BRPI0801056A2 - processo de moldagem por injeção de metal para aplicações em bi-metálicos e aerofólio - Google Patents

processo de moldagem por injeção de metal para aplicações em bi-metálicos e aerofólio

Info

Publication number
BRPI0801056A2
BRPI0801056A2 BRPI0801056-0A BRPI0801056A BRPI0801056A2 BR PI0801056 A2 BRPI0801056 A2 BR PI0801056A2 BR PI0801056 A BRPI0801056 A BR PI0801056A BR PI0801056 A2 BRPI0801056 A2 BR PI0801056A2
Authority
BR
Brazil
Prior art keywords
airfoil
injection molding
molding process
preform
metal
Prior art date
Application number
BRPI0801056-0A
Other languages
English (en)
Inventor
Thomas Joseph Kelly
Mark Kevin Meyer
Melissa Jane Parks
Stephen Joseph Ferrigno
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BRPI0801056A2 publication Critical patent/BRPI0801056A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/22—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
    • B22F3/225—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip by injection molding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • 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
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
    • F01D5/20—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
    • 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
    • F05D2230/22—Manufacture essentially without removing material by sintering

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Powder Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Processo de moldagem por injeção de metal para aplicações em bi-metálicos e aerofólio. é descrito um método para a produção de um aerofólio (12), incluindo as etapas de fornecer uma primeira preforma (32), a qual é formada por um pó metálico de uma primeira liga, a primeira preforma definindo um corpo de aerofólio apresentando lados curvos de pressão e de sucção (20, 22). Uma cobertura de ponteira (28) é disposta entre os lados de pressão e de sucção em uma extremidade radialmente externa do corpo do aerofólio. Uma ponteira indicadora (30) de altura parcial se estende radialmente para fora a partir da cobertura de ponteira de modo a fornecer uma segunda preforma (34) formada de um pó metálico de uma segunda liga, diferente da primeira liga. A cobertura de ponteira apresenta a forma de uma extensão da ponteira indicadora. A primeira e a segunda preformas são sinterizadas para consolidar os pós metálicos. Também é descrito um aerofólio produzido de acordo com este método.
BRPI0801056-0A 2007-03-26 2008-03-13 processo de moldagem por injeção de metal para aplicações em bi-metálicos e aerofólio BRPI0801056A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/691,032 US20080237403A1 (en) 2007-03-26 2007-03-26 Metal injection molding process for bimetallic applications and airfoil

Publications (1)

Publication Number Publication Date
BRPI0801056A2 true BRPI0801056A2 (pt) 2009-05-12

Family

ID=39327998

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0801056-0A BRPI0801056A2 (pt) 2007-03-26 2008-03-13 processo de moldagem por injeção de metal para aplicações em bi-metálicos e aerofólio

Country Status (7)

