49.025.20 铝 标准查询与下载

SAE AMS4241D-2009 枝晶叉间隔(DAS)控制的溶液和沉淀热处理的7.0Si 0.58Mg 0.15Ti 0.06Be(D357.0-T6)铝合金铸件

This specification covers an aluminum alloy in the form of sand castings. These castings have been used typically for structural aircraft components requiring DAS quality control, but usage is not limited to such applications.

Aluminum Alloy Castings 7.0Si 0.58Mg 0.15Ti 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled

SAE AMS2658C-2009 锻造铝合金部分的硬度和导电性检验

This specification establishes hardness and electrical conductivity acceptance criteria of finished or semi-finished parts of wrought aluminum alloys. This specification has been used typically for nondestructive testing of wrought aluminum alloy parts to aid in determining correctness of alloy, temper, and/or heat treatment, but usage is not limited to such applications.

Hardness and Conductivity Inspection of Wrought Aluminum Alloy Parts

SAE AMS4079G-2009 拉伸的圆形无缝铝合金配管1.0Mg 0.06Si 0.28Cu 0.20Cr (6061-0)精密公差,煅烧

This specification covers an aluminum alloy in the form of drawn, round, seamless tubing. This tubing has been used typically for ducts requiring small radius bends and moderate strength after solution and precipitation heat treatment, but usage is not limited to such applications.

Aluminum Alloy, Drawn, Round, Seamless, Tubing 1.0Mg 0.06Si 0.28Cu 0.20Cr (6061-0) Close Tolerance, Annealed

SAE AMS4004D-2009 铝合金箔2.5 Mg 0.25Cr(5052-H191)应变硬化

This specification covers an aluminum alloy in the form of foil. This foil has been used typically for corrugated or expanded honeycomb core material for use in sandwich construction, but usage is not limited to such applications.

Aluminum Alloy, Foil 2.5 Mg 0.25Cr (5052-H191) Strain Hardened

SAE AMS4470-2009 固溶热处理,消除应力和过老化的7.5Zn-1.6Cu-1.5Mg-0.12Zr铝合金板(7085-T7451)

This specification covers an aluminum alloy in the form of plate. This product may be used in aerospace applications requiring a high level of mechanical properties and fracture toughness, good resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.

Aluminum Alloy, Plate (7085-T7451) 7.5Zn 1.6Cu 1.5Mg 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged

SAE AMS4077G-2009 淬火单面包铝层4.4Cu-1.5Mg-0.60Mn铝合金片材和板材(单面包层2024-0)

This specification covers an aluminum alloy in the form of sheet and plate. This product has been used typically for structural components, including machine tapered parts, but usage is not limited to such applications.

Aluminum Alloy Sheet and Plate, Alclad One Side 4.4Cu 1.5Mg 0.60Mn (Clad One Side 2024-0) Annealed

BS EN 2116:2009 航空航天系列.铝合金2017A-T42.实心铆钉用线材.D≤10 mm

This standard specifies the requirements relating to: Aluminium alloy 2017A-T42 Wire for solid rivets D ≤ 10 mm for aerospace applications.

Aerospace series - Aluminium alloy 2017A-T42 - Wire for solid rivets - D 10 mm

BS EN 2115:2009 航空航天系列.铝合金2117-T42.实心铆钉用线材.D≤10 mm

This standard specifies the requirements relating to: Aluminium alloy 2117-T42 Wire for solid rivets D ≤ 10 mm for aerospace applications.

Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D 10 mm

BS EN 3115:2009 航空航天系列.铝合金7050-T73.实心铆钉用线材.D≤10 mm

This standard specifies the requirements relating to: Aluminium alloy 7050-T73 Wire for solid rivets D ≤ 10 mm for aerospace applications.

Aerospace series - Aluminium alloy 7050-T73 - Wire for solid rivets - D 10 mm

BS EN 2117:2009 航空航天系列.铝合金AL-P5056A(5056A)-H32.实心铆钉线材.D≤10 mm

This standard specifies the requirements relating to: Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D ≤ 10 mm for aerospace applications.

