BR112016027014A8 - pá de turbina de turbomotor, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina - Google Patents

pá de turbina de turbomotor, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina

Info

Publication number
BR112016027014A8
BR112016027014A8 BR112016027014A BR112016027014A BR112016027014A8 BR 112016027014 A8 BR112016027014 A8 BR 112016027014A8 BR 112016027014 A BR112016027014 A BR 112016027014A BR 112016027014 A BR112016027014 A BR 112016027014A BR 112016027014 A8 BR112016027014 A8 BR 112016027014A8
Authority
BR
Brazil
Prior art keywords
blade
turbomachinery
turbine
air
root
Prior art date
Application number
BR112016027014A
Other languages
English (en)
Other versions
BR112016027014A2 (pt
BR112016027014B1 (pt
Inventor
Marie Dujol Charlotte
Eneau Patrice
Original Assignee
Safran Aircraft Engines
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 filed Critical Safran Aircraft Engines
Publication of BR112016027014A2 publication Critical patent/BR112016027014A2/pt
Publication of BR112016027014A8 publication Critical patent/BR112016027014A8/pt
Publication of BR112016027014B1 publication Critical patent/BR112016027014B1/pt

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/10—Cores; Manufacture or installation of cores
    • B22C9/103—Multipart cores
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on 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
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • 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
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F05D2230/211—Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
    • 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
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
    • 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
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/123—Fluid guiding means, e.g. vanes related to the pressure side of a stator vane
    • 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
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/124—Fluid guiding means, e.g. vanes related to the suction side of a stator vane
    • 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
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/125—Fluid guiding means, e.g. vanes related to the tip of a stator vane
    • 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
    • F05D2250/70—Shape
    • F05D2250/75—Shape given by its similarity to a letter, e.g. T-shaped
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/204—Heat transfer, e.g. cooling by the use of microcircuits
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

pá de turbina de turbomotor, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina a invenção refere-se a uma pá de turbina (91) que compreende uma raiz (p), uma palheta que se estende em uma direção de envergadura (ev), que termina em uma ponta (s) e que compreende um bordo de ataque e um bordo de fuga e uma parede de pressão lateral e uma parede de sucção lateral, em que a dita palheta compreende adicionalmente: pelo menos um duto a montante (93) configurado para coletar ar na raiz (p) para resfriar o bordo de ataque, descarregando o dito ar através de orifícios que atravessam a parede do bordo de ataque; pelo menos um duto a jusante (96) separado do duto a montante (93) e configurado para coletar ar na raiz (p) para resfriar o bordo de fuga, descarregando o dito ar através de orifícios (97) que atravessam a parede de pressão a montante do bordo de fuga; e uma cavidade lateral interna (101) que percorre a parede de pressão lateral para formar uma proteção térmica que isola o duto a jusante (96).
BR112016027014-2A 2014-05-28 2015-05-26 Pá de turbina de turbomotor, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina BR112016027014B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1454869 2014-05-28
FR1454869A FR3021699B1 (fr) 2014-05-28 2014-05-28 Aube de turbine a refroidissement optimise au niveau de son bord de fuite
PCT/FR2015/051382 WO2015181488A1 (fr) 2014-05-28 2015-05-26 Aube de turbine a refroidissement optimise au niveau de son bord de fuite comprenant des conduits amont et aval et des cavités latérales internes

Publications (3)

Publication Number Publication Date
BR112016027014A2 BR112016027014A2 (pt) 2017-08-15
BR112016027014A8 true BR112016027014A8 (pt) 2021-06-22
BR112016027014B1 BR112016027014B1 (pt) 2022-11-08

Family

ID=51905217

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016027014-2A BR112016027014B1 (pt) 2014-05-28 2015-05-26 Pá de turbina de turbomotor, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina

Country Status (8)

