ES2153640T3 - Procedimiento de fabricacion de un alabe hueco de turbomaquina que comprende un desprendimiento despues de soldadura. - Google Patents

Procedimiento de fabricacion de un alabe hueco de turbomaquina que comprende un desprendimiento despues de soldadura.

Info

Publication number
ES2153640T3
ES2153640T3 ES97401926T ES97401926T ES2153640T3 ES 2153640 T3 ES2153640 T3 ES 2153640T3 ES 97401926 T ES97401926 T ES 97401926T ES 97401926 T ES97401926 T ES 97401926T ES 2153640 T3 ES2153640 T3 ES 2153640T3
Authority
ES
Spain
Prior art keywords
alabe
welding
manufacturing procedure
detachment
hollow
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
ES97401926T
Other languages
English (en)
Inventor
Gilles Michel Georges Lo Calle
Gilles Charles Klein
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 ES2153640T3 publication Critical patent/ES2153640T3/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
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
    • B21D26/021—Deforming sheet bodies
    • B21D26/027—Means for controlling fluid parameters, e.g. pressure or temperature
    • 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
    • B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
    • B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
    • B21D26/055—Blanks having super-plastic properties
    • 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
    • B21D53/00—Making other particular articles
    • B21D53/78—Making other particular articles propeller blades; turbine blades
    • 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
    • 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
    • Y10T29/49341—Hollow blade with cooling passage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • Arc Welding In General (AREA)
  • Forging (AREA)

Abstract

PROCEDIMIENTO DE FABRICACION DE UN ALABE HUECA DE TURBOMOTOR QUE LLEVA UN DESPRENDIMIENTO DESPUES DE LA SOLDADURA. UN PROCEDIMIENTO DE FABRICACION DE UN ALABE (1) HUECA DE TURBOMOTOR QUE DESPUES DE LA SOLDADURA-DIFUSION DE LAS PIEZAS CONSTITUYENTES (2,3,4) CONSISTE EN UNA ETAPA COMPLEMENTARIA QUE REALIZA EL DESPRENDIMIENTO DE LAS ZONAS REVESTIDAS POR UN REVESTIMIENTO ANTIDIFUSION DURANTE LA CUAL SE FORMA UN CONDUCTO DE ALIMENTACION DE GAS (90) EN UNA ZONA DEL ALABE DONDE ESTAN DISPUESTOS UNOS ORIFICIOS (5) EN LA CHAPA INTERMEDIA (4), MEDIANTE INYECCIONES DE GAS A PRESION A LA VEZ QUE SE PROPORCIONA UN CALENTAMIENTO LOCALIZADO DE DICHA ZONA DEL ALABE. SE PREVE UN DISPOSITIVO PARTICULAR PARA LA REALIZACION DE LA OPERACION.
ES97401926T 1996-08-14 1997-08-13 Procedimiento de fabricacion de un alabe hueco de turbomaquina que comprende un desprendimiento despues de soldadura. Expired - Lifetime ES2153640T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9610194A FR2752388B1 (fr) 1996-08-14 1996-08-14 Procede de fabrication d'une aube creuse de turbomachine comportant un decollement apres soudage

Publications (1)

Publication Number Publication Date
ES2153640T3 true ES2153640T3 (es) 2001-03-01

Family

ID=9495050

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97401926T Expired - Lifetime ES2153640T3 (es) 1996-08-14 1997-08-13 Procedimiento de fabricacion de un alabe hueco de turbomaquina que comprende un desprendimiento despues de soldadura.

Country Status (8)

Country Link
US (1) US5946802A (es)
EP (1) EP0824048B1 (es)
JP (1) JP3477036B2 (es)
CA (1) CA2207828C (es)
DE (1) DE69703866T2 (es)
ES (1) ES2153640T3 (es)
FR (1) FR2752388B1 (es)
IL (1) IL121600A (es)

Families Citing this family (9)

* 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
US6264880B1 (en) * 1998-07-22 2001-07-24 The Regents Of The University Of California Manifold free multiple sheet superplastic forming
GB2360236B (en) * 2000-03-18 2003-05-14 Rolls Royce Plc A method of manufacturing an article by diffusion bonding and superplastic forming
FR2820062B1 (fr) * 2001-02-01 2003-03-07 Snecma Moteurs Installation de formage d'une piece et application au formage a chaud
FR2867096B1 (fr) * 2004-03-08 2007-04-20 Snecma Moteurs Procede de fabrication d'un bord d'attaque ou de fuite de renforcement pour une aube de soufflante
WO2015070409A1 (zh) * 2013-11-14 2015-05-21 深圳智慧能源技术有限公司 制造中空结构的方法
GB201809397D0 (en) * 2018-06-07 2018-07-25 Group Rhodes Ltd Super plastic forming apparatus and method
US10808550B2 (en) * 2018-12-13 2020-10-20 Raytheon Technologies Corporation Fan blade with integral metering device for controlling gas pressure within the fan blade
CN114669970A (zh) * 2022-05-06 2022-06-28 北京航空航天大学 一种复材叶片钛合金包边的成形方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4882823A (en) * 1988-01-27 1989-11-28 Ontario Technologies Corp. Superplastic forming diffusion bonding process
FR2672826B1 (fr) * 1991-02-20 1995-04-21 Snecma Procede de fabrication d'une aube creuse pour turbomachine.
GB9209464D0 (en) * 1992-05-01 1992-06-17 Rolls Royce Plc A method of manufacturing an article by superplastic forming and diffusion bonding
US5457884A (en) * 1992-08-14 1995-10-17 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
US5692881A (en) * 1995-06-08 1997-12-02 United Technologies Corporation Hollow metallic structure and method of manufacture
FR2739045B1 (fr) * 1995-09-27 1997-10-31 Snecma Procede de fabrication d'une aube creuse de turbomachine

Also Published As

Publication number Publication date
US5946802A (en) 1999-09-07
CA2207828C (fr) 2005-02-22
DE69703866T2 (de) 2001-05-23
IL121600A (en) 2004-03-28
EP0824048A1 (fr) 1998-02-18
FR2752388A1 (fr) 1998-02-20
DE69703866D1 (de) 2001-02-15
IL121600A0 (en) 1998-02-08
JPH10103005A (ja) 1998-04-21
FR2752388B1 (fr) 1998-09-18
JP3477036B2 (ja) 2003-12-10
CA2207828A1 (fr) 1998-02-14
EP0824048B1 (fr) 2001-01-10

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