Country Link
US (1) US20080237403A1 (pt)
JP (1) JP2008248387A (pt)
BR (1) BRPI0801056A2 (pt)
CA (1) CA2625382A1 (pt)
FR (1) FR2914204A1 (pt)
GB (1) GB2448031A (pt)
SG (2) SG165415A1 (pt)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7726944B2 (en) * 2006-09-20 2010-06-01 United Technologies Corporation Turbine blade with improved durability tip cap
CN102159346A (zh) * 2008-09-17 2011-08-17 库欧聚合物公司 多组分金属注射模制
US20100200189A1 (en) * 2009-02-12 2010-08-12 General Electric Company Method of fabricating turbine airfoils and tip structures therefor
US10226818B2 (en) * 2009-03-20 2019-03-12 Pratt & Whitney Canada Corp. Process for joining powder injection molded parts
US10159574B2 (en) 2009-04-29 2018-12-25 Flextronics Global Services Canada Inc. Method for co-processing components in a metal injection molding process, and components made via the same
EP2366476B1 (en) * 2010-03-10 2014-07-02 General Electric Company Method for Fabricating Turbine Airfoils and Tip Structures Therefor
DE102010061958A1 (de) 2010-11-25 2012-05-31 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung von Triebwerksbauteilen mit geometrisch komplexer Struktur
FR2981590B1 (fr) * 2011-10-21 2014-06-06 Snecma Procede de realisation d'une preforme frittee et d'assemblage de ladite preforme sur une piece
DE102011089260A1 (de) 2011-12-20 2013-06-20 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung eines Bauteils durch Metallpulverspritzgießen
DE102012206087A1 (de) * 2012-04-13 2013-10-17 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung eines Bauteils eines Flugtriebwerks durch Metallpulverspritzgießen
US9470095B2 (en) 2012-04-24 2016-10-18 United Technologies Corporation Airfoil having internal lattice network
US9283621B2 (en) * 2012-06-21 2016-03-15 Deere & Company Method for forming a composite article
US10005125B2 (en) 2012-12-14 2018-06-26 United Technologies Corporation Hybrid turbine blade for improved engine performance or architecture
US9687910B2 (en) 2012-12-14 2017-06-27 United Technologies Corporation Multi-shot casting
CA2900221C (en) * 2013-02-26 2021-01-19 Ted Joseph Freeman Adjustable turbine vanes with sealing device and corresponding method
WO2014152172A1 (en) * 2013-03-15 2014-09-25 United Technologies Corporation Powder metallurgy alloy extrusion
WO2014152183A2 (en) * 2013-03-15 2014-09-25 United Technologies Corporation Powder metallurgy alloy forging
US9903275B2 (en) 2014-02-27 2018-02-27 Pratt & Whitney Canada Corp. Aircraft components with porous portion and methods of making
US9970318B2 (en) 2014-06-25 2018-05-15 Pratt & Whitney Canada Corp. Shroud segment and method of manufacturing
US9517507B2 (en) 2014-07-17 2016-12-13 Pratt & Whitney Canada Corp. Method of shaping green part and manufacturing method using same
US20160263656A1 (en) 2015-03-12 2016-09-15 Pratt & Whitney Canada Corp. Method of forming a component from a green part
WO2017050324A1 (de) * 2015-09-22 2017-03-30 Schaeffler Technologies AG & Co. KG Von einem nocken beaufschlagbarer hebel zur betätigung von gaswechselventilen einer brennkraftmaschine
US10443447B2 (en) 2016-03-14 2019-10-15 General Electric Company Doubler attachment system
DE102016208761A1 (de) * 2016-05-20 2017-11-23 Rolls-Royce Deutschland Ltd & Co Kg Pulverspritzgießverfahren, Pulverspritzgießvorrichtung und Pulverspritzgussteil
CN108248824B (zh) * 2017-12-29 2021-12-21 南京航空航天大学 一种微小型无人机翼面前缘结构、成型模具及其制备方法
US10774653B2 (en) 2018-12-11 2020-09-15 Raytheon Technologies Corporation Composite gas turbine engine component with lattice structure
FR3095975A1 (fr) * 2019-05-16 2020-11-20 Safran Aircraft Engines Procédé de moulage par injection d’une poudre d’une aube de turbomachine
JP7144374B2 (ja) * 2019-07-29 2022-09-29 日立Ｇｅニュークリア・エナジー株式会社 トランジションピースの製造方法およびトランジションピース
FR3099717B1 (fr) * 2019-08-06 2022-06-10 Safran Aircraft Engines Procédé de fabrication d’une pièce métallique
US11618075B2 (en) 2020-11-13 2023-04-04 Garrett Transportation I Inc. Methods for the combined sintering and surface treatment of variable geometry turbocharger vanes
DE102020216193A1 (de) * 2020-12-17 2022-08-11 Rolls-Royce Deutschland Ltd & Co Kg Schaufelbauteil, Verfahren zu dessen Herstellung und Gasturbine

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4250610A (en) * 1979-01-02 1981-02-17 General Electric Company Casting densification method
DE3527367A1 (de) * 1985-07-31 1987-02-12 Mtu Muenchen Gmbh Auf pulvermetallurgischem wege hergestellte bauteile
US5359770A (en) * 1992-09-08 1994-11-01 General Motors Corporation Method for bonding abrasive blade tips to the tip of a gas turbine blade
US6183689B1 (en) * 1997-11-25 2001-02-06 Penn State Research Foundation Process for sintering powder metal components
US6468040B1 (en) * 2000-07-24 2002-10-22 General Electric Company Environmentally resistant squealer tips and method for making
US6558119B2 (en) * 2001-05-29 2003-05-06 General Electric Company Turbine airfoil with separately formed tip and method for manufacture and repair thereof
US20030012677A1 (en) * 2001-07-11 2003-01-16 Senini Robert J. Bi-metallic metal injection molded hand tool and manufacturing method
US6623692B2 (en) * 2001-08-29 2003-09-23 General Electric Company Rhodium-based alloy and articles made therefrom
US20030062660A1 (en) * 2001-10-03 2003-04-03 Beard Bradley D. Process of metal injection molding multiple dissimilar materials to form composite parts
US6532656B1 (en) * 2001-10-10 2003-03-18 General Electric Company Gas turbine engine compressor blade restoration method
US6837687B2 (en) * 2001-12-20 2005-01-04 General Electric Company Foil formed structure for turbine airfoil
DE10343782A1 (de) * 2003-09-22 2005-04-14 Mtu Aero Engines Gmbh Verfahren zur Herstellung von Bauteilen
US20070202000A1 (en) * 2004-08-24 2007-08-30 Gerhard Andrees Method For Manufacturing Components
US7282681B2 (en) * 2005-05-05 2007-10-16 General Electric Company Microwave fabrication of airfoil tips
US7290986B2 (en) * 2005-09-09 2007-11-06 General Electric Company Turbine airfoil with curved squealer tip
US20070081912A1 (en) * 2005-10-11 2007-04-12 Honeywell International, Inc. Method of producing multiple microstructure components

Also Published As

Publication number Publication date
JP2008248387A (ja) 2008-10-16
SG165415A1 (en) 2010-10-28
CA2625382A1 (en) 2008-09-26
GB0804607D0 (en) 2008-04-16
US20080237403A1 (en) 2008-10-02
GB2448031A (en) 2008-10-01
FR2914204A1 (fr) 2008-10-03
SG146552A1 (en) 2008-10-30

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Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 4A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: NAO APRESENTADA A GUIA DE CUMPRIMENTO DE EXIGENCIA. REFERENTE A 4A ANUIDADE.