CA2124105A1 - Procede de sougage laser d'un assemblage de deux pieces metalliques - Google Patents

Procede de sougage laser d'un assemblage de deux pieces metalliques

Info

Publication number
CA2124105A1
CA2124105A1 CA2124105A CA2124105A CA2124105A1 CA 2124105 A1 CA2124105 A1 CA 2124105A1 CA 2124105 A CA2124105 A CA 2124105A CA 2124105 A CA2124105 A CA 2124105A CA 2124105 A1 CA2124105 A1 CA 2124105A1
Authority
CA
Canada
Prior art keywords
laser beam
assembling
method used
welding method
metal parts
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.)
Granted
Application number
CA2124105A
Other languages
English (en)
Other versions
CA2124105C (fr
Inventor
Jacques Georges Wilfrid Rene Havard
Michel Robert Jouardet
Jean-Yves Maurice Loreau
Gerard Louis Zanolin
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
Jacques Georges Wilfrid Rene Havard
Michel Robert Jouardet
Jean-Yves Maurice Loreau
Gerard Louis Zanolin
Lexvall
Snecma Moteurs
Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snec Ma"
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 Jacques Georges Wilfrid Rene Havard, Michel Robert Jouardet, Jean-Yves Maurice Loreau, Gerard Louis Zanolin, Lexvall, Snecma Moteurs, Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snec Ma" filed Critical Jacques Georges Wilfrid Rene Havard
Publication of CA2124105A1 publication Critical patent/CA2124105A1/fr
Application granted granted Critical
Publication of CA2124105C publication Critical patent/CA2124105C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/0604—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/0604—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams
    • B23K26/0608—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams in the same heat affected zone [HAZ]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/21—Bonding by welding
    • B23K26/24—Seam welding
    • B23K26/244—Overlap seam welding

Abstract

Le procédé permet de fabriquer des caissons cloisonnés en réalisant la fixation à partir de l'extérieur de ces caissons.
On utilise deux tirs successifs d'un faisceau laser (8A, 8B) inclinés, se croisant au niveau de la surface supérieure (1B) de la pièce (1) constituant la tête de l'assemblage. Les deux axes de soudage laser (8A, 8B)coupent deux coins supérieurs (2C) de la pièce (2) faisant office de pied du T. Le dispositif de soudage est placé à l'extérieur du caisson, c'est-à-dire du côte de la surface supérieure (1B) de la tête (1) du T.
Application à la fabrication des bras du canal externe d'un turboréacteur.
CA002124105A 1993-05-25 1994-05-20 Procede de sougage laser d'un assemblage de deux pieces metalliques Expired - Fee Related CA2124105C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9306208 1993-05-25
FR9306208A FR2705603B1 (fr) 1993-05-25 1993-05-25 Procédé de soudage laser d'un assemblage de deux pièces métalliques.

Publications (2)

Publication Number Publication Date
CA2124105A1 true CA2124105A1 (fr) 1994-11-26
CA2124105C CA2124105C (fr) 1999-02-16

Family

ID=9447409

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002124105A Expired - Fee Related CA2124105C (fr) 1993-05-25 1994-05-20 Procede de sougage laser d'un assemblage de deux pieces metalliques

Country Status (8)

Country Link
US (1) US5483034A (fr)
EP (1) EP0626231B1 (fr)
JP (1) JP2730664B2 (fr)
CA (1) CA2124105C (fr)
DE (1) DE69400674T2 (fr)
ES (1) ES2092869T3 (fr)
FR (1) FR2705603B1 (fr)
IL (1) IL109743A (fr)

