49.025.20 铝 标准查询与下载

SAE AMS4600-2011 固溶热处理,冷加工(8%)和自然老化(2219 - T37)含6.3Cu-0.30Mn-0.06Ti-0.10V-0.18Zr铝合金薄板和板材

This specification covers an aluminum alloy in the form of sheet and plate. This product form has been used typically for structural parts requiring high strength up to 500 °F (260 °C) after proper precipitation heat treatment and which may require forming or welding during fabrication, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy, Sheet and Plate 6.3Cu 0.30Mn 0.06Ti 0.10V 0.18Zr Solution Heat Treated, Cold Worked (8%) and Naturally aged (2219 - T37)

SAE AMS4599-2011 溶解沉淀热处理工艺制备的6.3Cu-0.30Mn-0.06Ti-0.10V-0.18Zr铝合金薄板和厚板(2219-T81/-T851)

This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for parts requiring high strength up to 500 φF (260 φC), but usage is not limited to such applications. Product may be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy, Sheet and Plate 6.3Cu 0.30Mn 0.06Ti 0.10V 0.18Zr Solution and Precipitation Heat Treated (2219-T81/-T851)

SAE AMS4617-2011 5.6Zn-2.5Mg-1.6Cu-0.23Cr铝合金挤压制品(7075-T73,7075-T73511,7075-T73510)

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing These extrusions have been used typically for parts subject to excessive warpage during machining and for parts requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy, Extrusions 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T73, 7075-T73511, 7075-T73510)

SAE AMS4613-2011 溶解热处理,冷加工(8%)和沉淀热处理工艺制备的6.3Cu-0.30Mn-0.06Ti-0.10V-0.18Zr铝合金薄板和厚板(2219-T87)

This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for parts requiring high strength up to 500 φF (260 φC), but usage is not limited to such applications. Material may be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy, Sheet and Plate 6.3Cu 0.30Mn 0.06Ti 0.10V 0.18Zr Solution Heat Treated, Cold Worked (8%) and Precipitation Heat Treated (2219-T87)

SAE AMS3673C-2011 硅橡胶背铝面玻璃布

This specification covers one type of glass cloth coated on one face with aluminum and the other face with silicone rubber. Primarily for use as a thermal curtain for protection of personnel and equipment from short-time exposure to high intensity thermal radiation.

Cloth, Glass, Aluminum Face, Silicone Rubber Back

SAE AMS4472-2011 经过热溶解处理和重压过的4.0Cu 1.oLi 0.40Mg 0.35Ag 0.132Zr(2195-T34)铝合金板

This specification covers an aluminum alloy in the form of plate. This plate has been used typically for aerospace structural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications. Material is delivered in T34 temper and precipitation heat treated to obtain T82 temper by the end user.

Aluminum Alloy, Plate 4.0Cu 1.oLi 0.40Mg 0.35Ag 0.132Zr (2195-T34) Solution Heat Treated and Stress Relieved

SAE AMS7909B-2011 38AI - 62Be NNS预成型等静热压铝铍

This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of blocks, blanks or shapes. These performs have been used typically for parts requiring high thermal conductivity, low density and high modulus of elasticity, but usage is not limited to such applications.

Aluminum Beryllium, NNS Preforms Hot Isostatic Pressed 38Al - 62Be

SAE AMS4085D-2011 经固溶处理和过老化的5.7Zn 2.2Mg 1.6Cu 0.22Cr(7475- T761)铝合金板材

This specification covers an aluminum alloy in the form of sheet. This product has been used typically for structural applications applications requiring sheet with high strength and resistance to exfoliation-corrosion, moderate fatigue strength, and high fracture-toughness, but usage is not limited to such applications.

Aluminum Alloy Sheet 5.7Zn 2.2Mg 1.6Cu 0.22Cr (7475-T761) Solution Heat Treated and Overaged

SAE AMS-B-20148B-2011 铝合金钎焊板

This specification covers aluminum alloy brazing sheet for use in brazed aluminum joints.

Brazing Sheet, Aluminum Alloy

SAE AMS4154P-2011 经固溶处理以及必要时的拉伸解除应力和沉淀热处理的 5.6Zn 2.5Mg 1.6Cu 0.23Cr(7075 - T6,7075,7075 - T6511 T6510)铝合金挤压件

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing. These extrusions have been used typically for parts requiring high strength and whose fabrication does not usually involve welding or forming, but usage is not limited to such applications.

