published As

Publication number Publication date
FR3030613A1 (fr) 2016-06-24

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