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FR2848480B1 - Procede de fabrication d'elements structuraux par usinage de toles epaisses - Google Patents

Procede de fabrication d'elements structuraux par usinage de toles epaisses

Info

Publication number
FR2848480B1
FR2848480B1 FR0215997A FR0215997A FR2848480B1 FR 2848480 B1 FR2848480 B1 FR 2848480B1 FR 0215997 A FR0215997 A FR 0215997A FR 0215997 A FR0215997 A FR 0215997A FR 2848480 B1 FR2848480 B1 FR 2848480B1
Authority
FR
France
Prior art keywords
sheet
machined
optionally
machining
fabrication
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 - Fee Related
Application number
FR0215997A
Other languages
English (en)
Other versions
FR2848480A1 (fr
Inventor
Fabrice Heymes
David Godard
Timothy Warner
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.)
Constellium Issoire SAS
Original Assignee
Pechiney Rhenalu SAS
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
Priority to FR0215997A priority Critical patent/FR2848480B1/fr
Application filed by Pechiney Rhenalu SAS filed Critical Pechiney Rhenalu SAS
Priority to AT03813619T priority patent/ATE486149T1/de
Priority to DE60334731T priority patent/DE60334731D1/de
Priority to ES03813619T priority patent/ES2355234T3/es
Priority to CN2003801067403A priority patent/CN1729308B/zh
Priority to US10/736,979 priority patent/US7837808B2/en
Priority to CA2508534A priority patent/CA2508534C/fr
Priority to JP2005502575A priority patent/JP2006510808A/ja
Priority to EP03813619A priority patent/EP1573080B1/fr
Priority to AU2003300632A priority patent/AU2003300632A1/en
Priority to PCT/FR2003/003753 priority patent/WO2004056501A2/fr
Priority to RU2005122471/02A priority patent/RU2341585C2/ru
Priority to UAA200507045A priority patent/UA82859C2/uk
Priority to BRPI0317336-4B1A priority patent/BR0317336B1/pt
Publication of FR2848480A1 publication Critical patent/FR2848480A1/fr
Application granted granted Critical
Publication of FR2848480B1 publication Critical patent/FR2848480B1/fr
Priority to US11/691,326 priority patent/US7763128B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12Construction or attachment of skin panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C37/00Manufacture of metal sheets, rods, wire, tubes, profiles or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
    • B21C37/02Manufacture of metal sheets, rods, wire, tubes, profiles or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of sheets
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/05Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/053Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/057Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with copper as the next major constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0081Fuselage structures substantially made from particular materials from metallic materials
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2261/00Machining or cutting being involved

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Thermal Sciences (AREA)
  • Metallurgy (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Heat Treatment Of Articles (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Metal Rolling (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
FR0215997A 2002-12-17 2002-12-17 Procede de fabrication d'elements structuraux par usinage de toles epaisses Expired - Fee Related FR2848480B1 (fr)

Priority Applications (15)

Application Number Priority Date Filing Date Title
FR0215997A FR2848480B1 (fr) 2002-12-17 2002-12-17 Procede de fabrication d'elements structuraux par usinage de toles epaisses
PCT/FR2003/003753 WO2004056501A2 (fr) 2002-12-17 2003-12-17 Procede de fabrication d'elements de structure par usinage de toles epaisses
ES03813619T ES2355234T3 (es) 2002-12-17 2003-12-17 Procedimiento de fabricación de elementos de esturctura por mecanizado de chapas gruesas.
CN2003801067403A CN1729308B (zh) 2002-12-17 2003-12-17 通过加工厚板材制造结构件的方法
US10/736,979 US7837808B2 (en) 2002-12-17 2003-12-17 Process for manufacturing structural components by machining plates
CA2508534A CA2508534C (fr) 2002-12-17 2003-12-17 Procede de fabrication d'elements de structure par usinage de toles epaisses
JP2005502575A JP2006510808A (ja) 2002-12-17 2003-12-17 厚板の加工による構造要素の製造方法
EP03813619A EP1573080B1 (fr) 2002-12-17 2003-12-17 Procede de fabrication d'elements de structure par usinage de toles epaisses
AT03813619T ATE486149T1 (de) 2002-12-17 2003-12-17 Verfahren zur herstellung von konstruktionselementen durch maschinelle bearbeitung dicker platten
DE60334731T DE60334731D1 (de) 2002-12-17 2003-12-17 Verfahren zur herstellung von konstruktionselementen durch maschinelle bearbeitung dicker platten
RU2005122471/02A RU2341585C2 (ru) 2002-12-17 2003-12-17 Способ изготовления элементов конструкции при помощи механической обработки толстых листов
UAA200507045A UA82859C2 (en) 2002-12-17 2003-12-17 Method for production of machining metal part, machined metal part, use of metal part and desing element
BRPI0317336-4B1A BR0317336B1 (pt) 2002-12-17 2003-12-17 processo de fabricaÇço de elementos de estrutura por usinagem de chapas espessas e peÇa metÁlica usinada
AU2003300632A AU2003300632A1 (en) 2002-12-17 2003-12-17 Method for making structural elements by machining thick plates
US11/691,326 US7763128B2 (en) 2002-12-17 2007-03-26 Process for manufacturing structural components by machining plates

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0215997A FR2848480B1 (fr) 2002-12-17 2002-12-17 Procede de fabrication d'elements structuraux par usinage de toles epaisses

