CA2560672C - Element de structure pour construction aeronautique presentant une variation des proprietes d'emploi - Google Patents

Element de structure pour construction aeronautique presentant une variation des proprietes d'emploi Download PDF

Info

Publication number
CA2560672C
CA2560672C CA2560672A CA2560672A CA2560672C CA 2560672 C CA2560672 C CA 2560672C CA 2560672 A CA2560672 A CA 2560672A CA 2560672 A CA2560672 A CA 2560672A CA 2560672 C CA2560672 C CA 2560672C
Authority
CA
Canada
Prior art keywords
mpa
length
zones
sqroot
temperature
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
CA2560672A
Other languages
English (en)
French (fr)
Other versions
CA2560672A1 (fr
Inventor
Philippe Lequeu
David Dumont
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
Constellium France 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
Application filed by Constellium France SAS filed Critical Constellium France SAS
Publication of CA2560672A1 publication Critical patent/CA2560672A1/fr
Application granted granted Critical
Publication of CA2560672C publication Critical patent/CA2560672C/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/053—Changing 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
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27B—FURNACES, KILNS, OVENS, OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B9/00—Furnaces through which the charge is moved mechanically, e.g. of tunnel type; Similar furnaces in which the charge moves by gravity
    • F27B9/30—Details, accessories, or equipment peculiar to furnaces of these types
    • F27B9/40—Arrangements of controlling or monitoring devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D19/00—Arrangements of controlling devices

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Physics & Mathematics (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Heat Treatment Of Articles (AREA)
  • Forging (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Metal Rolling (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Rod-Shaped Construction Members (AREA)
CA2560672A 2004-03-23 2005-03-21 Element de structure pour construction aeronautique presentant une variation des proprietes d'emploi Expired - Fee Related CA2560672C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0402971 2004-03-23
FR0402971A FR2868084B1 (fr) 2004-03-23 2004-03-23 Element de structure pour construction aeronautique presentant une variation des proprietes d'emploi
PCT/FR2005/000681 WO2005098072A2 (fr) 2004-03-23 2005-03-21 Element de structure pour construction aeronautique presentant une variation des proprietes d’emploi

Publications (2)

Publication Number Publication Date
CA2560672A1 CA2560672A1 (fr) 2005-10-20
CA2560672C true CA2560672C (fr) 2012-07-17

Family

ID=34944905

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2560672A Expired - Fee Related CA2560672C (fr) 2004-03-23 2005-03-21 Element de structure pour construction aeronautique presentant une variation des proprietes d'emploi

Country Status (9)

Country Link
EP (1) EP1727921B1 (zh)
CN (1) CN100507066C (zh)
AT (1) ATE395444T1 (zh)
BR (1) BRPI0507940B1 (zh)
CA (1) CA2560672C (zh)
DE (1) DE602005006764D1 (zh)
ES (1) ES2307180T3 (zh)
FR (1) FR2868084B1 (zh)
WO (1) WO2005098072A2 (zh)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2894857B1 (fr) 2005-12-16 2009-05-15 Alcan Rhenalu Sa Procede de fabrication de demi-produits comportant deux alliages a base d'aluminium
WO2007106772A2 (en) * 2006-03-13 2007-09-20 Alcoa Inc. Method and process of non-isothermal aging for aluminum alloys
FR2900160B1 (fr) * 2006-04-21 2008-05-30 Alcan Rhenalu Sa Procede de fabrication d'un element de structure pour construction aeronautique comprenant un ecrouissage differentiel
EP2193214B1 (en) 2007-10-04 2018-01-10 Aleris Rolled Products Germany GmbH A method for manufacturing a wrought metal plate product having a gradient in engineering properties
FR2945464B1 (fr) * 2009-05-13 2012-03-23 Alcan Rhenalu Procede d'assemblage par soudage de pieces en alliage d'aluminium.
WO2011091983A2 (en) 2010-01-29 2011-08-04 Tata Steel Nederland Technology Bv Process for the heat treatment of metal strip material, and strip material produced in that way
DE102010000292B4 (de) * 2010-02-03 2014-02-13 Thyssenkrupp Steel Europe Ag Metallband hergestellt aus Stahl mit unterschiedlichen mechanischen Eigenschaften
JP5776874B2 (ja) 2011-02-14 2015-09-09 住友電気工業株式会社 マグネシウム合金圧延材、およびマグネシウム合金部材、ならびにマグネシウム合金圧延材の製造方法
FR2997706B1 (fr) * 2012-11-08 2014-11-07 Constellium France Procede de fabrication d'un element de structure d'epaisseur variable pour construction aeronautique
US11220729B2 (en) 2016-05-20 2022-01-11 Ut-Battelle, Llc Aluminum alloy compositions and methods of making and using the same
US11242587B2 (en) 2017-05-12 2022-02-08 Ut-Battelle, Llc Aluminum alloy compositions and methods of making and using the same
US11180839B2 (en) 2017-10-26 2021-11-23 Ut-Battelle, Llc Heat treatments for high temperature cast aluminum alloys

