49.025.20 铝 标准查询与下载

SAE AMS4178D-2006 夹层结构用5052、350 (177)处理的柔性蜂窝铝合金芯

This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form. This honeycomb core has been used typically in contoured sandwich construction for short-term service up to 350 °F (177 °C) or for long-term service up to 200 °F (93 °C), but usage is not limited to such applications.

Core, Flexible Honeycomb, Aluminum Alloy, Treated, For Sandwich Construction, 5052, 350 (177)

SAE AMS4177D-2006 夹层结构用5052、350 (177)处理的柔性蜂窝铝合金芯

This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form. This honeycomb core has been used typically in contoured sandwich construction for short-term service up to 350 °F (177 °C) or for long-term service up to 200 °F (93 °C), but usage is not limited to such applications.

Core, Flexible Honeycomb, Aluminum Alloy For Sandwich Construction 5056, 350 (177)

SAE AMS4341E-2006 用拉伸、拉直和覆盖法释放应力的(7050-T73511)6.2Zn 2.3Cu 2.2Mg 0.12Zr溶液热处理的铝合金挤压型材

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. This product has 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-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged UNS A97050

SAE AMS4340E-2006 通过拉直和覆盖释放应力的6.2Zn 2.3Cu 2.2Mg 0.12Zr溶液热处理铝合金挤压型材

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

Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T76511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged UNS A97050

SAE AMS4349D-2006 5056、350 (177)夹层结构用耐腐铝合金蚀蜂巢芯

This specification covers one type of honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered. This honeycomb core has been used typically in sandwich construction for short-term exposure up to 350 °F (177 °C) or for long-term exposure up to 200 °F (93 °C), but usage is not limited to such applications.

Core, Honeycomb, Aluminum Alloy, Corrosion Inhibited for Sandwich Construction, 5056, 350 (177)

SAE AMS4344C-2006 用拉伸、拉直和覆盖法释放应力的(7175-T73511)5.6Zn 2.5Mg 1.6Cu 0.23Cr溶液热处理的铝合金挤压型材

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles. These extrusions have been used typically for structural applications requiring a combination of high tensile properties, moderate fatigue strength, stress-corrosion resistance, and good fracture toughness, but usage is not limited to such applications.

Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Staightened,, and Overaged UNS A97175

SAE AMS4337A-2006 通过拉直和覆盖释放应力的(7055-T77511) 8.0Zn 2.3Cu 2.0Mg 0.16Zr 溶液热处理铝合金挤压型材

This specification covers an aluminum alloy in the form of extruded profiles (shapes). This product has been used typically for structural applications requiring a combination of high mechanical properties and good resistance to exfoliation corrosion, but usage is not limited to such applications.

Aluminum Alloy, Extruded Profiles (7055-T77511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged UNS A97055

SAE AMS4248B-2006 通过加压释放应力和沉淀热处理的1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T652)溶液热处理铝合金手工铸件和卷形环材

This specification covers an aluminum alloy in the form of hand forgings and rolled rings. These products have been used typically for complex shaped parts requiring moderate strength and good forgeability of the alloy and where stability is required during machining, but usage is not limited to such applications. Corrosion resistance of this alloy is superior to that of aluminum alloys having copper as the principal alloying element.

Aluminum Alloy, Hand Forgings and Rolled Rings 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T652) Solution Heat Treated, Stress Relief by Compression, and Precipitation Heat Treated

SAE AMS4348D-2006 5052、350 (177)夹层结构用耐腐蚀蜂巢铝合金芯

This specification covers bonded honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered. This honeycomb core has been used typically in sandwich construction for short-term exposure up to 350 °F (177 °C) or for long-term exposure up to 200 °F (93 °C), but usage is not limited to such applications.

