49.025.20 铝 标准查询与下载

SAE AMS4211B-2007 老化、应力释放和溶解热处理的6.2Zn 1.9Cu 2.1Mg 0.10Zr 铝合金板材(7040-T7451)

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

Alluminum Alloy, Plate 6.2Zn - 1.9Cu - 2.1Mg - 0.10Zr (7040-T7451) Solution Heat Treated, Stress Relieved, and Overaged UNS A97040

SAE AMS4223D-2007 4.5Cu 0.70Ag 0.30Mn 0.25Mg 0.25Ti (A201.0-T4)铝合金铸件的溶解热处理和自然老化

This specification covers an aluminum alloy in the form of castings. These castings have been used typically for components requiring high strength combined with good ductility and impact strength, but usage is not limited to such applications. Certain design and processing procedures may cause these castings to become susceptible to stress-corrosion cracking.

Aluminum Alloy, Castings 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (A201.0-T4) Solution Heat Treated and Naturally Aged

SAE AMS4217H-2007 7.0Si 0.32Mg (356.0-T6)铝合金铸件的溶解和沉淀热处理

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

Aluminum Alloy, Castings 7.0Si - 0.32Mg (356.0-T6) Solution and Precipitation Heat Treated UNS A03560

DIN EN 3339:2007 航天航空系列.AL-P7010-T76型铝合金.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 200 mm; German and English version EN 3339:2006

DIN EN 4003:2007 航空航天系列.AL-P2219-T87型铝合金.0.5mm≤a≤6mm的薄板材和带材.

The document specifies the requirements relating to sheet and strip, in aluminium alloy AL-P2219, for use in the T87 condition,0,5 mm (kursiv)a 6 mm, for aerospace applications.#,,#

Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm ≤ a ≤ 6 mm; German and English version EN 4003:2006

BS EN 4003:2006 航空航天系列.AL-P2219-T87型铝合金.0.5mm≤a≤6mm的薄板材和带材

This standard specifies the requirements relating to: Aluminium alloy AL-P2219-T87 — Sheet and strip 0,5 mm ≤ a ≤ 6 mm for aerospace applications.

Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm a 6 mm

BS EN 4003:2007 航空航天系列 AL-P2219-T87型铝合金 0.5mm≤a≤6mm的薄板材和带材

Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm a 6 mm

DS/EN 3339:2007 航天系列 铝合金 AL-P7010 T76 模锻件 a <= 200 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P7010-T76Die forgingsa

Aerospace series - Aluminium alloy AL-P7010- - T76 - Die forgings - a <= 200 mm

SAE ARP1575B-2007 应用磷酸阳极氧化的高耐久性结构粘结铝合金零件的表面制备和涂底

This document describes a hand-applied, nontank, phosphoric acid anodizing process for surface preparation of aluminum alloys required to achieve optimum bondline durability for structural adhesive bonding.

Surface Preparation and Priming of Aluminum Alloy Parts for High Durability Structural Adhesive Bonding, Hand Applied Phosphoric Acid Anodizing

SAE AMS4270B-2007 铝合金,铝衣合金平板, 4.1Cu - 1.4Mg - 0.45Mn (铝衣合金2424-T3),溶解热处理和冷加工

This specification covers an aluminum alloy in the form of sheet clad on both sides with a different aluminum alloy.

Aluminum Alloy, Alclad Flat Sheet, 4.1Cu - 1.4Mg - 0.45Mn (Alclad 2424-T3), Solution Heat Treated and Cold Worked

SAE AMS-QQ-A-200/13B-2007 挤压的铝合金7178, 棒材, 杆材, 型材, 管材, 以及线材

This specification covers the specific requirements for aluminum alloy 7178 bar, rod, shapes, tube, and wire produced by extrusion.

Aluminum Alloy 7178, Bar, Rod, Shapes, Tube, and Wire, Extruded

SAE AMS4088K-2007 (2024-T3)4.4Cu 1.5Mg O.60Mn溶解热处理和冷加工铝合金拉制无缝管件

This specification covers an aluminum alloy in the form of seamless, drawn tubing. This tubing has been used typically for parts requiring a high-strength alloy and part is not welded, but usage is not limited to such applications.

Aluminum Alloy, Drawn, Seamless Tubing 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated and Cold Worked UNS A92024

SAE AMS4296B-2007 4.3Cu 1.4Mg O.60Mn(阿尔克莱德包铝 2524-T3)溶解热处理和冷加工阿尔克莱德包铝(Alclad)铝合金薄板和板材

This speicification covers an aluminum alloy in the form of sheet and plate clad on both sides. These products have been used typically for formed structural aircraft parts requiring improved resistance to fatigue crack growth and high toughness with strength similar to Alclad 2024-T3, but usage is not limited to such applications. Certain design and processing procedures may cause these products to be come susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy, Alclad Sheet and Plate 4.3Cu - 1.4Mg - 0.60Mn (Alclad 2524-T3) Solution Heat Treated and Cold Worked UNS A82524

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-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

EN 3998:2007 铝合金AL-P2024-T4或T42.薄板和带材.0.3 mm≤a≤6 mm

This standard specifies the requirements relating to: Aluminium alloy AL-P2024-T4 or T42 - 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

DIN EN 2072:2007 航空航天系列.AL-P1050A-H14铝合金.薄板与带材.0.4≥a≥6mm

This standard specifies the requirements relating to: Aluminium AL-P1050A - H14 Sheet and strip 0,4 mm or =a or = 6 mm for aerospace applications.#,,#

Aerospace series - Aluminium AL-P1050A-H14 - Sheet and strip - 0,4 mm a 6 mm; German and English version EN 2072:2005

DS/EN 4003:2007 航空航天系列 铝合金 AL-P2219-T87 板材和带材 0,5 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm

Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm <= a <= 6 mm

SAE AMS4015L-2007 2.5Mg 0.25Cr (5052-0)退火的铝合金薄板材和厚板材

This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for formed parts requiring moderate strength and good corrosion resistance and where welding may be required in fabrication, but usage is not limited to such applications.

Aluminum Alloy, Sheet and Plate 2.5Mg - 0.25CR (5052-0) Annealed

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

SAE AMS4031G-2007 6.3Cu 0.30Mn 0.18Zr 0.10V 0.06Ti (2219-0)退火的铝合金薄板材和厚板材

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 600 °F (316 °C), but usage is not limited to such applications. These products are also well suited for cryogenic applications and where welding is required.

Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-0) Annealed UNS A92219