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DE19609722B4 (de) * 1996-03-13 2007-01-18 Trumpf Systemtechnik Gmbh Verfahren zum Verbinden zweier metallischer Profile, insbesondere zweier stranggepreßter Aluminiumprofilteile
DE19639667C1 (de) * 1996-09-27 1998-03-12 Daimler Benz Aerospace Airbus Verfahren zum Schweißen von Profilen auf großformatigen Aluminium-Strukturbauteilen mittels Laserstrahlen
DE19717737B4 (de) * 1997-04-26 2008-02-28 Oerlikon Textile Gmbh & Co. Kg Spinnboxrahmen für eine Offenend-Spinnvorrichtung
DE19719279A1 (de) * 1997-05-07 1998-11-12 Schlafhorst & Co W Offenend-Spinnvorrichtung
ES2131479B1 (es) * 1997-11-10 2000-03-01 Torres Martinez M Util y proceso de ensamblaje para soldadura laser.
SE519782C2 (sv) * 2001-08-29 2003-04-08 Volvo Aero Corp Förfarande för framställning av ett ihåligt blad avsett för en stator-eller rotorkomponent
SE519781C2 (sv) * 2001-08-29 2003-04-08 Volvo Aero Corp Förfarande för framställning av en stator-eller rotorkomponent
DE10234242B4 (de) 2002-07-09 2005-10-27 Airbus Deutschland Gmbh Anordnung und Verfahren zur Regelung der Nahtlage eines laserstrahlgefügten Profils
ES2285131T3 (es) * 2002-08-14 2007-11-16 Volvo Aero Corporation Procedimiento para la fabricacion de un componente de estator o de rotor.
ATE363018T1 (de) * 2002-08-14 2007-06-15 Volvo Aero Corp Verfahren zur herstellung einer statorkomponente
US7614150B2 (en) * 2002-08-14 2009-11-10 Volvo Aero Corporation Method for manufacturing a stator or rotor component
FR2846898B1 (fr) * 2002-11-07 2005-07-15 Snecma Moteurs Procede de soudage laser en une passe d'un assemblage en t de pieces metalliques
DE10307610A1 (de) * 2003-02-22 2004-09-02 Rolls-Royce Deutschland Ltd & Co Kg Verdichterschaufel für ein Flugzeugtriebwerk
EP2094430A4 (fr) * 2006-12-18 2010-07-28 Volvo Aero Corp Procédé de raccordement de parties métalliques et dispositif de soudage
JP5061836B2 (ja) * 2007-10-10 2012-10-31 株式会社日立プラントテクノロジー 羽根車の溶接方法及び羽根車
JP5290606B2 (ja) * 2008-03-31 2013-09-18 株式会社総合車両製作所 レーザ溶接方法
IT1397327B1 (it) * 2009-12-11 2013-01-10 Nuovo Pignone Spa Metodi e sistemi per saldatura a raggio di giranti.
US20130056449A1 (en) * 2011-09-07 2013-03-07 General Electric Company Welding system and method
US9409251B2 (en) 2011-10-12 2016-08-09 Asml Netherlands B.V. Radiation beam welding method, body and lithographic apparatus
US9221121B2 (en) * 2013-03-27 2015-12-29 General Electric Company Welding process for welding three elements using two angled energy beams
JP6650575B2 (ja) * 2014-01-08 2020-02-19 パナソニックＩｐマネジメント株式会社 レーザ溶接方法
CN104942439B (zh) * 2015-03-26 2017-04-19 上海工程技术大学 一种907a高强钢t型接头激光焊接加工方法
RU2614358C2 (ru) * 2015-08-27 2017-03-24 Открытое акционерное общество "Национальный институт авиационных технологий" (ОАО НИАТ) Способ соединения лучевой сваркой стрингеров с обшивкой при изготовлении стрингерных панелей
RU2653396C1 (ru) * 2016-12-19 2018-05-08 Публичное акционерное общество "Региональный инжиниринговый центр промышленных лазерных технологий "КАИ-Лазер" Способ изготовления тавровой балки лазерным лучом
PT3604792T (pt) 2018-08-03 2022-01-31 Ge Renewable Tech Tampa preformada com perfis interpás para turbinas hidráulicas
US11331752B2 (en) * 2018-08-30 2022-05-17 Ipg Photonics Corporation Backside surface welding system and method
CN112388255A (zh) * 2020-11-06 2021-02-23 安徽四建控股集团有限公司 一种基于公交站牌用t型钢板的自动焊接方法

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US3695778A (en) * 1970-09-18 1972-10-03 Trw Inc Turbine blade
US4644126A (en) * 1984-12-14 1987-02-17 Ford Motor Company Method for producing parallel-sided melt zone with high energy beam
JPS62127188A (ja) * 1985-11-28 1987-06-09 Nippon Kokan Kk <Nkk> 船体の二重底ブロツクの建造方法
US4868365A (en) * 1988-06-06 1989-09-19 Ford Motor Company Method for welding torque converter blades to a housing using a laser welding beam
IT1239663B (it) * 1990-03-05 1993-11-11 Prima Cimolai Procedimento di saldatura per travi metalliche e travi metalliche cosi' ottenute

Also Published As

Publication number Publication date
FR2705603B1 (fr) 1995-06-30
JPH0747484A (ja) 1995-02-21
DE69400674T2 (de) 1997-02-27
CA2124105C (fr) 1999-02-16
IL109743A0 (en) 1994-10-07
EP0626231B1 (fr) 1996-10-09
FR2705603A1 (fr) 1994-12-02
EP0626231A1 (fr) 1994-11-30
DE69400674D1 (de) 1996-11-14
US5483034A (en) 1996-01-09
ES2092869T3 (es) 1996-12-01
IL109743A (en) 1998-07-15
JP2730664B2 (ja) 1998-03-25

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