Country Link
US (1) US10662789B2 (pt)
EP (1) EP3149282A1 (pt)
CN (1) CN106470782B (pt)
BR (1) BR112016027014B1 (pt)
CA (1) CA2949920C (pt)
FR (1) FR3021699B1 (pt)
RU (1) RU2688090C2 (pt)
WO (1) WO2015181488A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3021697B1 (fr) * 2014-05-28 2021-09-17 Snecma Aube de turbine a refroidissement optimise
FR3037830B1 (fr) 2015-06-29 2024-02-16 Snecma Ensemble de moulage d'une aube de turbomachine, comprenant une portion en relief de grande section
FR3056631B1 (fr) * 2016-09-29 2018-10-19 Safran Circuit de refroidissement ameliore pour aubes
FR3057906B1 (fr) 2016-10-20 2019-03-15 Safran Aircraft Engines Aube de turbomachine a refroidissement optimise
US10641105B2 (en) 2017-08-08 2020-05-05 United Technologies Corporation Airfoil having forward flowing serpentine flow
US10794195B2 (en) 2017-08-08 2020-10-06 Raytheon Technologies Corporation Airfoil having forward flowing serpentine flow
US11644046B2 (en) * 2018-01-05 2023-05-09 Aurora Flight Sciences Corporation Composite fan blades with integral attachment mechanism
ES2954182T3 (es) * 2018-03-08 2023-11-20 Siemens Gamesa Renewable Energy As Cubierta protectora para proteger un borde de ataque de una pala de turbina eólica
US10753210B2 (en) * 2018-05-02 2020-08-25 Raytheon Technologies Corporation Airfoil having improved cooling scheme
US11015457B2 (en) 2018-10-01 2021-05-25 Raytheon Technologies Corporation Multi-walled airfoil core
FR3090040B1 (fr) * 2018-12-12 2021-06-25 Safran Aube de turbomachine à refroidissement amélioré
DE102020207646A1 (de) * 2020-06-22 2021-12-23 Siemens Aktiengesellschaft Turbinenschaufel und Verfahren zum Bearbeiten einer solchen
US11913353B2 (en) 2021-08-06 2024-02-27 Rtx Corporation Airfoil tip arrangement for gas turbine engine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1587401A (en) * 1973-11-15 1981-04-01 Rolls Royce Hollow cooled vane for a gas turbine engine
US5720431A (en) * 1988-08-24 1998-02-24 United Technologies Corporation Cooled blades for a gas turbine engine
US5820774A (en) 1996-10-28 1998-10-13 United Technologies Corporation Ceramic core for casting a turbine blade
US6168381B1 (en) * 1999-06-29 2001-01-02 General Electric Company Airfoil isolated leading edge cooling
EP1126134A1 (de) * 2000-02-17 2001-08-22 Siemens Aktiengesellschaft Luft- und dampfgekühlte Gasturbinenschaufel
US7217095B2 (en) * 2004-11-09 2007-05-15 United Technologies Corporation Heat transferring cooling features for an airfoil
RU2283432C2 (ru) * 2004-11-23 2006-09-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Охлаждаемая лопатка турбомашины
US7377746B2 (en) * 2005-02-21 2008-05-27 General Electric Company Airfoil cooling circuits and method
EP1882819B1 (en) * 2006-07-18 2010-09-08 United Technologies Corporation Integrated platform, tip, and main body microcircuits for turbine blades
US7625178B2 (en) * 2006-08-30 2009-12-01 Honeywell International Inc. High effectiveness cooled turbine blade
EP1895096A1 (de) * 2006-09-04 2008-03-05 Siemens Aktiengesellschaft Gekühlte Turbinenlaufschaufel
US8177507B2 (en) * 2008-05-14 2012-05-15 United Technologies Corporation Triangular serpentine cooling channels
US8171978B2 (en) 2008-11-21 2012-05-08 United Technologies Corporation Castings, casting cores, and methods
US9011077B2 (en) * 2011-04-20 2015-04-21 Siemens Energy, Inc. Cooled airfoil in a turbine engine
US9551228B2 (en) * 2013-01-09 2017-01-24 United Technologies Corporation Airfoil and method of making

Also Published As

Publication number Publication date
RU2016151765A3 (pt) 2018-11-27
EP3149282A1 (fr) 2017-04-05
US10662789B2 (en) 2020-05-26
RU2016151765A (ru) 2018-06-28
WO2015181488A1 (fr) 2015-12-03
FR3021699B1 (fr) 2019-08-16
US20170191368A1 (en) 2017-07-06
FR3021699A1 (fr) 2015-12-04
RU2688090C2 (ru) 2019-05-17
BR112016027014A2 (pt) 2017-08-15
BR112016027014B1 (pt) 2022-11-08
CA2949920C (en) 2022-07-19
CA2949920A1 (en) 2015-12-03
CN106470782A (zh) 2017-03-01
CN106470782B (zh) 2020-05-08

Similar Documents

Publication Publication Date Title
BR112016027014A8 (pt) pá de turbina de turbomotor, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina
BR112016027042A8 (pt) pá de turbina de turbomáquina, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina
BR112016024618A2 (pt) ?lâmina para uma turbina de turbomáquina de aeronave, turbina de turbomáquina de aeronave e turbomáquina de aeronave?
BR112015001398B8 (pt) Rotor de um turbocompressor de gás de escape
BR112015020506A2 (pt) lâmina de turbina
BR112015028251A2 (pt) aerofólio compósito
WO2014113162A3 (en) Turbine blade with integrated serpentine and axial tip cooling circuits
WO2014028090A3 (en) Blade outer air seal for a gas turbine engine
GB2523961A (en) Compressor blade for gas turbine engine
WO2014058493A3 (en) Suction side turbine blade tip cooling
EP2851511A3 (en) Turbine blades with tip portions having converging cooling holes
BR102016007993A2 (pt) conjunto de pá de rotor, turbina eólica e kit de separação de fluxo de ar
BR112016010173A2 (pt) aerofólios e método de refrigeração
BR112014011838A2 (pt) pá de turbina de gás com seções de ponta deslocadas em direção ao lado de pressão e com canais de resfriamento
BR112016007481A2 (pt) método para fabricar um estágio de uma turbina a vapor, setor para a montagem e estágio para uma turbina a vapor
WO2015057310A3 (en) Platform cooling core for a gas turbine engine rotor blade
ES2721160T3 (es) Grupo de álabes directores para una turbomáquina
MY162384A (en) Turbine Vane
BR112017005345A2 (pt) pá de rotor de turbina eólica
WO2014204542A3 (en) Lightweight blade for gas turbine engine
SA515360834B1 (ar) ريشة تربين
WO2014186005A3 (en) Gas turbine engine component with combined mate face and platform cooling
BR112017000814A2 (pt) ?peça extensora de aeroescudo para uma pá de turbina eólica?
BR112017008587A2 (pt) pá de turbina de turbomáquina, disco de turbina e turbina de alta pressão de turborreator
MX2015009316A (es) Un componente de turbomaquinacion una cavidad de alivio de tension.

Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
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 26/05/2015, OBSERVADAS AS CONDICOES LEGAIS