DE602005006764D1 - Konstruktionselement für die luftfahrt mit variation der anwendungstechnischen eigenschaften - Google Patents

Konstruktionselement für die luftfahrt mit variation der anwendungstechnischen eigenschaften

Info

Publication number
DE602005006764D1
DE602005006764D1 DE602005006764T DE602005006764T DE602005006764D1 DE 602005006764 D1 DE602005006764 D1 DE 602005006764D1 DE 602005006764 T DE602005006764 T DE 602005006764T DE 602005006764 T DE602005006764 T DE 602005006764T DE 602005006764 D1 DE602005006764 D1 DE 602005006764D1
Authority
DE
Germany
Prior art keywords
sub
areas
groups
equal
variation
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.)
Active
Application number
DE602005006764T
Other languages
English (en)
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
Alcan 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
Application filed by Alcan Rhenalu SAS filed Critical Alcan Rhenalu SAS
Publication of DE602005006764D1 publication Critical patent/DE602005006764D1/de
Active 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
DE602005006764T 2004-03-23 2005-03-21 Konstruktionselement für die luftfahrt mit variation der anwendungstechnischen eigenschaften Active DE602005006764D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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 (1)

Publication Number Publication Date
DE602005006764D1 true DE602005006764D1 (de) 2008-06-26

Family

ID=34944905

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005006764T Active DE602005006764D1 (de) 2004-03-23 2005-03-21 Konstruktionselement für die luftfahrt mit variation der anwendungstechnischen eigenschaften

Country Status (9)

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

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
CN101815804B (zh) 2007-10-04 2013-07-24 阿勒里斯铝业科布伦茨有限公司 制造在工程性质上具有梯度的锻造金属板产品的方法
FR2945464B1 (fr) * 2009-05-13 2012-03-23 Alcan Rhenalu Procede d'assemblage par soudage de pieces en alliage d'aluminium.
CN102770565B (zh) 2010-01-29 2015-04-22 塔塔钢铁荷兰科技有限责任公司 金属带材的热处理方法以及以这种方式生产的带材
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
WO2019084320A1 (en) * 2017-10-26 2019-05-02 Amit Shyam THERMAL 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
EP1727921A2 (de) 2006-12-06
BRPI0507940B1 (pt) 2018-04-17
FR2868084B1 (fr) 2006-05-26
FR2868084A1 (fr) 2005-09-30
ATE395444T1 (de) 2008-05-15
CN1930317A (zh) 2007-03-14
CA2560672C (fr) 2012-07-17
EP1727921B1 (de) 2008-05-14
CA2560672A1 (fr) 2005-10-20
BRPI0507940A (pt) 2007-07-17
ES2307180T3 (es) 2008-11-16
WO2005098072A3 (fr) 2006-05-04
WO2005098072A2 (fr) 2005-10-20
CN100507066C (zh) 2009-07-01

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Legal Events

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8327 Change in the person/name/address of the patent owner

Owner name: ALCAN RHENALU, COURBEVOIE, FR

8328 Change in the person/name/address of the agent

Representative=s name: BEETZ & PARTNER PATENTANWAELTE, 80538 MUENCHEN

8364 No opposition during term of opposition
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Representative=s name: BEETZ & PARTNER PATENT- UND RECHTSANWAELTE, DE