FR3107551B1 - Aube de turbine - Google Patents

Aube de turbine Download PDF

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Publication number
FR3107551B1
FR3107551B1 FR2001707A FR2001707A FR3107551B1 FR 3107551 B1 FR3107551 B1 FR 3107551B1 FR 2001707 A FR2001707 A FR 2001707A FR 2001707 A FR2001707 A FR 2001707A FR 3107551 B1 FR3107551 B1 FR 3107551B1
Authority
FR
France
Prior art keywords
axis
bulb
turbine blade
stilt
called
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
FR2001707A
Other languages
English (en)
Other versions
FR3107551A1 (fr
Inventor
Bruno Marc-Etienne Loisel
Etienne Léon Francois
Quentin Bruno Guy André Emile Lievoux
Alexandre Thanh Nhan Nguyen
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 FR2001707A priority Critical patent/FR3107551B1/fr
Publication of FR3107551A1 publication Critical patent/FR3107551A1/fr
Application granted granted Critical
Publication of FR3107551B1 publication Critical patent/FR3107551B1/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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
    • 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

La présente invention concerne une aube (1) de turbine comprenant successivement selon une direction radiale un bulbe (13) sensiblement axialement rectiligne selon un premier axe longitudinal (X) dit axe bulbe (X), une échasse (14) et une pale (10) présentant un extrados (E) et un intrados (I). L’échasse (14) comprend au moins une face latérale (18) plane orientée selon un deuxième axe longitudinal (X’), dit axe face latérale (X’), sécant de l’axe bulbe (X). Figure pour l’abrégé : Fig. 1
FR2001707A 2020-02-20 2020-02-20 Aube de turbine Active FR3107551B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2001707A FR3107551B1 (fr) 2020-02-20 2020-02-20 Aube de turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2001707A FR3107551B1 (fr) 2020-02-20 2020-02-20 Aube de turbine
FR2001707 2020-02-20

Publications (2)

Publication Number Publication Date
FR3107551A1 FR3107551A1 (fr) 2021-08-27
FR3107551B1 true FR3107551B1 (fr) 2022-08-12

Family

ID=70154782

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2001707A Active FR3107551B1 (fr) 2020-02-20 2020-02-20 Aube de turbine

Country Status (1)

Country Link
FR (1) FR3107551B1 (fr)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004116364A (ja) * 2002-09-25 2004-04-15 Mitsubishi Heavy Ind Ltd 軸流タービンにおける動翼
US7097429B2 (en) * 2004-07-13 2006-08-29 General Electric Company Skirted turbine blade
JP4335771B2 (ja) * 2004-09-16 2009-09-30 株式会社日立製作所 タービン動翼及びタービン設備
DE102005030516A1 (de) * 2005-06-28 2007-01-04 Man Turbo Ag Rotor für eine Turbine sowie Verfahren und Vorrichtung zur Herstellung des Rotors
US8113780B2 (en) * 2008-11-21 2012-02-14 United Technologies Corporation Castings, casting cores, and methods
US20100166561A1 (en) * 2008-12-30 2010-07-01 General Electric Company Turbine blade root configurations
FR3082878B1 (fr) * 2018-06-20 2021-06-04 Safran Aircraft Engines Aube de turbomachine

Also Published As

Publication number Publication date
FR3107551A1 (fr) 2021-08-27

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