49.025.20 铝 标准查询与下载

SAE AMS4152M-2007 4.4Cu 1.5Mg 0.60Mn溶解热处理的铝合金挤压件

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing. Primarily for parts requiring good strength and whose fabrication does not involve welding, but usage is not limited to such applications. Certain processing procedures may cause these products to be susceptible to stress-corrosion cracking; ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated UNS A92024

DIN EN 2632:2007 航空航天系列.铝合金AL-P7075-T73511.挤压棒材和型材.带周边粗晶粒控制的.a或D≤100mm

This standard specifies the requirements relating to: Aluminium alloy AL-P7075-T73511, extruded bar and section a or D 150 mm with peripheral coarse grain controlfor aerospace application. This standard may also be used to supply material in the T73510 condition if specified by the purchaser on the order and the product is marked accordingly.#,,#

Aerospace series - Aluminium alloy AL-P7075-T73511 - Extruded bar and section - a or D 150 mm with peripheral coarse grain control; German and English version EN 2632:2005

DIN EN 2088:2007 航空航天系列.AL-P2014A-T4或T42型铝合金铠装薄材和带材.0.4mm≥a≥6mm

Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Clad sheet and strip - 0,4 mm a 6 mm; German and English version EN 2088:2005

BS EN 3339:2007 航空航天系列 AL-P7010-T76型铝合金 压模锻件 a≤200mm

Aerospace series - Aluminium alloy AL-P7010-T76 - Die Forgings - a 200 mm

BS EN 3339:2006 航空航天系列.AL-P7010-T76型铝合金.压模锻件.a≤200mm

This standard specifies the requirements relating to: Aluminium alloy AL-P7010- T76 Die forgings a ≤ 200 mm for aerospace applications.

Aerospace series — Aluminium alloy AL-P7010- — T76 — Die forgings — a u 200 mm

SAE AMS4407-2007 老化、应力释放和溶解热处理的9.1Zn 1.6Cu 1.9Mg铝合金板材(7056-T7651)

This product has been used typically for parts requiring high mechanical properties and fracture toughness, coupled with moderate stress corrosion and exfoliation corrosion resistance but usage is not limited to such applications.

Aluminum Alloy, Plate (7056-T7651) 9.1Zn - 1.6Cu - 1.9Mg Solution Heat Treated, Stress Relieved, and Overaged UNS A97056

SAE AMS4122K-2007 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T6)溶解和沉淀热处理的铝合金轧制或冷加工的棒材、杆材、线材和环材

This specification covers an aluminum alloy in the form of rolled or cold finished bars, rods, and wire, and of flash welded rings. These products have been used typically for parts requiring high strength where limited formability is acceptable. Certain design and processing procedures may cause these products to be susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy Bars, Rods, and Wire Rolled or Cold Finished, and Rings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T6) Solution and Precipitation Heat Treated UNS A97075

SAE AMS2368B-2007 除锻件和锻造原料以外的锻造钛原料用取样和测试

This specification provides a standard set of procedures for sampling and testing to meet the requirements of material specifications for wrought titanium and titanium alloy products except forgings and forging stock. It is applicable to the extent specified in a material specification.

Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging Stock

SAE AMS4347C-2007 1.0Mg 0.8Si 0.8Cu 0.50Mn (6013-t4)溶解热处理和自然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 typically for formed structural parts where good stretch formability is required and where, after precipitation heat treatment, good strength, toughness, and fatigue properties and maximum corrosion resistance are inherent, but usage is not limited to such applications.

Aluminum Alloy Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.5Mn (6013-T4) Solution Heat Treated and Naturally Aged UNS A96013

SAE AMS4411-2007 7.2Zn 1.5Cu 2.0Mg 0.10Zr溶解热处理、应力释放和老化的铝合金厚板材(7081-T7651)

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 moderate resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy Plate (7081-T7651) 7.2Zn - 1.5Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved and Overaged UNS A97081

SAE AMS4409-2007 4.0Zn 2.0Mg 0.32Mn (7019-T651)溶解热处理、应力释放和人工老化的铝合金厚板材

This specification covers an aluminum alloy in the form of plate. This product has been used as a moderate strength engineered plate used also for selected structural applications, but usage is not limited to such applications. Armor plate applications are possible, but specific sampling and testing procedures regarding material properties required for this application shall be mutually agreed by producer and user.