Publications (2)

Publication Number Publication Date
FR2848480A1 FR2848480A1 (fr) 2004-06-18
FR2848480B1 true FR2848480B1 (fr) 2005-01-21

Family

ID=32338884

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0215997A Expired - Fee Related FR2848480B1 (fr) 2002-12-17 2002-12-17 Procede de fabrication d'elements structuraux par usinage de toles epaisses

Country Status (7)

Country Link
US (2) US7837808B2 (fr)
CN (1) CN1729308B (fr)
AT (1) ATE486149T1 (fr)
DE (1) DE60334731D1 (fr)
ES (1) ES2355234T3 (fr)
FR (1) FR2848480B1 (fr)
UA (1) UA82859C2 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106624653A (zh) * 2016-12-27 2017-05-10 西南铝业(集团)有限责任公司 6061t6铝合金板生产方法
CN106826127A (zh) * 2017-02-22 2017-06-13 青岛北琪实业有限公司 一种马口铁易开盖成型工艺

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US20050098245A1 (en) * 2003-11-12 2005-05-12 Venema Gregory B. Method of manufacturing near-net shape alloy product
JP4740896B2 (ja) * 2007-05-24 2011-08-03 富士フイルム株式会社 平版印刷版用アルミニウム合金板の製造方法
FR2925523B1 (fr) * 2007-12-21 2010-05-21 Alcan Rhenalu Produit lamine ameliore en alliage aluminium-lithium pour applications aeronautiques
EP2345044A4 (fr) * 2008-09-10 2014-01-15 9128 5270 Quebec Inc Procédé de fabrication de plaques d aluminium à conductivité électrique élevée
CN102392117A (zh) * 2011-11-02 2012-03-28 沈阳飞机工业(集团)有限公司 一种解决国产非预拉伸薄板化铣变形的方法
US8496764B2 (en) 2011-12-01 2013-07-30 Ford Global Technologies, Llc System and method for manufacturing an F-temper 7xxx series aluminum alloy
EP2623639A1 (fr) 2012-02-02 2013-08-07 Hydro Aluminium Deutschland GmbH Bande d'alliage en aluminium ayant une surface avec un aspect visuel amélioré et son procédé de fabrication
FR3014904B1 (fr) * 2013-12-13 2016-05-06 Constellium France Produits files pour planchers d'avion en alliage cuivre lithium
US9757784B2 (en) 2015-03-10 2017-09-12 Ford Global Technologies, Llc Temperature measurement device for metal sheet
CN105423113B (zh) * 2015-11-30 2018-03-27 太原科技大学 镁合金铸轧板制备宽幅薄板的坯料形状及尺寸的确定方法
CN109844150A (zh) * 2016-07-05 2019-06-04 纳诺尔有限责任公司 来自高强度耐腐蚀铝合金的带材和粉末
US11603583B2 (en) 2016-07-05 2023-03-14 NanoAL LLC Ribbons and powders from high strength corrosion resistant aluminum alloys
CA3032261A1 (fr) 2016-08-26 2018-03-01 Shape Corp. Procede de formage a chaud et appareil de pliage transversal d'une poutre d'aluminium profilee pour former a chaud un composant structural de vehicule
EP3529394A4 (fr) 2016-10-24 2020-06-24 Shape Corp. Procédé de formage et de traitement thermique d'un alliage d'aluminium en plusieurs étapes pour la production de composants pour véhicules
CN108161345B (zh) * 2017-12-08 2019-11-29 航天材料及工艺研究所 一种7055铝合金复杂结构零件的加工制造方法
EP3810819A2 (fr) 2018-06-20 2021-04-28 Nanoal LLC Alliages d'aluminium hautes performances à base d'al-zn-mg-zr pour la soudure et la fabrication additive
US11447228B2 (en) * 2020-04-23 2022-09-20 The Boeing Company Methods of manufacture for aircraft substructure
CN113441917B (zh) * 2021-07-15 2022-12-09 东北轻合金有限责任公司 一种航空用高强铝合金厚板整体结构件的加工方法
FR3138122A1 (fr) * 2022-07-25 2024-01-26 Airbus Operations Système de transport de grille de plancher de cabine d’aéronef en vue d’un assemblage d’un corps de fuselage d’aéronef et procédé de calibration dudit système de transport.
CN116372510B (zh) * 2023-03-20 2025-09-23 江西昌兴航空装备股份有限公司 一种横梁零件数控加工方法

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106624653A (zh) * 2016-12-27 2017-05-10 西南铝业(集团)有限责任公司 6061t6铝合金板生产方法
CN106826127A (zh) * 2017-02-22 2017-06-13 青岛北琪实业有限公司 一种马口铁易开盖成型工艺

Also Published As

Publication number Publication date
UA82859C2 (en) 2008-05-26
US7763128B2 (en) 2010-07-27
FR2848480A1 (fr) 2004-06-18
US20040182483A1 (en) 2004-09-23
CN1729308A (zh) 2006-02-01
DE60334731D1 (de) 2010-12-09
US7837808B2 (en) 2010-11-23
ATE486149T1 (de) 2010-11-15
ES2355234T3 (es) 2011-03-24
US20080236708A1 (en) 2008-10-02
CN1729308B (zh) 2010-04-14

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