Aluminum Alloy, Extrusions 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T6, 7075-T6510, 7075-T6511) Solution Heat Treated, Stress Relieved by Stretching when Required and Precipitation Heat Treated

SAE AMS4285E-2011 溶解和沉淀热处理7.0Si 0.3Mg (356.0-T6)离心铝合金铸件

This specification covers an aluminum alloy in the form of centrifugal castings. These castings have been used typically for intricate castings with thin walls or sections used at relatively high stresses, but usage is not limited to such applications.

Aluminum Alloy Castings, Centrifugal, 7.0Si 0.3Mg (356.0-T6) Solution and Precipitation Heat Treated

SAE AMS4221D-2011 铝合金板 4.4Cu 1.5mg 0.60Mn(2124-T8151)解决方案热处理,消除应力和沉淀热处理

This specification covers an aluminum alloy in the form of plate 1.5 inches (38 mm) and over in nominal thickness. This plate has been used typically for parts requiring a high level of mechanical properties up to 300 °F (149 °C), but usage is not limited to such applications. Certain design and fabrication procedures may cause plate to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy, Plate 4.4Cu 1.5Mg 0.60Mn (2124-T8151) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

SAE AMS4183A-2011 铝合金型材,控制叶型(2027-T3511)4.4Cu 1.2Mg 0.8Mn 0.10Zr固溶处理及拉伸解除应力

This specification covers an aluminum alloy in the form of extruded profiles.

Aluminum Alloy, Extruded Profiles (2027-T3511) 4.4Cu 1.2Mg 0.8Mn 0.10Zr Solution Heat Treated and Stress Relieved by Stretching

SAE AMS4213A-2011 (2027-T351)4.4Cu 1.2Mg 0.8Mn 0.10Zr溶解热处理,冷轧和自然终产物的铝合金板

This specification covers an aluminum alloy in the form of plate.

Aluminum Alloy Plate (2027-T351) 4.4Cu - 1.2Mg - 0.8Mn - 0.10Zr Solution Heat Treated, Cold Worked and Naturally Aged

SAE AMS2355K-2011 铝合金和镁合金锻造(除锻坯外)和轧制产品,锻造或闪速对焊环的抽样和测试质量保证

This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought aluminum alloy and wrought magnesium alloy mill products (except forging stock), and includes quality assurance and testing procedures for rolled, forged, and flash welded rings. Requirements are specified in inch/pound units.

Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings

SAE AMS4284J-2011 永久模7.0Si-0.30Mg (355.0-T6)固溶和沉淀热处理铝合金铸件

This specification covers an aluminum alloy in the form of permanent mold castings. These castings have been used typically for components requiring low weight, moderate strength, and soundness, but usage is not limited to such applications.

Aluminum Alloy Castings, Permanent Mold 7.0Si - 0.30Mg (356.0-T6) Solution and Precipitation Heat Treated

SAE AMS-A-22771B-2011 热处理铝合金铸件

This specification has previously been widely used and may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, considers this specification non-current and does not recommend this specification for future use in new designs. This specification covers the requirements for heat treated aluminum alloy die forgings, hand forgings, and ring forgings, produced under additional mechanical property control to ensure known mechanical properties for parts used in aerospace critical applications. This specification also covers the requirements for forgings furnished in the F or 01 conditions which will ultimately be used in the heat treated condition.

Aluminum Alloy Forgings, Heat Treated

SAE AMS4229E-2011 高强度铝合金铸件4.5Cu 0.70Ag 0.30Mn 0.25Mg 0.25Ti (A201.0-T7),热处理和应用解决方案

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

Aluminum Alloy Castings, High Strength 4.5Cu 0.70Ag 0.30Mn 0.25Mg 0.25Ti (A201.0-T7) Solution Heat Treated and Overaged

SAE AMS4212K-2011 铝合金铸件5.0Si 1.2Cu 0.50Mg(355.0-T6),固溶和降水热处理

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

Aluminum Alloy Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated (UNS A03550)

SAE AMS4078H-2010 过度老化,应力消失,溶解热处理5.6Zn-2.5Mg-1.6Cu-0.23Cr 7075 (-T73片材 -T7351板材)铝合金片和板材

This specification covers an aluminum alloy in the form of plate. This plate has been used typically for machined parts subject to excessive warpage during machining due to residual stresses and for parts requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy Sheet and Plate 5.6Zn 2.5Mg 1.6Cu 0.23Cr 7075 (-T73 Sheet -T7351 Plate) Solution Heat Treated, Stress Relieved, and Overaged