Aluminum Alloy, Plate 4.0Zn - 2.0Mg - 0.32Mn (7019-T651) Solution Heat Treated, Stress Relieved and Artificially Aged UNS A97019

SAE AMS4410-2007 7.2Zn 1.5Cu 2.0Mg 0.10Zr溶解热处理、应力释放和过度老化的铝合金厚板材(7081-T7451)

The 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 (7081-T7451) 7.2Zn - 1.5Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved and Overaged UNS A97081

SAE AMS4121H-2007 4.5Cu 0.85Si 0.80Mn 0.50Mg (2014-T6)溶解和沉淀热处理的轧制或冷精轧铝合金棒材、杆材和线材

This specification covers an aluminum alloy in the form of bars, rods, and wire. These product have been used typically for parts requiring high strength where limited formability is acceptable but usage is not limited to such applications. 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 Bars, Rods, and Wire, Rolled or Cold Finished 4.5Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T6) Solution and Precipitation Heat Treated UNS A92014

SAE AMS4128D-2007 1.0Mg 0.60Si 0.30Cu 0.20Cr(6061-T451)溶解热处理和通过拉伸消除应力的轧制或冷精整的铝合金棒材

This specification covers an aluminum alloy in the form of bars and rods 0.500 inch (12.50mm) and over in nominal diameter or least difference between parallel sides. These bars have been used typically for parts where moderate ductility, formability, and response to precipitation heat treatment are required and where distortion during machining must be minimized, but usage is not limited to such applications.

Aluminum Alloy Bars, Rolled or Cold Finished 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T451) Solution Heat Treated and Stress Relieved by Stretching UNS A96061

SAE AMS4287A-2007 2.7 Cu 1.8 Li 0.7 Zn 0.3 Mn 0.3 Mg 0.08 Zr (2099-T83)溶解热处理、用1%～4%拉伸的应力释放和老化的挤压成形铝合金

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) produced with cross sectional area of 15 square inches (97 cm) maximum and a circumscribing circle diameter (circle size) of 11 inches (28 cm) maximum.

Aluminum Alloy, Extrusion 2.7 Cu - 1.8 Li - 0.7 Zn - 0.3 Mn - 0.3 Mg - 0.08 Zr (2099-T83) Solution Heat Treated, Stress Relieved by Stretching 1% to 4% and Aged UNS A92099

SAE AMS4036K-2006 单侧包和按SAE 2024标准规定形变小于1～1.5%的4.4Cu - 1.5Mg - 0.60Mn铝合金片材和板材及按SAE2024-T3规定形变小于1-1.5%的单侧包铝合金片材、按2024-T351规定的形变小于1-1.5%单侧包铝合金板材

This specification covers an aluminum alloy in the form of sheet and plate clad on one side with a different aluminum alloy.

Aluminum Alloy, Sheet and Plate, Alclad One Side, 4.4Cu - 1.5Mg - 0.60Mn, Alclad One Side 2024 and 1-1/2% Alcald One Side 2024-T3 Sheet; 1-1/2% Alclad One Side 2024-T351 Plate

SAE AMS4304A-2006 沉淀热处理和2009/SiC/15W(T8P)溶解热处理的拉伸非连续加固铝合金薄板材

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

DIN EN 4286:2006 航空航天系列.铝合金AL-P8090-T89.模锻件.a≤125mm

This standard specifies the requirements relating to: Aluminium alloy AL-P8090- T89 Die forgings a 125 mm for aerospace application.

Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings - a ≤ 125 mm; German and English version EN 4286:2005

DIN EN 2086:2006 航空航天系列.铝合金AL-P2618A-T851.手锻和模锻件.a ≤150 mm

Aerospace series - Aluminium alloy AL-P2618A-T851 - Hand and die forgings - a ≤ 150 mm; German and English version EN 2086:2004

DIN EN 4291:2006 航空航天系列.铝合金AL-P8090.锻坯

Aerospace series - Aluminium alloy AL-P8090 - Forging stock; German and English version EN 4291:2005