Aerospace series - Aluminium alloy AL-P5056A (5056A)-H32 - Wire for solid rivets - D 10 mm

SAE AMS4304B-2009 固溶热和脱溶热处理的拉伸的非连续加强铝合金薄板2009/SiC/15W(T8P)

This specification covers discontinuously reinforced aluminum alloy (DRA) metal matrix composites (MMC) in the form of sheet. This sheet has been used typically for structural applications requiring high static strength, moderate fatigue strength, and high elastic modulus, but usage is not limited to such applications.

Aluminum Alloy, Discontinuously Reinforced Sheet 2009/SiC/15W (T8P) Solution Heat Treated, Stretched, and Precipitation Heat Treated

SAE AMS4465-2009 0.6Mg-0.35Si-0.28Cu焊接的单面涂层预制铝合金薄板(23号钎焊板)

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

Aluminum Alloy, Clad One Side Sheet 0.6Mg 0.35Si 0.28Cu (No. 23 Brazing Sheet) As Fabricated

SAE AMS4460-2009 0.6Mg-0.35Si-0.28Cu焊接用预制铝合金外覆双面板(24号钎焊板)

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

Aluminum Alloy, Clad Two Sides Sheet 0.6Mg 0.35Si 0.28Cu (No. 24 Brazing Sheet) As Fabricated

SAE AMS4125K-2009 固溶热处理和脱溶热处理的铝合金模锻件和滚压或锻造环材0.90Si - 0.62Mg - 0.25Cr, (6151-T6)

This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. NONCURRENT refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. NONCURRENT specifications are available from SAE upon request.

Aluminum Alloy Die Forgings, and Rolled or Forged Rings, 0.90Si - 0.62Mg - 0.25Cr, (6151-T6) Solution and Precipitation Heat Treated

SAE AMS-QQ-A-591A-2009 铝合金压模铸件

This specification covers aluminum alloy die castings.

Aluminum Alloy Die Castings

SAE AMS4130M-2009 固溶和脱溶热处理的铝合金模锻件4.4Cu - 0.85Si - 0.80Mn (2025-T6)

This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. NONCURRENT refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. NONCURRENT specifications are available from SAE upon request.

Aluminum Alloy Die Forgings, 4.4Cu - 0.85Si - 0.80Mn (2025-T6), Solution and Precipitation Heat Treated

SAE AMS4140J-2009 固溶及沉淀热处理的4.0Cu-2.0Ni-0.68Mg(2018-T61)铝合金型锻

This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. NONCURRENT refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. NONCURRENT specifications are available from SAE upon request.

Aluminum Alloy Die Forgings, 4.0Cu - 2.0Ni - 0.68Mg (2018-T61), Solution and Precipitation Heat Treated

DIN EN 2117:2009 航空航天系列.铝合金AL-P5056A(5056A)-H32.实心铆钉用线材.D 10毫米,德文版本和英文版本EN 2117:2009

This standard specifies the requirements relating to: Aluminium alloy AL-P5056A (5056A)-H3 Wire for solid rivets D 10mm for aerospace applications.

Aerospace series - Aluminium alloy AL-P5056A (5056A)-H32 - Wire for solid rivets - D 10 mm; German and English version EN 2117:2009

DIN EN 2115:2009 航空航天系列.铝合金2117-T42.实心铆钉用线材.D 10 mm,德文版本和英文版本EN 2115:2009

This standard specifies the requirements relating to: Aluminium alloy 2117-T42 Wire for solid rivets D 10mm for aerospace applications.

Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D 10 mm; German and English version EN 2115:2009

SAE AMS4117J-2009 溶液和沉淀热处理1.0Mg-0.60Si-0.28Cu-0.20Cr(6061.-T6,-T651)滚轧或冷加工铝合金棒材,杆材,线材和闪速对焊环

This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire and of flash welded rings and stock for flash welded rings. These products have been used typically for parts requiring moderate strength where limited formability is acceptable, but usage is not limited to such applications.

Aluminum Alloy, Rolled or Cold Finished Bars, Rods, and Wire and Flash Welded Rings 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061; -T6, -T651) Solution and Precipitation Heat Treated