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RU2012128885A - Изделия из алюминиевого сплава, имеющие улучшенные комбинации свойств и способ их искусственного старения - Google Patents

Изделия из алюминиевого сплава, имеющие улучшенные комбинации свойств и способ их искусственного старения Download PDF

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Publication number
RU2012128885A
RU2012128885A RU2012128885/02A RU2012128885A RU2012128885A RU 2012128885 A RU2012128885 A RU 2012128885A RU 2012128885/02 A RU2012128885/02 A RU 2012128885/02A RU 2012128885 A RU2012128885 A RU 2012128885A RU 2012128885 A RU2012128885 A RU 2012128885A
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RU
Russia
Prior art keywords
aluminum alloy
properties
amount
artificial aging
alloy products
Prior art date
Application number
RU2012128885/02A
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English (en)
Inventor
Гари Г. БРЭЙ
Дхруба Дж. ЧАКРАБАРТИ
Диана К. ДЕНЦЕР
Джен К. ЛИН
Джон НЬЮМАН
Грегори Б. ВЕНЕМА
Кагатай ЯНАР
Жюльен БОЗЕЛЛИ
Original Assignee
Алкоа Инк.
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First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=40026309&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=RU2012128885(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Алкоа Инк. filed Critical Алкоа Инк.
Publication of RU2012128885A publication Critical patent/RU2012128885A/ru

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—Stringers, longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • 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
    • C22C21/10—Alloys based on aluminium 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Laminated Bodies (AREA)
  • Heat Treatment Of Steel (AREA)
  • Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
  • Extrusion Of Metal (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

1. Листовое изделие из алюминиевого сплава, состоящего из 6,8-8,5 вес.% Zn, 1,95-2,25 вес.% Cu, 1,55-1,75 вес.% Mg и до 0,25 вес.% по меньшей мере одного из Zr, Hf, Sc, Mn и V, и, при необходимости, добавок, измельчающих зерно, а остальное составляют алюминий и неизбежные примеси.2. Изделие по п.1, в котором количество Cu в алюминиевом сплаве составляет от 1,9 до 2,3 вес.%.3. Изделие по п.2, в котором количество Zn в алюминиевом сплаве составляет от 7,5 до 8,5 вес.%.4. Изделие по п.2, в котором количество Zn в алюминиевом сплаве составляет от 7,5 до 8,0 вес.%.5. Изделие по п.2, в котором количество Mg в алюминиевом сплаве составляет от 1,6 до 1,7 вес.%

Claims (5)

1. Листовое изделие из алюминиевого сплава, состоящего из 6,8-8,5 вес.% Zn, 1,95-2,25 вес.% Cu, 1,55-1,75 вес.% Mg и до 0,25 вес.% по меньшей мере одного из Zr, Hf, Sc, Mn и V, и, при необходимости, добавок, измельчающих зерно, а остальное составляют алюминий и неизбежные примеси.
2. Изделие по п.1, в котором количество Cu в алюминиевом сплаве составляет от 1,9 до 2,3 вес.%.
3. Изделие по п.2, в котором количество Zn в алюминиевом сплаве составляет от 7,5 до 8,5 вес.%.
4. Изделие по п.2, в котором количество Zn в алюминиевом сплаве составляет от 7,5 до 8,0 вес.%.
5. Изделие по п.2, в котором количество Mg в алюминиевом сплаве составляет от 1,6 до 1,7 вес.%
RU2012128885/02A 2007-05-14 2012-07-09 Изделия из алюминиевого сплава, имеющие улучшенные комбинации свойств и способ их искусственного старения RU2012128885A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/748,021 US8673209B2 (en) 2007-05-14 2007-05-14 Aluminum alloy products having improved property combinations and method for artificially aging same
US11/748,021 2007-05-14

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
RU2009146037/02A Division RU2465360C2 (ru) 2007-05-14 2008-05-14 Изделия из алюминиевого сплава, имеющие улучшенные комбинации свойств

Publications (1)

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RU2012128885A true RU2012128885A (ru) 2014-01-20

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ID=40026309

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RU2009146037/02A RU2465360C2 (ru) 2007-05-14 2008-05-14 Изделия из алюминиевого сплава, имеющие улучшенные комбинации свойств
RU2012128885/02A RU2012128885A (ru) 2007-05-14 2012-07-09 Изделия из алюминиевого сплава, имеющие улучшенные комбинации свойств и способ их искусственного старения

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Country Status (11)

Country Link
US (1) US8673209B2 (ru)
EP (2) EP3026136B1 (ru)
JP (1) JP2010527408A (ru)
KR (2) KR20100017775A (ru)
CN (1) CN101688269B (ru)
AU (2) AU2008267121B2 (ru)
BR (1) BRPI0811532A2 (ru)
CA (1) CA2686628C (ru)
ES (2) ES2747360T3 (ru)
RU (2) RU2465360C2 (ru)
WO (1) WO2008156532A2 (ru)

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