ES2176637T3 - Procedimiento de fabricacion de un alabe hueco de una turbomaquina y prensa-horno de efecto multiple utilizada en dicho procedimiento. - Google Patents

Procedimiento de fabricacion de un alabe hueco de una turbomaquina y prensa-horno de efecto multiple utilizada en dicho procedimiento.

Info

Publication number
ES2176637T3
ES2176637T3 ES97401325T ES97401325T ES2176637T3 ES 2176637 T3 ES2176637 T3 ES 2176637T3 ES 97401325 T ES97401325 T ES 97401325T ES 97401325 T ES97401325 T ES 97401325T ES 2176637 T3 ES2176637 T3 ES 2176637T3
Authority
ES
Spain
Prior art keywords
procedure
alabe
turbomaquine
hollow
oven
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.)
Expired - Lifetime
Application number
ES97401325T
Other languages
English (en)
Inventor
Jean-Pierre Serges Bergue
Mathieu Philippe Albert Bichon
Jean-Francois Georges Lacuisse
Alain Georges Henri Lorieux
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
SNECMA Moteurs SA
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 Moteurs SA filed Critical SNECMA Moteurs SA
Application granted granted Critical
Publication of ES2176637T3 publication Critical patent/ES2176637T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J9/00—Forging presses
    • B21J9/02—Special design or construction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/20—Deep-drawing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/20—Deep-drawing
    • B21D22/26—Deep-drawing for making peculiarly, e.g. irregularly, shaped articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K3/00—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
    • B21K3/04—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like blades, e.g. for turbines; Upsetting of blade roots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Forging (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat Treatment Of Articles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Press Drives And Press Lines (AREA)
  • Powder Metallurgy (AREA)

Abstract

UN PROCEDIMIENTO DE FABRICACION DE UN ALABE (9) HUECO DE TURBOMAQUINA DE ALEACION DE TITANIO DEL TIPO TA6V COMPRENDE UNA OPERACION DE FORMACION EN CALIENTE POR CONFORMACION ISOTERMICA BAJO PRENSA (48, 49) A UNA TEMPERATURA COMPRENDIDA ENTRE 700 (GRADOS) Y 940 (GRADOS) C, BAJO LA ACCION DE AL MENOS DOS PUNZONES (46) Y DE UN SUJETADOR (45) QUE BLOQUEA EL ALABE (9) COLOCADO BAJO UN MOLDE DE FORMACION (21) QUE GARANTIZA UNA VELOCIDAD DE DEFORMACION CONTROLADA PARA OBTENER UN ALARGAMIENTO DE LAS FIBRAS, ES DECIR ALARGAMIENTOS DE LAS DIFERENTES FIBRAS DE LA PIEZA CON UNA DISTRIBUCION CONTROLADA A UNA Y OTRA PARTE DE LA FIBRA CENTRAL. UNA PRENSA DE HORNO CON EFECTO MULTIPLE ESTA ESPECIALMENTE CONCEBIDA PARA LA REALIZACION DEL PROCEDIMIENTO.
ES97401325T 1996-06-13 1997-06-12 Procedimiento de fabricacion de un alabe hueco de una turbomaquina y prensa-horno de efecto multiple utilizada en dicho procedimiento. Expired - Lifetime ES2176637T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9607329A FR2749784B1 (fr) 1996-06-13 1996-06-13 Procede de fabrication d'un aube creuse de turbomachine et presse-four a multiple effet utilisee dans sa mise en oeuvre

Publications (1)

Publication Number Publication Date
ES2176637T3 true ES2176637T3 (es) 2002-12-01

Family

ID=9493010

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97401325T Expired - Lifetime ES2176637T3 (es) 1996-06-13 1997-06-12 Procedimiento de fabricacion de un alabe hueco de una turbomaquina y prensa-horno de efecto multiple utilizada en dicho procedimiento.

Country Status (7)

