BR0317336A - Structure element fabrication process by thick plate machining - Google Patents

Structure element fabrication process by thick plate machining

Info

Publication number
BR0317336A
BR0317336A BR0317336-4A BR0317336A BR0317336A BR 0317336 A BR0317336 A BR 0317336A BR 0317336 A BR0317336 A BR 0317336A BR 0317336 A BR0317336 A BR 0317336A
Authority
BR
Brazil
Prior art keywords
thick plate
fabrication process
structure element
machined
plate machining
Prior art date
Application number
BR0317336-4A
Other languages
Portuguese (pt)
Other versions
BR0317336B1 (en
Inventor
Fabrice Heymes
David Godard
Timothy Warner
Julien Boselli
Raphaul Muzzolini
Sjoerd Van Der Veen
Original Assignee
Pechiney Rhenalu
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 claimed from FR0215997A external-priority patent/FR2848480B1/en
Application filed by Pechiney Rhenalu filed Critical Pechiney Rhenalu
Publication of BR0317336A publication Critical patent/BR0317336A/en
Publication of BR0317336B1 publication Critical patent/BR0317336B1/en

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
    • C22F1/057—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 copper 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
    • C22F1/047—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 magnesium 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
    • 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

Abstract

"PROCESSO DE FABRICAçãO DE ELEMENTOS DE ESTRUTURA POR USINAGEM DE CHAPAS ESPESSAS". A presente invenção refere-se a um processo de fabricação de uma peça metálica usinada, comportando a fabricação de uma chapa metálica, a pré-usinagem dessa chapa sobre uma ou duas faces para se obter um esboço pré-usinado, um tratamento de colocação em solução desse esboço pré-usinado, um tratamento de têmpera, eventualmente seguido de uma tração controlada. Essa peça pode ser utilizada como elemento de estrutura em construção aeronáutica."MANUFACTURING PROCESS OF STRUCTURE ELEMENTS BY THICK PLATE MACHINING". The present invention relates to a method of fabricating a machined metal part, comprising fabricating a metal plate, pre-machining such a sheet onto one or two sides to obtain a pre-machined sketch, a setting-up treatment. solution of this pre-machined sketch, a quenching treatment, eventually followed by controlled traction. This part can be used as a structural element in aeronautical construction.

BRPI0317336-4B1A 2002-12-17 2003-12-17 fabrication of structural elements by thick sheet metal machining and machined metal parts BR0317336B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0215997A FR2848480B1 (en) 2002-12-17 2002-12-17 METHOD OF MANUFACTURING STRUCTURAL ELEMENTS BY MACHINING THICK TOLES
US44699303P 2003-02-13 2003-02-13
PCT/FR2003/003753 WO2004056501A2 (en) 2002-12-17 2003-12-17 Method for making structural elements by machining thick plates

Publications (2)

Publication Number Publication Date
BR0317336A true BR0317336A (en) 2005-11-08
BR0317336B1 BR0317336B1 (en) 2013-07-09

Family

ID=32683898

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0317336-4B1A BR0317336B1 (en) 2002-12-17 2003-12-17 fabrication of structural elements by thick sheet metal machining and machined metal parts

Country Status (7)

