BR112015017351A2 - palheta fixa de distribuição de fluxo em uma turbomáquina, turbomáquina e processo de fabricação de uma palheta fixa de distribuição de fluxo - Google Patents

palheta fixa de distribuição de fluxo em uma turbomáquina, turbomáquina e processo de fabricação de uma palheta fixa de distribuição de fluxo

Info

Publication number
BR112015017351A2
BR112015017351A2 BR112015017351A BR112015017351A BR112015017351A2 BR 112015017351 A2 BR112015017351 A2 BR 112015017351A2 BR 112015017351 A BR112015017351 A BR 112015017351A BR 112015017351 A BR112015017351 A BR 112015017351A BR 112015017351 A2 BR112015017351 A2 BR 112015017351A2
Authority
BR
Brazil
Prior art keywords
flow distribution
vane
fixed flow
turbocharger
distribution vane
Prior art date
Application number
BR112015017351A
Other languages
English (en)
Other versions
BR112015017351B1 (pt
Inventor
Richard Bruno
Chambre Marion
Roullet Romain
Congratel Sébastien
Original Assignee
Snecma
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 filed Critical Snecma
Publication of BR112015017351A2 publication Critical patent/BR112015017351A2/pt
Publication of BR112015017351B1 publication Critical patent/BR112015017351B1/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • F05D2230/237Brazing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/80Platforms for stationary or moving blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

resumo “palheta fixa de distribuição de fluxo em uma turbomáquina, turbomáquina e processo de fabricação de uma palheta fixa de distribuição de fluxo” a presente invenção trata de uma palheta (10) fixa de distribuição de flux em uma turbomáquina, que compreende uma plataforma anular interna (12) e uma pluralidade de palhetas fixas (11) montadas sobre ela, sendo que a plataforma interna compreende uma placa de suporte (121) que forma a base das referidas palhetas, uma divisória anular radial (120) que se estende a partir da placa de suporte para um eixo da palhea, e uma coroa interna (122) aplicada sobre a divisória anular radial, e que apresenta uma superfície interna sobre a qual está disposto um material abrasivo (123), a qual palheta se caracteriza pelo fato de que a coroa interna comporta pelo menos um corte (1223) que delimita uma lingueta (1226), e a lingueta está dobrada para se apoiar sobre a divisória anular radial (120). a presente invenção trata igualmente de um processo de fabricação de tal palheta e de uma turbomáquina que integra tal palheta.
BR112015017351-9A 2013-01-23 2014-01-22 Palheta fixa de distribuição de fluxo em uma turbomáquina, turbomáquina e processo de fabricação de uma palheta fixa de distribuição de fluxo BR112015017351B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1350582 2013-01-23
FR1350582A FR3001252B1 (fr) 2013-01-23 2013-01-23 Aubage fixe de distribution de flux comprenant une plate-forme interne a renforts integres
PCT/FR2014/050113 WO2014114873A1 (fr) 2013-01-23 2014-01-22 Aubage fixe de distribution de flux dans une turbomachine, comprenant une plate-forme interne a renforts intégrés, turbomachine et procédé de fabrication associés

Publications (2)

Publication Number Publication Date
BR112015017351A2 true BR112015017351A2 (pt) 2017-07-11
BR112015017351B1 BR112015017351B1 (pt) 2021-12-14

Family

ID=48521143

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015017351-9A BR112015017351B1 (pt) 2013-01-23 2014-01-22 Palheta fixa de distribuição de fluxo em uma turbomáquina, turbomáquina e processo de fabricação de uma palheta fixa de distribuição de fluxo

Country Status (8)

Country Link
US (1) US10024179B2 (pt)
EP (1) EP2948640B1 (pt)
CN (1) CN104937216B (pt)
BR (1) BR112015017351B1 (pt)
CA (1) CA2898864C (pt)
FR (1) FR3001252B1 (pt)
RU (1) RU2651919C2 (pt)
WO (1) WO2014114873A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3082233B1 (fr) * 2018-06-12 2020-07-17 Safran Aircraft Engines Ensemble de turbine
FR3100838B1 (fr) * 2019-09-13 2021-10-01 Safran Aircraft Engines Anneau d’etancheite de turbomachine
FR3103012B1 (fr) * 2019-11-12 2021-11-19 Safran Aircraft Engines Rangée annulaire sectorisée d’aubes fixes
DE102020200073A1 (de) 2020-01-07 2021-07-08 Siemens Aktiengesellschaft Leitschaufelkranz
FR3113298B1 (fr) * 2020-08-10 2023-09-01 Safran Aircraft Engines Porte-abradable d’un distributeur basse pression comprenant une unique tôle
FR3146931A1 (fr) * 2023-03-23 2024-09-27 Safran Aircraft Engines Ensemble statorique pour une turbomachine d’aéronef

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB807231A (en) * 1955-05-20 1959-01-14 Gen Electric Securing means for blading of compressors or turbines
US3018085A (en) * 1957-03-25 1962-01-23 Gen Motors Corp Floating labyrinth seal
DE3003469C2 (de) * 1980-01-31 1987-03-19 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Verbindung einander rotationssymmetrisch zugeordneter, unterschiedlichen thermischen Einflüssen ausgesetzter Bauteile für Strömungsmaschinen, insbesondere Gasturbinentriebwerke
US4767267A (en) * 1986-12-03 1988-08-30 General Electric Company Seal assembly
RU2171380C2 (ru) * 1999-04-27 2001-07-27 Открытое акционерное общество "Авиадвигатель" Сопловой аппарат турбомашины
FR2928961B1 (fr) * 2008-03-19 2015-11-13 Snecma Distributeur sectorise pour une turbomachine.
FR2930592B1 (fr) * 2008-04-24 2010-04-30 Snecma Distributeur de turbine pour une turbomachine

Also Published As

Publication number Publication date
CA2898864A1 (fr) 2014-07-31
FR3001252B1 (fr) 2015-02-13
EP2948640A1 (fr) 2015-12-02
CN104937216A (zh) 2015-09-23
WO2014114873A1 (fr) 2014-07-31
US10024179B2 (en) 2018-07-17
US20150377044A1 (en) 2015-12-31
FR3001252A1 (fr) 2014-07-25
CA2898864C (fr) 2020-08-25
RU2651919C2 (ru) 2018-04-24
EP2948640B1 (fr) 2017-04-19
RU2015135580A (ru) 2017-03-02
BR112015017351B1 (pt) 2021-12-14
CN104937216B (zh) 2016-08-10

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B09W Correction of the decision to grant [chapter 9.1.4 patent gazette]

Free format text: RETIFICACAO DA PUBLICACAO (9.1)

B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 22/01/2014, OBSERVADAS AS CONDICOES LEGAIS.