49.025.20 铝 标准查询与下载

SAE AMS4041Q-2007 单侧包铝的铝合金薄板材和厚板材4.4Cu 1.5Mg 0.6Mn、单侧包铝的2024平板材、1-1/2%单侧包铝的2024-T3平板材.1-1/2%单侧包铝的2024-T351厚板材

This specification covers an aluminum alloy in the form of sheet and plate clad on both sides with a different aluminum alloy. These products have been used typically for formed structural components requiring good strength and maximum corrosion resistance, but usage is not limited to such applications. Plate is also suitable for structural machined parts where warpage, during machining, due to residual stresses must be minimized. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy, Alclad Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn Alclad 2024 and 1-1/2% Alclad 2024, -T3 Flat Sheet; 1-1/2% Alclad 2024-T351 Plate [Superseded: SAE AMS 4034C]

SAE ARP1947B-2007 航空器结构质量D357型铝合金铸件枝状晶体分支间距的测定和验收

This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50,000 psi (345 MPa). To apply this method, at least two coupons used for DAS measurement and tensile testing, shall be attached to the casting in locations as defined by the cognizant engineering organization. Areas of the casting which require DAS control must be accessible for surface DAS measurements.

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of

SAE AMS4342E-2007 6.2Zn 2.3Cu 2.2Mg 0.12Zr (7050-T74511)溶解热处理、应力消除、拉直和过度老化的铝合金挤压型材

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These product have been used typically for structural applications requiring a combination of high mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T74511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged UNS A97050

SAE AMS4311E-2007 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T7351、7075-T352)溶解热处理、机械应力释放和沉淀热处理的铝合金轧制或锻制环材

This specification covers an aluminum alloy in the form of rolled or forged rings. These rings have been used typically for applications requiring a combination of high strength, resistance to stress-corrosion cracking, and good stability during machining, but usage is not limited to such applications. Rings covered by this specification are classified by type of mechanical stress relief as follows: Type 1 - Stress-relieved by stretching (7075-T7351); and Type II - Stress-relieved by compression (7075-T7352). Either type may be supplied, unless a specific type is ordered.

Aluminum Alloy, Rolled or Forged Rings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7351, 7075-T7352) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated UNS A97075

NF L14-220:2007 航空航天系列.AL-P2024-T3型铝合金.薄板材和带材.0.4mm≤a≤6mm

Aerospace series - Aluminium alloy AL-P2024-T3 - Sheet and strip - 0,4 mm < or = a < or = 6 mm.

SAE AMS4338A-2007 4.0Cu 1.3Mg 0.60Mn (2026-T3511)通过拉伸进行溶解热处理和应力释放的铝合金挤压制品

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes). These extrusions have been used typically for machined parts requiring dimensional stability during machining processes and for parts requiring high strength and damage tolerance, where fabrication does not normally involve welding, but usage is not limited to such applications. Certain processing procedures may cause this product to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy, Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching UNS A92026

SAE AMS4143E-2007 6.3Cu 0.3Mn 0.18Zr 0.10V 0.06Ti (2219-T6)溶解热处理和沉淀热处理的铝合金锻件和轧制或锻制环材

This specification covers an aluminum alloy in the form of die forgings, hand forgings, forged rings, rolled rings, and stock for forging or rings. These products have been used typically for structural, machined parts but usage is not limited to such applications. This material may be welded in the T6 condition but properties are improved by heat treatment after welding. Certain design and fabricating procedures may cause these products to become susceptible to stress-corrosion cracking; ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy Forgings and Rolled or Forged Rings 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T6) Solution and Precipitation Heat Treated UNS A92219

SAE AMS4242B-2007 4.7Cu 0.60Ag 0.35Mn 0.25Mg 0.25Ti(B201.0-T7)溶解热处理和老化的铝合金铸件

This specification covers an aluminum alloy in the form of castings. These castings have been used typically for aircraft components requiring high strength and reliability, both at room and elevated temperatures, but usage is not limited to such applications. Alloy B201.0, the alloy designated in this specification, has restricted composition within the limits of alloy A201.0.

Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged

DIN EN 4001:2007 航空航天系列.AL-P2024-T351型铝合金.改进的化学铣削性能1.6mm≤a≤6mm的镀铝薄板材和带材

This standard specifies the requirements relating to： Aluminium alloy AL—P2024-T351一Clad sheet and strip with improved chemical milling capability 1,6 mm≤a ≤6 mm for aerospace applications． The material is manufactured to a minimum residual stress requirement for chemical milling applications.

Aerospace series - Aluminium alloy AL-P2024-T351 - Clad sheet and strip with improved chemical milling capability 1,6 mm ≤ a ≤ 6 mm; German and English version EN 4001:2007

DIN EN 2089:2007 航空航天系列.AL-P2014A-T6或T62型铝合金.薄板材和带材.0.4mm≤a≤6mm

This standard specifies the requirements relating to: Aluminium alloy AL-P201A T6 or T62 Sheet and strip 0,4 mm≤a≤6 mm for aerospace application.

Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 2089:2005

DIN EN 4005:2007 航空航天系列.AL-P5052-0型铝合金.0.3mm≤a≤6mm的薄板材和带材

This standard specifies the requirements relating to Aluminium alloy AL-P5052-O——Sheet and strip 0,3 mm≤a≤6 mm for aerospace applications．

Aerospace series - Aluminium alloy AL-P5052-O - Sheet and strip 0,3 mm ≤ a ≤ 6 mm; German and English version EN 4005:2007

DIN EN 3998:2007 航空航天系列.AL-P2024-T4或T42型铝合金.0.3mm≤a≤6mm的薄板材和带材

This standard specifies the requirements relating to： Aluminium alloy AL-P2024一T4 or T42一Sheet and strip 0,3 mm≤a≤6 mm for aerospace application.

Aerospace series - Aluminium alloy AL-P2024-T4 or T42 - Sheet and strip 0,3 mm ≤ a ≤ 6 mm; German and English version EN 3998:2007

DIN EN 4006:2007 航空航天系列.AL-P6082-T4或T42型铝合金.0.4mm≤a≤6mm的薄板材和带材

This standard specifies the requirements relating to： Alumlnlum alloy AL-P6082-T4 or T42-Sheer and strip 0,4 mm ≤ a ≤ mm for aerospace applications.

Aerospace series - Aluminium alloy AL-P6082-T4 or T42 - Sheet and strip 0,4 mm ≤ a ≤ 6 mm; German and English version EN 4006:2007

DIN EN 3997:2007 航空航天系列.AL-P2024-T3型铝合金.0.4mm≤a≤6mm的薄板材和带材

This standard specifies the requirements relating to: Aluminium alloy AL-P2024-T3-Sheet and strip O，4 mm≤a≤6 mm for aerospace application．

Aerospace series - Aluminium alloy AL-P2024-T3 - Sheet and strip 0,4 mm ≤ a ≤ 6 mm; German and English version EN 3997:2007

DIN EN 4004:2007 航空航天系列.AL-P3103-H16型铝合金.0.4mm≤a≤6mm的薄板材和带材

This standard specifies the requirements relating to： Aluminium alloy AL—P3103-H16一sheet and strip 0,4 mm ≤a ≤6 mm for aerospace applications．

Aerospace series - Aluminium alloy AL-P3103-H16 - Sheet and strip 0,4 mm ≤ a ≤ 6 mm; German and English version EN 4004:2007

DIN EN 2085:2007 航空航天系列.AL-P2618A-T6型铝合金.自由锻件和模锻件.a≤150mm

This standard specifies the requirements relating to: Aluminium alloy AL-P2618A-T6 Hand and die forgings a≤150 mm for aerospace application.

Aerospace series - Aluminium alloy AL-P2618A-T6 - Hand and die forgings - a≤ 150 mm; German and English version EN 2085:2004

SAE AMS-QQ-A-200/7B-2007 铝合金5456条,棒,型材,管材,以及线材,挤出物

This specification covers the specific requirements for aluminum alloy 5456 bar, rod, shapes, tube, and wire produced by extrusion.

Aluminum Alloy 5456, Bar, Rod, Shapes, Tube, and Wire, Extruded

SAE AMS-QQ-A-200/5A-2007 铝合金5086棒材,杆材,型材,管材,以及线材,挤出物

This specification covers the specific requirements for aluminum alloy 5086 bar, rod, shapes, tube, and wire produced by extrusion.

Aluminum Alloy 5086, Bar, Rod, Shapes, Tube, and Wire, Extruded

SAE AMS4111D-2007 7.7Zn 2.5Mg 1.5Cu 0.16Cr溶解热处理和沉淀热处理的铝合金锻件

This specification covers an aluminum alloy in the form of die forgings, hand forgings, and forging stock. These bars have been typically for parts requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy Forgings 7.7Zn - 2.5Mg - 1.5Cu - 0.16Cr (7049-T73) Solution and Precipitation Heat Treated UNS A97049

SAE AMS4225D-2007 溶解热处理和稳定化处理的5.0Cu 1.5Ni 0.25Mn 0.25Sb 0.25Co 0.20Ti 0.20Zr铸件用耐高温铝合金

This specification covers an aluminum alloy in the form of castings. These castings have been used typically for components requiring moderate strength and good stability up to 600 °F (316 °C) with resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy, Heat-Resistant, Castings 5.0Cu - 1.5Ni - 0.25Mn - 0.25Sb - 0.25Co - 0.20Ti - 0.20Zr (203.0-T6) Solution Heat Treated and Precipitation Heat Treated