Country Link
EP (1) EP1573080B1 (en)
JP (1) JP2006510808A (en)
AU (1) AU2003300632A1 (en)
BR (1) BR0317336B1 (en)
CA (1) CA2508534C (en)
RU (1) RU2341585C2 (en)
WO (1) WO2004056501A2 (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103834837B (en) * 2005-02-10 2016-11-09 肯联铝业轧制品-雷文斯伍德有限公司 Al-Zn-Cu-Mg acieral and manufacture method thereof and purposes
FR2900160B1 (en) * 2006-04-21 2008-05-30 Alcan Rhenalu Sa METHOD FOR MANUFACTURING A STRUCTURAL ELEMENT FOR AERONAUTICAL CONSTRUCTION COMPRISING A DIFFERENTIAL NUT
JP5345056B2 (en) * 2006-06-30 2013-11-20 コンステリウム ロールド プロダクツ−レイヴンズウッド，エルエルシー Heat-treatable high-strength aluminum alloy
WO2010081889A1 (en) * 2009-01-16 2010-07-22 Aleris Aluminum Koblenz Gmbh Method for the manufacture of an aluminium alloy plate product having low levels of residual stress
US9314826B2 (en) 2009-01-16 2016-04-19 Aleris Rolled Products Germany Gmbh Method for the manufacture of an aluminium alloy plate product having low levels of residual stress
CN102179422B (en) * 2010-12-29 2013-03-27 山东华盛荣镁业科技有限公司 Method for preparing metal plane plate
CN102303064A (en) * 2011-09-13 2012-01-04 王辉 Trapezoidal teeth dual-roller extrusion steel plate forming machine device
FR2997706B1 (en) * 2012-11-08 2014-11-07 Constellium France METHOD FOR MANUFACTURING A VARIABLE THICKNESS STRUCTURE ELEMENT FOR AERONAUTICAL CONSTRUCTION
JP6093192B2 (en) * 2013-01-25 2017-03-08 三菱航空機株式会社 Aircraft fuselage panel, aircraft wing
MX2017014219A (en) * 2015-05-08 2018-03-01 Novelis Inc Shock heat treatment of aluminum alloy articles.
RU2621499C2 (en) * 2015-11-17 2017-06-06 Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский технологический университет "МИСиС" Method for producing castings of high-strength aluminium-based alloys
EP3526352B1 (en) 2016-10-17 2021-09-01 Novelis Inc. Metal sheet with tailored properties
FR3059578B1 (en) 2016-12-07 2019-06-28 Constellium Issoire METHOD FOR MANUFACTURING A STRUCTURE ELEMENT
JP2022532347A (en) * 2019-06-03 2022-07-14 ノベリス・インコーポレイテッド Ultra-high-strength aluminum alloy products and their manufacturing methods
RU2771167C1 (en) * 2021-06-10 2022-04-27 Акционерное общество "Государственный Рязанский приборный завод" (АО "ГРПЗ") Method for manufacturing an aluminum wrought alloy casing

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62263954A (en) * 1986-05-08 1987-11-16 Nippon Light Metal Co Ltd Manufacture of heat-treatment-type aluminum alloy sheet for drawing
JPH086160B2 (en) * 1987-10-28 1996-01-24 日産自動車株式会社 Method for manufacturing conical tubular member
JP2510729B2 (en) * 1989-07-12 1996-06-26 日産自動車株式会社 Method for manufacturing heat-treatable aluminum alloy member
JPH083139B2 (en) * 1990-11-22 1996-01-17 日本鋼管株式会社 Method for manufacturing thick and complex heat-treating aluminum alloy member
FR2744136B1 (en) * 1996-01-25 1998-03-06 Pechiney Rhenalu THICK ALZNMGCU ALLOY PRODUCTS WITH IMPROVED PROPERTIES
JPH10298692A (en) * 1997-04-22 1998-11-10 Sky Alum Co Ltd Frame-shaped member with high strength and high precision, and its production
JP3764274B2 (en) * 1998-06-04 2006-04-05 Ｊｆｅ条鋼株式会社 Free-cutting hot-worked steel material and rough profile, manufacturing methods thereof, free-cutting hot-worked product, and manufacturing method thereof
FR2802946B1 (en) * 1999-12-28 2002-02-15 Pechiney Rhenalu AL-CU-MG ALLOY AIRCRAFT STRUCTURAL ELEMENT

Also Published As

Publication number Publication date
AU2003300632A8 (en) 2004-07-14
RU2005122471A (en) 2006-02-10
RU2341585C2 (en) 2008-12-20
JP2006510808A (en) 2006-03-30
CA2508534C (en) 2011-06-21
BR0317336B1 (en) 2013-07-09
CA2508534A1 (en) 2004-07-08
WO2004056501A3 (en) 2004-08-19
WO2004056501A2 (en) 2004-07-08
EP1573080A2 (en) 2005-09-14
EP1573080B1 (en) 2010-10-27
AU2003300632A1 (en) 2004-07-14

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Legal Events

Date Code Title Description
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B25D Requested change of name of applicant approved

Owner name: ALCAN RHENALU (FR)

B25D Requested change of name of applicant approved

Owner name: CONSTELLIUM FRANCE (FR)

B25G Requested change of headquarter approved

Owner name: CONSTELLIUM FRANCE (FR)

B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 17/12/2003, OBSERVADAS AS CONDICOES LEGAIS.

B25D Requested change of name of applicant approved
B25G Requested change of headquarter approved
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 15A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2494 DE 23-10-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.