Core, Honeycomb, Aluminum Alloy, Corrosion Inhibited for Sandwich Construction 5052, 350 (177)

SAE AMS4044K-2006 装配的(7075-F)和退火的(7075-0)5.6Zn 2.5Mg 1.6Cu 0.23Cr铝合金薄板材和厚板材或按另行规定

This specification covers an aluminum alloy in the form of sheet and plate supplied in the annealed (0) condition. These products have been used typically for formed structural parts which will be subsequently heat treated, 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; 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 AMS4148E-2006 溶液和沉淀热处理的铝合金型锻件(7175-T66)

This specification covers an aluminum alloy in the form of die forgings and forging stock.

Aluminum Alloy Die Forgings (7175-T66) Solution and Precipitation Heat Treated

SAE AMS4028G-2006 退火铝合金片材和板材4.4Cu 0.85Si 0.80Mn 0.50Mg

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

Aluminum Alloy Sheet and Plate, 4.4Cu - 0.85Si - 0.80Mn - 0.50Mg, Annealed

SAE AMS4401-2006 固溶热处理、应力消除和过老化铝合金板材(7140-T7451) 6.6Zn 1.8Cu 2.0Mg 0.10Zr

This specification covers an aluminum alloy in the form of plate. This product has been used typically for parts requiring a high level of mechanical properties and fracture toughness with good resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy Plate (7140-T7451) 6.6Zn - 1.8Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved and Overaged

SAE AMS4207B-2006 溶液和沉淀热处理的铝合金包铝片材5.7Zn 2.2Mg 1.6Cu 0.22Cr (7454-T61)

This specification covers an aluminum alloy in the form of sheet. Primarily for structural applications requiring a combination of high strength, moderate fatigue strength, and high fracture toughness.

Aluminum Alloy Sheet, Alclad 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475- T61) Solution and Precipitation Heat Treated

SAE AMS4403-2006 固溶热处理、压缩应力消除和过老化铝合金模锻件7.5Zn 1.6Cu 1.5Mg 0.12Zr (7085-T7452)

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

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

SAE AMS4405-2006 溶液热处理和自然老化的铝合金包铝的薄板(6156-T4) 1.0Si 0.90Cu 0.60Mn 0.90Mg

This specification covers an aluminum alloy procured in the form of sheet Alclad on both sides. These products have been used typically for formed structural parts requiring good formability in T4 temper and ability to develop improved resistance to fatigue crack growth and high toughness with moderate strength when aged to T62 temper, but usage is not limited to such applications.

Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged

SAE AMS4206A-2006 溶液热处理、应力释放和过度老化的铝合金板材(7055-T7751) 8.0Zn 2.3Cu 2.0Mg 0.16Zr

This specification covers an aluminum alloy in the form of plate. This product has typically been used for parts requiring a high level of mechanical properties and moderate exfoliation corrosion resistance, but usage is not limited to such applications.

Aluminum Alloy, Plate (7055-T7751) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged UNS A97055

SAE AMS2770H-2006 锻造铝合金零件的热处理

This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors. It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper. It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2048, 2117, 2124, 2219, 3003, 5052, 6013, 6061, 6063, 6066, 6951,7049, 7050, 7075, 7149, 7178, 7475. This specification may be used for heat treatment of parts made from other alloys provided that temperature, temperature uniformity tolerances, times, and quenchants are specified or approved by the cognizant engineering organization.

Heat Treatment of Wrought Aluminum Alloy Parts [Superseded: SAE AMS-H-6088C, SAE AMS-H-6088B, SAE AMS-H-6088A, SAE AMS-H-6088]

DIN EN 4287:2006 航空航天系列.铝合金AL-P7010.锻坯

This standard specifies the requirements relating to: Aluminium alaloy AL-P7010 - Forging stock for aerospace applications.

Aerospace series - Aluminium alloy AL-P7010 - Forging stock; German and English version EN 4287:2005

NAVY MIL-DTL-5541 F-2006 铝和铝合金的化学转变外壳

This specification covers chemical conversion coatings formed by the reaction of chemical conversion materials with the surfaces of aluminum and aluminum alloys.

CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS