BR112015013992A2 - método para fabricar componente moldado de liga de alumínio para aeronave e componente moldado para aeronave - Google Patents

método para fabricar componente moldado de liga de alumínio para aeronave e componente moldado para aeronave

Info

Publication number
BR112015013992A2
BR112015013992A2 BR112015013992A BR112015013992A BR112015013992A2 BR 112015013992 A2 BR112015013992 A2 BR 112015013992A2 BR 112015013992 A BR112015013992 A BR 112015013992A BR 112015013992 A BR112015013992 A BR 112015013992A BR 112015013992 A2 BR112015013992 A2 BR 112015013992A2
Authority
BR
Brazil
Prior art keywords
aircraft
molded component
aluminum alloy
fabricating
molded
Prior art date
Application number
BR112015013992A
Other languages
English (en)
Inventor
Ishikawa Chikara
Yamada Etsuko
Okada Hideki
Wada Takumi
Original Assignee
Kawasaki Heavy Ind Ltd
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 Kawasaki Heavy Ind Ltd filed Critical Kawasaki Heavy Ind Ltd
Publication of BR112015013992A2 publication Critical patent/BR112015013992A2/pt

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21B—ROLLING OF METAL
    • B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/18—Alloys based on aluminium with copper as the next major constituent with zinc
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21B—ROLLING OF METAL
    • B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/22—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21B—ROLLING OF METAL
    • B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
    • B21B2003/001—Aluminium or its alloys

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Metal Rolling (AREA)

Abstract

resumo patente de invenção: "método para fabricar componente moldado de liga de alumínio para aeronave e componente moldado para aeronave". trata-se de um método para fabricar um componente moldado para aeronave que inclui uma etapa para realizar um tratamento em solução em um material de liga de alumínio, então, realizar moldagem para um formato predeterminado sob condições de trabalho a frio e subsequentemente realizar um tratamento de endurecimento por envelhecimento artificial. no trabalho a frio, o material é moldado para um formato predeterminado ao mesmo tempo que é submetido a uma deformação que corresponde a uma têmpera t8 por um aparelho de conformação por rolos. é possível, dessa maneira, fabricar um componente moldado para uma aeronave produzido a partir de uma liga de alumínio no estado t8 em um custo mais baixo que no passado.
BR112015013992A 2012-12-21 2013-12-19 método para fabricar componente moldado de liga de alumínio para aeronave e componente moldado para aeronave BR112015013992A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2012279796 2012-12-21
PCT/JP2013/007463 WO2014097631A1 (ja) 2012-12-21 2013-12-19 アルミニウム合金製航空機用成形部品の製造方法および航空機用成形部品

Publications (1)

Publication Number Publication Date
BR112015013992A2 true BR112015013992A2 (pt) 2017-07-11

Family

ID=50977990

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015013992A BR112015013992A2 (pt) 2012-12-21 2013-12-19 método para fabricar componente moldado de liga de alumínio para aeronave e componente moldado para aeronave

Country Status (6)

Country Link
US (1) US20150299836A1 (pt)
EP (1) EP2937435B1 (pt)
JP (1) JP6480733B2 (pt)
BR (1) BR112015013992A2 (pt)
CA (1) CA2890535C (pt)
WO (1) WO2014097631A1 (pt)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6403515B2 (ja) * 2014-09-24 2018-10-10 三菱重工業株式会社 接合部処理方法及びドーム部材
CN105344786A (zh) * 2015-10-12 2016-02-24 中国航空工业集团公司北京航空材料研究院 一种人工时效态铝合金薄板的成形方法
CN105215124B (zh) * 2015-10-12 2018-06-05 中国航空工业集团公司北京航空材料研究院 一种人工时效态铝合金薄板的成形方法
CN105344779A (zh) * 2015-10-12 2016-02-24 中国航空工业集团公司北京航空材料研究院 一种人工时效态铝合金薄板的成形方法
CN105344780A (zh) * 2015-10-12 2016-02-24 中国航空工业集团公司北京航空材料研究院 一种人工时效态铝合金薄板的成形方法
CN105215125A (zh) * 2015-10-12 2016-01-06 中国航空工业集团公司北京航空材料研究院 一种自然时效态铝合金薄板的成形方法
CN105215123B (zh) * 2015-10-12 2018-06-05 中国航空工业集团公司北京航空材料研究院 一种自然时效态铝锂合金薄板的成形方法
CN105215122A (zh) * 2015-10-12 2016-01-06 中国航空工业集团公司北京航空材料研究院 一种自然时效态铝合金薄板的成形方法
CN105215121A (zh) * 2015-10-12 2016-01-06 中国航空工业集团公司北京航空材料研究院 一种人工时效态铝合金薄板的成形方法
JP7118688B2 (ja) * 2018-03-28 2022-08-16 三菱重工業株式会社 被加工物の加工方法及び加工装置
KR102494830B1 (ko) * 2022-03-22 2023-02-06 국방과학연구소 다단 시효처리를 이용한 Al-Li 합금의 제조방법

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02160134A (ja) * 1988-12-13 1990-06-20 Mitsubishi Heavy Ind Ltd Ａｌ−Ｌｉ合金形材の製作方法
US5393357A (en) * 1992-10-06 1995-02-28 Reynolds Metals Company Method of minimizing strength anisotropy in aluminum-lithium alloy wrought product by cold rolling, stretching and aging
JP2003213387A (ja) 2002-01-22 2003-07-30 Mitsubishi Heavy Ind Ltd 航空機用ロール成形部品の製造方法
BRPI0408432B1 (pt) * 2003-03-17 2015-07-21 Corus Aluminium Walzprod Gmbh Método para produção de uma estrutura integrada de alumínio monolítico e produto de alumínio usinado daquela estrutura
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
RU2481412C2 (ru) * 2007-09-21 2013-05-10 Алерис Алюминум Кобленц Гмбх ПРОДУКТ ИЗ Al-Cu-Li СПЛАВА, ПРИГОДНЫЙ ДЛЯ ПРИМЕНЕНИЯ В АВИАЦИИ И КОСМОНАВТИКЕ
CN103168110A (zh) * 2010-09-08 2013-06-19 美铝公司 改进的铝-锂合金及其生产方法

Also Published As

Publication number Publication date
JPWO2014097631A1 (ja) 2017-01-12
US20150299836A1 (en) 2015-10-22
CA2890535A1 (en) 2014-06-26
EP2937435A4 (en) 2016-09-07
CA2890535C (en) 2018-03-06
JP6480733B2 (ja) 2019-03-13
WO2014097631A1 (ja) 2014-06-26
EP2937435B1 (en) 2024-06-12
EP2937435A1 (en) 2015-10-28

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]

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