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FR3085412B1 - Secteur de distributeur d'une turbomachine comprenant une encoche anti-rotation a insert d'usure - Google Patents

Secteur de distributeur d'une turbomachine comprenant une encoche anti-rotation a insert d'usure Download PDF

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Publication number
FR3085412B1
FR3085412B1 FR1857866A FR1857866A FR3085412B1 FR 3085412 B1 FR3085412 B1 FR 3085412B1 FR 1857866 A FR1857866 A FR 1857866A FR 1857866 A FR1857866 A FR 1857866A FR 3085412 B1 FR3085412 B1 FR 3085412B1
Authority
FR
France
Prior art keywords
area including
wear insert
notch
turbomachine
rotation notch
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
FR1857866A
Other languages
English (en)
Other versions
FR3085412A1 (fr
Inventor
Somphone Sombounkhanh
Etienne Leon Francois
Thomas Pierre-Henri Paul Gardon
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 FR1857866A priority Critical patent/FR3085412B1/fr
Priority to US16/556,129 priority patent/US11415025B2/en
Publication of FR3085412A1 publication Critical patent/FR3085412A1/fr
Application granted granted Critical
Publication of FR3085412B1 publication Critical patent/FR3085412B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • 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
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position

Landscapes

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

Abstract

L'invention concerne un secteur de distributeur d'une turbine d'une turbomachine, comprenant une plateforme externe (14) comprenant un crochet cylindrique (15) aval adapté pour venir en prise avec un carter de la turbomachine, le crochet (15) comprenant une partie (19) dans laquelle est formée une encoche (17) anti-rotation en forme de U comprenant un fond (171) et deux parois latérales (172, 173) s'étendant depuis ledit fond (171), ladite encoche (17) étant recouverte au moins partiellement d'un insert d'usure inséré dans ladite encoche (17), l'insert étant amovible.
FR1857866A 2018-08-31 2018-08-31 Secteur de distributeur d'une turbomachine comprenant une encoche anti-rotation a insert d'usure Active FR3085412B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1857866A FR3085412B1 (fr) 2018-08-31 2018-08-31 Secteur de distributeur d'une turbomachine comprenant une encoche anti-rotation a insert d'usure
US16/556,129 US11415025B2 (en) 2018-08-31 2019-08-29 Distributor sector of a turbomachine comprising an anti-rotation notch with a wear insert

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1857866A FR3085412B1 (fr) 2018-08-31 2018-08-31 Secteur de distributeur d'une turbomachine comprenant une encoche anti-rotation a insert d'usure

Publications (2)

Publication Number Publication Date
FR3085412A1 FR3085412A1 (fr) 2020-03-06
FR3085412B1 true FR3085412B1 (fr) 2020-12-04

Family

ID=63896422

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1857866A Active FR3085412B1 (fr) 2018-08-31 2018-08-31 Secteur de distributeur d'une turbomachine comprenant une encoche anti-rotation a insert d'usure

Country Status (2)

Country Link
US (1) US11415025B2 (fr)
FR (1) FR3085412B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11834967B1 (en) * 2022-05-13 2023-12-05 Rtx Corporation Liner for anti-rotation tab and ceramic component
US12180859B2 (en) * 2023-02-01 2024-12-31 Ge Infrastructure Technology Llc Nozzle segment for use with multiple different turbine engines

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2917276A (en) * 1955-02-28 1959-12-15 Orenda Engines Ltd Segmented stator ring assembly
US4687413A (en) * 1985-07-31 1987-08-18 United Technologies Corporation Gas turbine engine assembly
US7334983B2 (en) * 2005-10-27 2008-02-26 United Technologies Corporation Integrated bladed fluid seal
US20100068050A1 (en) * 2008-09-12 2010-03-18 General Electric Company Gas turbine vane attachment
FR2938872B1 (fr) * 2008-11-26 2015-11-27 Snecma Dispositif anti-usure pour aubes d'un distributeur de turbine d'une turbomachine aeronautique
FR2960591B1 (fr) * 2010-06-01 2012-08-24 Snecma Dispositif pour caler en rotation un segment de distributeur dans un carter de turbomachine ; pion antirotation
US9650905B2 (en) * 2012-08-28 2017-05-16 United Technologies Corporation Singlet vane cluster assembly
US9796055B2 (en) * 2013-02-17 2017-10-24 United Technologies Corporation Turbine case retention hook with insert
FR3003894B1 (fr) * 2013-03-29 2017-10-27 Snecma Organe de verrouillage en rotation pour un distributeur et un anneau d'une turbomachine
US10316861B2 (en) * 2017-01-19 2019-06-11 United Technologies Corporation Two-piece multi-surface wear liner

Also Published As

Publication number Publication date
FR3085412A1 (fr) 2020-03-06
US20200072085A1 (en) 2020-03-05
US11415025B2 (en) 2022-08-16

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