FR3081915B1 - Aube de turboreacteur comportant des lechettes prolongeant les extremites de son talon - Google Patents

Aube de turboreacteur comportant des lechettes prolongeant les extremites de son talon Download PDF

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Publication number
FR3081915B1
FR3081915B1 FR1854626A FR1854626A FR3081915B1 FR 3081915 B1 FR3081915 B1 FR 3081915B1 FR 1854626 A FR1854626 A FR 1854626A FR 1854626 A FR1854626 A FR 1854626A FR 3081915 B1 FR3081915 B1 FR 3081915B1
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FR
France
Prior art keywords
heel
extending
lechettes
turboreactor
dawn
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
FR1854626A
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English (en)
Other versions
FR3081915A1 (fr
Inventor
Quentin Bruno Guy Andre Emile Lievoux
Pragash Douglas
Vijeay Patel
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 FR1854626A priority Critical patent/FR3081915B1/fr
Publication of FR3081915A1 publication Critical patent/FR3081915A1/fr
Application granted granted Critical
Publication of FR3081915B1 publication Critical patent/FR3081915B1/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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/284—Selection of ceramic materials
    • 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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6033—Ceramic matrix composites [CMC]

Abstract

L'invention a pour objet une aube de turbine, issue de fonderie, comportant une pale (14) s'étendant selon une direction d'envergure (EV) terminée par un talon (16) incluant une plateforme (17) portant au moins une léchette (18, 19) ayant un bord radialement externe destiné à coopérer avec un élément abradable (21). Selon l'invention, la léchette (18, 19) s'étend dans le prolongement de la plateforme (17) en formant un angle (A, B) par rapport à cette plateforme (17).
FR1854626A 2018-05-30 2018-05-30 Aube de turboreacteur comportant des lechettes prolongeant les extremites de son talon Active FR3081915B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1854626A FR3081915B1 (fr) 2018-05-30 2018-05-30 Aube de turboreacteur comportant des lechettes prolongeant les extremites de son talon

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1854626A FR3081915B1 (fr) 2018-05-30 2018-05-30 Aube de turboreacteur comportant des lechettes prolongeant les extremites de son talon
FR1854626 2018-05-30

Publications (2)

Publication Number Publication Date
FR3081915A1 FR3081915A1 (fr) 2019-12-06
FR3081915B1 true FR3081915B1 (fr) 2020-08-14

Family

ID=62952132

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1854626A Active FR3081915B1 (fr) 2018-05-30 2018-05-30 Aube de turboreacteur comportant des lechettes prolongeant les extremites de son talon

Country Status (1)

Country Link
FR (1) FR3081915B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3127984B1 (fr) * 2021-10-07 2023-10-06 Safran Aircraft Engines Aube de turbine de turbomachine avec un effort de contact de prétorsion en fonctionnement auto-généré

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2961845B1 (fr) * 2010-06-28 2013-06-28 Snecma Propulsion Solide Aube de turbomachine a geometrie complementaire paire/impaire et son procede de fabrication
FR2977909B1 (fr) * 2011-07-12 2016-07-15 Snecma Aube de rotor pour une turbomachine
FR3002870B1 (fr) * 2013-03-07 2015-03-06 Snecma Procede de fabrication d'une aube de rotor pour une turbomachine
GB201519869D0 (en) * 2015-11-11 2015-12-23 Rolls Royce Plc Shrouded turbine blade

Also Published As

Publication number Publication date
FR3081915A1 (fr) 2019-12-06

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