49.025.20 铝 标准查询与下载

SAE AMS4044L-2008 5.6Zn 2.5Mg 1.6Cu 0.23Cr Annealed(7075-0)或制造(7075-F)特指的铝合金薄板材和厚板材

1.1 FormThis specification covers an aluminum alloy in the form of sheet and plate supplied in the annealed (0) condition. When specified, product may be supplied in the “as fabricated” (F) condition.1.2 ApplicationThese products have been used typically for formed structural parts which will be subsequently heat treated, but usage is not limited to such applications.1.2.1 Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy, Sheet and Plate 5.6Zn 2.5Mg 1.6Cu 0.23Cr Annealed (7075-0) or when specified, As Fabricated (7075-F)

SAE AMS4063E-2008 1.25Mn 0.12Cu(No. 11-0铜焊薄板材)退火的铝合金单面涂覆薄板材

1.1 FormThis specification covers an aluminum alloy in the form of clad sheet.1.2 ApplicationThis sheet has been used typically for brazed assemblies which are not subject to heat treatment after joining, but usageis not limited to such applications.

Aluminum Alloy, Clad One Side, Sheet 1.25Mn 0.12Cu (No. 11-0 Brazing Sheet) Annealed

SAE AMS4235B-2008 溶解和沉淀热处理的4.6Cu 0.35Mn 0.25Mg 0.22Ti(A206.0-T71)铝合金铸件

This specification covers an aluminum alloy in the form of sand, permanent mold, and composite mold castings. This product has been typically used for components requiring high strength and moderate ductility at both room and elevated temperatures, but usage is not limited to such applications.

Aluminum Alloy Castings 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti (A206.0-T71) Solution and Precipitation Heat Treated UNS A12060

SAE AMS4215H-2008 溶解和沉淀热处理5.0Si1.2Cu0.50Mg(C355.0-T6)铝合金铸件

This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings. These castings have been used typically for components requiring good strength at room and elevated temperatures, but usage is not limited to such applications.

Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (C355.0-T6) Solution and Precipitation Heat Treated UNS A33550

SAE AMS2772E-2008 铝合金原材料的热处理

This specification covers requirements and recommendations for the heat treatment of wrought aluminum alloy raw materials by producers. It supersedes AMS-H-6088 and replaces MIL-H-6088. Aluminum alloy tempers are described in SAE AS1990 and ANSI H35.1 This specification may be used for alloys other than those specified herein providing temperatures, times, and quenchant are specified.

Heat Treatment of Aluminum Alloy Raw Materials

SAE AMS-QQ-A-200/4B-2008 挤压式铝合金5083条材,棒材,型材,管材和线材5083

This specification covers the specific requirements for aluminum alloy 5083 bar, rod, shapes, tube, and wire produced by extrusion.

Aluminum Alloy 5083, Bar, Rod, Shapes, Tube, and Wire, Extruded

SAE AMS4414-2008 7.5Zn 1.6Cu 1.5Mg 0.12Zr (7085-T7452)溶解热处理、压缩应力释放和老化的铝合金手工锻件

This specification covers an aluminum alloy in the form of hand forgings 12 inches (305 mm) and under in nominal thickness and forging stock. These forgings have been used typically for machined structural parts and requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such application.

Aluminum Alloy, Hand Forgings 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr (7085-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged UNS A97085

SAE AMS4274A-2008 4.4Cu 1.5Mg 0.60Mn (Alclad 2024-0)精细颗粒退火的铝合金包铝薄板材

This specification covers an aluminum alloy in the form of sheet. This sheet has been used typically for severely formed structured parts which will be subsequently heat treated and painted or otherwise protected from corrosion, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; SAE ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy, Alclad Sheet 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-0) Annealed, Fine Grain UNS A82024

SAE AMS4064F-2008 1.25Mn 0.12Cu (No. 12-0钎接金属片)退火的双面涂覆铝合金薄板材

This specification covers an aluminum alloy in the form of clad sheet. This sheet has been used typically for brazed assemblies which are not subject to heat treatment after joining, but usage is not limited to such applications.

Aluminum Alloy, Clad Two Sides Sheet 1.25Mn - 0.12Cu (No. 12-0 Brazing Sheet) Annealed UNS A83003

SAE AMS4412-2007 3.2Cu 0.52Mg 0.30Ag 0.12Zr (2198-T8)溶解热处理、冷加工和人工老化的铝合金薄板材

This specification covers an aluminum alloy in the form of sheet. This product has been used for aircraft applications where it offers a combination of high strength and low density, but usage is not limited to such applications.

Aluminum Alloy, Sheet, 3.2Cu 0.52Mg 0.30Ag 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged

DIN EN 4002:2007 航空航天系列.AL-P2219-T81型铝合金.薄板材和带材.0.5mm≤a≤6mm

Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm ≤ a ≤ 6 mm; German and English version EN 4002:2007

DIN EN 3999:2007 航空航天系列.AL-P2024-T351型铝合金.改进化学铣削性能的镀铝薄板材和带材.1.6mm≤a≤6mm

Aerospace series - Aluminium alloy AL-P2024-T351 - Sheet and strip with improved chemical milling capability 1,6 mm ≤ a ≤ 6 mm; German and English version EN 3999:2007

KS W 1140-2007(2017) 铝和铝合金化学转化涂层

Chemical conversion coatings on aluminum and aluminum alloys

KS W 1140-2007 航空航天取代薄膜铝和铝合金

이 표준은 화학치환 물질과 알루미늄 및 알루미늄 합금 표면의 반응으로 형성된 2가지 등급의

Chemical conversion coatings on aluminum and aluminum alloys

KS W 1140-2007(2022) 铝和铝合金上的化学转化涂层

Chemical conversion coatings on aluminum and aluminum alloys

BS EN 3999:2007 航空航天系列.AL-P2024-T351型铝合金.改进的化学铣削性能1.6 mm≤a≤6 mm的薄板材和带材

This standard specifies the requirements relating to: Aluminium alloy AL-P2024-T351 — Sheet and strip with improved chemical milling capability 1,6 mm ≤ a ≤ 6 mm for aerospace application. This material is manufactured to a minimum residual stress requirement for chemical milling applications.

Aerospace series - Aluminium alloy AL-P2024-T351 - Sheet and strip with improved chemical milling capability 1,6 mm a 6 mm

BS EN 4002:2007 航空航天系列.AL-P2219-T81型铝合金.0.5 mm≤a≤6 mm的薄板材和带材

This standard specifies the requirements relating to: Aluminium alloy AL-P2219-T81 — Sheet and strip 0,5 mm ≤ a ≤ 6 mm for aerospace applications.

Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm a 6 mm

DS/EN 3999:2007 航空航天系列 铝合金 AL-P2024-T351 具有改进的化学铣削能力的板材和带材 1,6 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P2024-T351 - Sheet and strip with improved chemical milling capability 1,6 mm

Aerospace series - Aluminium alloy AL-P2024-T351 - Sheet and strip with improved chemical milling capability 1,6 mm <= a <= 6 mm

DS/EN 4002:2007 航空航天系列 铝合金 AL-P2219-T81 板材和带材 0,5 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm

Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm <= a <= 6 mm

SAE AMS-QQ-A-200/6B-2007 挤压式铝合金5454条材,棒材,型材,管材和线材

This specification covers the specific requirements for aluminum alloy 5454 bar, rod, shapes, tube, and wire produced by extrusion.

Aluminum Alloy 5454, Bar, Rod, Shapes, Tube, and Wire, Extruded