PT3265595T - Ligas de alumínio 7xxx de resistência elevada e métodos de produção das mesmas - Google Patents

Ligas de alumínio 7xxx de resistência elevada e métodos de produção das mesmas

Info

Publication number
PT3265595T
PT3265595T PT16834065T PT16834065T PT3265595T PT 3265595 T PT3265595 T PT 3265595T PT 16834065 T PT16834065 T PT 16834065T PT 16834065 T PT16834065 T PT 16834065T PT 3265595 T PT3265595 T PT 3265595T
Authority
PT
Portugal
Prior art keywords
making
methods
same
high strength
aluminum alloys
Prior art date
Application number
PT16834065T
Other languages
English (en)
Inventor
G Kamat Rajeev
J Chakrabarti Dhruba
Ranjan MOHANTY Rashmi
Vilas Kulkarni Rahul
E Bendzinski Duane
Timm Juergen
Original Assignee
Novelis Inc
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 Novelis Inc filed Critical Novelis Inc
Publication of PT3265595T publication Critical patent/PT3265595T/pt

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D29/00Superstructures, understructures, or sub-units thereof, characterised by the material thereof
    • B62D29/008Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of light alloys, e.g. extruded
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/10Alloys based on aluminium 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
    • C22F1/002Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Architecture (AREA)
  • Structural Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Continuous Casting (AREA)
  • Metal Rolling (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Materials For Medical Uses (AREA)
  • Conductive Materials (AREA)
  • Heat Treatment Of Articles (AREA)
PT16834065T 2015-10-30 2016-10-28 Ligas de alumínio 7xxx de resistência elevada e métodos de produção das mesmas PT3265595T (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201562248796P 2015-10-30 2015-10-30
US201662326858P 2016-04-25 2016-04-25

Publications (1)

Publication Number Publication Date
PT3265595T true PT3265595T (pt) 2019-05-08

Family

ID=57960808

Family Applications (1)

Application Number Title Priority Date Filing Date
PT16834065T PT3265595T (pt) 2015-10-30 2016-10-28 Ligas de alumínio 7xxx de resistência elevada e métodos de produção das mesmas

Country Status (23)

Country Link
US (2) US11421309B2 (pt)
EP (2) EP3521466B1 (pt)
JP (2) JP6971151B2 (pt)
KR (2) KR20170138533A (pt)
CN (2) CN110453122A (pt)
AU (1) AU2016344192B2 (pt)
BR (1) BR112017021490B1 (pt)
CA (1) CA2979717C (pt)
CY (1) CY1121505T1 (pt)
DK (1) DK3265595T3 (pt)
ES (1) ES2719555T3 (pt)
HR (1) HRP20190548T1 (pt)
HU (1) HUE042400T2 (pt)
IL (1) IL258885A (pt)
LT (1) LT3265595T (pt)
MX (2) MX2017011840A (pt)
PL (1) PL3265595T3 (pt)
PT (1) PT3265595T (pt)
RS (1) RS58615B1 (pt)
RU (1) RU2717434C2 (pt)
SI (1) SI3265595T1 (pt)
WO (1) WO2017075319A1 (pt)
ZA (1) ZA201802759B (pt)

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CN108165849A (zh) * 2017-12-08 2018-06-15 四川福蓉科技股份公司 一种7系铝合金及其制备方法
CN107937773A (zh) * 2017-12-19 2018-04-20 辽宁忠大铝业有限公司 一种耐热铝合金及其制备方法
CN108048714A (zh) * 2017-12-27 2018-05-18 柳州智臻智能机械有限公司 一种电子产品结构件用铝合金及其制备方法
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CN108149095A (zh) * 2017-12-29 2018-06-12 西南铝业(集团)有限责任公司 一种用于重载列车牵引杆的低成本超高强7系铝合金材料的生产方法
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CN108330361B (zh) * 2018-05-20 2019-11-19 温州市赢创新材料技术有限公司 一种汽车保险杠用7000系合金材料及其生产方法
KR102076800B1 (ko) 2018-05-24 2020-02-12 (주)동양에이.케이코리아 알루미늄-실리콘 합금 압출재의 제조 방법 및 이를 이용하여 제조된 알루미늄-실리콘 합금 압출재
CN108707794A (zh) * 2018-05-31 2018-10-26 铜陵康达铝合金制品有限责任公司 一种汽车发动机用耐热耐腐蚀铝合金型材的制备方法
CN108642354A (zh) * 2018-05-31 2018-10-12 铜陵康达铝合金制品有限责任公司 一种汽车发动机用耐高温抗腐蚀铝合金型材及其制备方法
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CN108998710B (zh) * 2018-08-23 2019-11-12 山东创新金属科技有限公司 一种手机外壳用铝合金制备工艺
CN109266920B (zh) * 2018-08-30 2020-11-24 四川福蓉科技股份公司 一种7系铝合金及其生产方法
ES2978594T3 (es) 2018-11-12 2024-09-16 Novelis Inc Productos de aleación de aluminio termotratable, rápidamente envejecidos, de alta resistencia y métodos para fabricar los mismos
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CN109457151A (zh) * 2018-12-14 2019-03-12 烟台南山学院 一种高强高韧铝合金板材及其制备方法
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CN109666827B (zh) * 2019-02-22 2021-02-12 洛阳华陵镁业有限公司 一种超强超韧7055Sc铝合金锻件
KR102203716B1 (ko) * 2019-03-08 2021-01-15 한국생산기술연구원 압출성 및 강도가 향상된 고열전도도 알루미늄 합금, 상기 알루미늄 합금 제조 방법 및 상기 알루미늄 합금 압출성형제품 제작 방법
CN109763040A (zh) * 2019-03-27 2019-05-17 亚太轻合金(南通)科技有限公司 一种铝合金材料及其制备的方法
CN110042287A (zh) * 2019-04-22 2019-07-23 中南大学 一种超强高塑性Al-Zn-Mg-Cu系铝合金及其制备工艺
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CN110055445A (zh) * 2019-05-17 2019-07-26 亚太轻合金(南通)科技有限公司 一种高强度铝合金及其制备方法
CN110066931B (zh) * 2019-05-31 2020-08-14 上海纳特汽车标准件有限公司 一种适于冷成形的铝合金及其制备方法
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