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4518351A (en) * 1982-03-22 1985-05-21 Mellen Sr Robert H Method of providing a dynamic temperature gradient
FR2707092B1 (fr) * 1993-06-28 1995-08-25 Pechiney Rhenalu Produit métallurgique en alliage d'Al à durcissement structural présentant une variation continue des propriétés d'emploi suivant une direction donnée et un procédé et dispositif d'obtention de celui-ci.

Also Published As

Publication number Publication date
CN1930317A (zh) 2007-03-14
EP1727921B1 (fr) 2008-05-14
FR2868084A1 (fr) 2005-09-30
WO2005098072A2 (fr) 2005-10-20
CA2560672A1 (fr) 2005-10-20
ES2307180T3 (es) 2008-11-16
CN100507066C (zh) 2009-07-01
WO2005098072A3 (fr) 2006-05-04
BRPI0507940A (pt) 2007-07-17
ATE395444T1 (de) 2008-05-15
EP1727921A2 (fr) 2006-12-06
DE602005006764D1 (de) 2008-06-26
BRPI0507940B1 (pt) 2018-04-17
FR2868084B1 (fr) 2006-05-26

Similar Documents

Publication Publication Date Title
CA2560672C (fr) Element de structure pour construction aeronautique presentant une variation des proprietes d'emploi
EP1799391B1 (fr) Element de structure soude comprenant au moins deux parties en alliages d'aluminium presentant un etat metallurgique different, procede de fabrication d'un tel element
EP2364378B1 (fr) Produits en alliage aluminium-cuivre-lithium
EP2010689B1 (fr) Procédé de fabrication d'un élément de structure pour construction aéronautique comprenant un écrouissage differentiel
CA2528614C (fr) Produits en alliages al-zn-mg-cu a compromis caracteristiques mecaniques statiques/tolerance aux dommages ameliore
EP2449142B1 (fr) Alliage aluminium cuivre lithium a resistance mecanique et tenacite ameliorees
EP2766503B1 (fr) Procédé de transformation amélioré de tôles en alliage al-cu-li
EP2235224B1 (fr) PROCÉDÉ DE FABRICATION D'UN PRODUIT LAMINÉ EN Al-Li POUR DES APPLICATIONS AÉRONAUTIQUES
EP2917380B1 (fr) Procede de fabrication d'un element de structure d'epaisseur variable pour construction aeronautique
FR2855834A1 (fr) Produit ouvre en alliage a grande tolerance aux dommages, en particulier pour des applications dans le domaine aerospatial
EP2429752B1 (fr) Procede d'assemblage par soudage de pieces en alliage d'aluminium avec deformation a froid suivi d'un revenu post soudage de l'ensemble de la zone soudee ; assemblage correspondant
FR2907467A1 (fr) Procede de fabrication de produits en alliage d'aluminium de la serie aa2000 et produits fabriques selon ce procede
EP1544315B1 (fr) Produit corroyé sous forme de tôle laminée et élément de structure pour aéronef en alliage Al-Zn-Cu-Mg
EP3526358B1 (fr) Toles minces en alliage aluminium-magnesium-scandium pour applications aerospatiales
WO2007080265A1 (fr) Procede de fabrication de demi-produits comportant deux alliages a base d'aluminium
CA2508534C (fr) Procede de fabrication d'elements de structure par usinage de toles epaisses
FR2848480A1 (fr) Procede de fabrication d'elements structuraux par usinage de toles epaisses
US20050217770A1 (en) Structural member for aeronautical construction with a variation of usage properties
EP3610047B1 (fr) Produits en alliage aluminium-cuivre-lithium
CA3001519C (fr) Toles minces en alliage aluminium-magnesium-zirconium pour applications aerospatiales

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed

Effective date: 20210322