Country Link
US (2) US5933951A (es)
EP (1) EP0812649B1 (es)
JP (1) JP3618964B2 (es)
CA (1) CA2206160C (es)
DE (1) DE69714354T2 (es)
ES (1) ES2176637T3 (es)
FR (1) FR2749784B1 (es)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2749784B1 (fr) * 1996-06-13 1998-07-31 Snecma Procede de fabrication d'un aube creuse de turbomachine et presse-four a multiple effet utilisee dans sa mise en oeuvre
FR2752539B1 (fr) * 1996-08-22 1998-09-18 Snecma Procede de fabrication d'une aube creuse de turbomachine et equipement de vrillage evolutif a chaud utilise
JP3647612B2 (ja) * 1997-07-24 2005-05-18 富士重工業株式会社 航空機の前縁構造及びその製造方法
FR2784616B1 (fr) * 1998-10-15 2000-11-17 Snecma Procede d'obtention de pieces metalliques minces, legeres et rigides
US6223573B1 (en) * 1999-06-25 2001-05-01 General Electric Company Method for precision temperature controlled hot forming
US6138491A (en) * 1999-06-25 2000-10-31 General Electric Company Apparatus and method for low heat transfer rate chill down during forging
US6464129B2 (en) * 2000-12-22 2002-10-15 Triumph Group, Inc. Method of diffusion bonding superalloy components
JP2002210529A (ja) * 2001-01-12 2002-07-30 Mitsubishi Heavy Ind Ltd チタン合金製円筒形状部品の熱間成形方法
FR2820062B1 (fr) * 2001-02-01 2003-03-07 Snecma Moteurs Installation de formage d'une piece et application au formage a chaud
FR2871397B1 (fr) * 2004-06-11 2006-09-22 Snecma Moteurs Sa Installation de conformation d'une aube creuse
FR2874339B1 (fr) * 2004-08-23 2008-12-05 Snecma Moteurs Sa Procede de fabrication de pieces constitutives d'une aube creuse par forage sur presse
DE602006000955T2 (de) * 2005-02-25 2009-05-28 Snecma Verfahren zur mechanischen Charakterisierung eines metallischen Materials
US8062437B2 (en) * 2007-06-01 2011-11-22 Ethicon, Inc. Thermal forming of refractory alloy surgical needles and fixture and apparatus
US20090142221A1 (en) * 2007-11-30 2009-06-04 Honeywell International, Inc. Engine components and methods of forming engine components
GB0820424D0 (en) * 2008-11-10 2008-12-17 Rolls Royce Plc Forming apparatus
FR2970192B1 (fr) 2011-01-10 2013-12-13 Snecma Outillage et procede de forgeage a chaud de toles
FR2978926B1 (fr) * 2011-08-11 2014-05-09 Snecma Dispositif pour la mise en forme d'une tole par matricage
GB201117183D0 (en) * 2011-10-06 2011-11-16 Rolls Royce Plc Method and equipment for shaping a cast component
RU2497621C1 (ru) * 2012-05-10 2013-11-10 Открытое Акционерное Общество "Корпорация Всмпо-Ависма" Способ технологического испытания листов из титановых сплавов при глубокой вытяжке и устройство для его осуществления
ITTV20130031A1 (it) 2013-02-28 2014-08-29 Pietro Rosa T B M S R L Paletta per turbomacchine e relativo metodo di costruzione
ITTV20130029A1 (it) * 2013-02-28 2014-08-29 Pietro Rosa T B M S R L Paletta per turbomacchine e relativo metodo di costruzione
KR101491279B1 (ko) * 2013-07-16 2015-02-06 현대자동차주식회사 자동차용 부품 교정기
CN105436839B (zh) * 2015-12-16 2017-07-28 西北工业大学 航空发动机钛合金宽弦空心风扇叶片的制造方法
JP6922584B2 (ja) * 2017-09-19 2021-08-18 トヨタ自動車株式会社 プレス成形方法及びプレス成形装置
US10913133B2 (en) 2018-07-02 2021-02-09 Raytheon Technologies Corporation Processes and tooling associated with diffusion bonding the periphery of a cavity-back airfoil
CN109808283A (zh) * 2018-12-24 2019-05-28 吉林大学 一种蜂窝夹芯复合板用模具
US11014190B2 (en) * 2019-01-08 2021-05-25 Raytheon Technologies Corporation Hollow airfoil with catenary profiles
US10808542B2 (en) * 2019-01-11 2020-10-20 Raytheon Technologies Corporation Method of forming gas turbine engine components
US11148221B2 (en) * 2019-08-29 2021-10-19 Raytheon Technologies Corporation Method of forming gas turbine engine components
CN110578051B (zh) * 2019-09-04 2021-04-23 首钢京唐钢铁联合有限责任公司 一种连续退火炉排烟风机的控制方法
DE102022201470A1 (de) 2022-02-11 2023-08-17 Sms Group Gmbh Anlage zum isothermen Schmieden

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3769696A (en) * 1970-05-12 1973-11-06 Toyoda Chuo Kenkyusho Kk Process for making a flanged metal product having raised portions around its flange
US4301584A (en) * 1980-01-31 1981-11-24 United Technologies Corporation Method of forming fiber and metal matrix composite
GB2096513B (en) * 1981-04-10 1984-09-19 Superform Metals Ltd Dual motion press
US5083371A (en) * 1990-09-14 1992-01-28 United Technologies Corporation Hollow metal article fabrication
US5479705A (en) * 1992-05-01 1996-01-02 Rolls-Royce Plc Method of manufacturing an article by superplastic forming and diffusion bonding
GB2269555B (en) * 1992-08-14 1995-01-04 Rolls Royce Plc A method of manufacturing an article by superplastic forming and diffusion bonding
US5469618A (en) * 1993-12-06 1995-11-28 General Electric Company Method for manufacturing hollow airfoils (two-piece concept)
US5419040A (en) * 1994-04-29 1995-05-30 United Technologies Corporation Hollow fan blade fabrication
US5581882A (en) * 1994-06-07 1996-12-10 Rolls-Royce Plc Method of manufacturing an article by superplastic forming and diffusion bonding
FR2724127B1 (fr) * 1994-09-07 1996-12-20 Snecma Procede de fabrication d'une aube creuse de turbomachine
FR2749784B1 (fr) * 1996-06-13 1998-07-31 Snecma Procede de fabrication d'un aube creuse de turbomachine et presse-four a multiple effet utilisee dans sa mise en oeuvre
FR2752388B1 (fr) * 1996-08-14 1998-09-18 Snecma Procede de fabrication d'une aube creuse de turbomachine comportant un decollement apres soudage

Also Published As

Publication number Publication date
FR2749784B1 (fr) 1998-07-31
CA2206160A1 (fr) 1997-12-13
US5933951A (en) 1999-08-10
FR2749784A1 (fr) 1997-12-19
EP0812649A1 (fr) 1997-12-17
EP0812649B1 (fr) 2002-07-31
DE69714354D1 (de) 2002-09-05
CA2206160C (fr) 2002-12-31
DE69714354T2 (de) 2003-03-27
JP3618964B2 (ja) 2005-02-09
JPH1082303A (ja) 1998-03-31
US6210630B1 (en) 2001-04-03

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