49.025.20 铝 标准查询与下载

SAE AMS4207C-2012 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. This sheet has been used typically for structural applications requiring a combination of high strength, moderate fatigue strength, and high fracture toughness, but usage is not limited to such applications.

Aluminum Alloy Sheet, Alclad, 5.7Zn 2.2Mg 1.6Cu 0.22Cr (7454-T61) Solution and Precipitation Heat Treated

SAE AMS2672G-2012 钎焊,铝火焰或熔炉

This specification covers the engineering requirements for producing brazed joints on aluminum and aluminum alloys by torch or furnace brazing. This process has been used typically for joing aluminum and selected aluminum alloys.

Brazing, Aluminum Torch or Furnace

SAE AMS4468-2012 固溶热处理的,冷加工的和人工老化的含5.0Cu 0.4Mn 0.5Mg 0.4Ag (2139-T84)的铝合金板材

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

Aluminum Alloy, Plate 5.0Cu 0.4Mn 0.5Mg 0.4Ag (2139-T84) Solution Heat Treated, Cold Worked, and Artificially Aged

SAE AMS2673E-2012 铝和铝合金熔融焊剂(滴落)钎焊

This specification covers the engineering requirements for producing brazed joints of aluminum and aluminum alloys by immersion in molten flux bath. This process has been used typically for joining aluminum and selected aluminum alloys.

Brazing, Aluminum and Aluminum Alloys Molten Flux (Dip)

BS 5L 101:2011 铝基和镁基铸锭和铸件的检验、试验和验收程序

Procedure for inspection, testing and acceptance of aluminium-base and magnesium-base ingots and castings

BS 5L 100:2011+A1:2013 锻铝和铝合金的检验、测试和验收规程

Procedure for inspection, testing and acceptance of wrought aluminium and aluminium alloys

SAE AMS4035L-2011 含4.4Cu 1.5Mg 0.60Mn(2024-0)的退火铝合金薄板和板材.或加工制品(2024-F)(若有规定)

This specification covers an aluminum alloy in the form of sheet and plate supplied in the annealed (0) condition. When specified, product shall be supplied in the "as fabricated" (F) temper. 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 be susceptible to stress-corrosion cracking after heat treatment; SAE ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy, Sheet and Plate 4.4Cu 1.5Mg 0.60Mn (2024-0) Annealed; or when specified, As Fabricated (2024-F)

SAE AMS4206B-2011 含8.0Zn 2.3Cu 2.0Mg 0.16Zr的固溶热处理,消除应力和过老化的铝合金薄板和板材(7055-T7751)

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

SAE AMS4037P-2011 含4.4Cu 1.5Mg 0.60Mn (2024;-T3平薄板,-T351板材)的固溶热处理铝合金薄板和板材

This specification covers an aluminum alloy in the form of sheet and plate. These products have been typically used for formed structural parts of good strength. Plate is also suitable for structural machined parts where warpage, during maching, due to residual stresses must be minimized, but usage is not limited to such application. 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, Sheet and Plate 4.4Cu 1.5Mg 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate) Solution Heat Treated

SAE AMS4344D-2011 固溶热处理,拉伸消除应力,矫直和过老化的含5.6Zn 2.5Mg 1.6Cu 0.23Cr(7175-T73511)的铝合金挤压件

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, Straightened, and Overaged

SAE AMS4316A-2011 固溶热处理和沉淀硬化处理的含5.6Zn 2.5Mg 1.6Cu 0.23Cr 7075的铝合金,镀铝薄板和板材(-T76 薄板,-T7651板材)

RATIONALE: Corrects an error in Tables 3A and 3B. This specification covers an aluminum alloy in the form of Alclad sheet and plate. This product has been used typically for applications requiring a high level of mechanical properties and good resistance to exfoliation corrosion, but usage is not limited to such applications.

Aluminum Alloy, Alclad Sheet and Plate 5.6Zn 2.5Mg 1.6Cu 0.23Cr 7075: (-T76 Sheet, -T7651 Plate) Solution and Precipitation Heat Treated

SAE AMS4273C-2011 固溶热处理和冷加工铝合金薄板和板材(2424-T3 平薄板和板材)

This specification covers an aluminum alloy in the form of sheet. This product has been used typically for formed structural parts with good tensile strength, corrosion resistance, toughness, and resistance to fatigue crack growth, but usage is not limited to such applications. Certain design and processing procedures may cause this sheet to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy, Sheet and Plate (2424-T3 Flat Sheet and Plate) Solution Heat Treated and Cold Worked

SAE AMS4401A-2011 含6.6Zn 1.8Cu 2.0Mg 0.10Zr的固溶热处理,消除应力和过老化的铝合金板材(7140-T7451)

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 AMS4078J-2011 经溶液热处理的含有5.6Zn,2.5Mg,1.6Cu和0.23Cr 7075超龄铝合金钢片和钢板(-T73钢片,-T7351钢板)

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 and Overaged

SAE AMS-QQ-A-367C-2011 铝合金锻件

This specification covers aluminum alloy die forgings and hand forgings.

Aluminum Alloy Forgings

SAE AMS4473-2011 固溶热处理,冷加工和自然老化的含4.1Cu-1.4Mg-0.6Mn(2624-T39)铝合金板

This specification covers an aluminum alloy in the form of pate. This product has been used typically for structural parts requiring a high level of mechanical properties and good damage tolerance, but usage is not limited to such applications.

Aluminum Alloy Plate (2624-T39) 4.1Cu 1.4Mg 0.6Mn Solution Heat Treated, Cold Worked and Naturally Aged

SAE AMS-A-21180B-2011 高强度钛合金铸件

This specification covers the requirements for six alloy compositions, four inspection classes, four radiographic quality grades and six classes of mechanical properties of high strength aluminum-alloy castings.

Aluminum-Alloy Casting, High Strength

SAE AMS2772F-2011 铝合金原材料的热处理

This specification covers requirements and recommendations for the heat treatment of wrought aluminum alloy raw materials by producers. It supersedes AMS-H-6088 and replaces MIL-H-6088. Aluminum alloy tempers are described in SAE AS1990 and ANSI H35.1 This specification may be used for alloys other than those specified herein providing temperatures, times, and quenchant are specified.

Heat Treatment of Aluminum Alloy Raw Materials

SAE AMS2771D-2011 铝合金铸件的热处理

The specification covers the engineering requirements for heat treatment of aluminum alloy castings and for parts machined from castings.

Heat Treatment of Aluminum Alloy Castings

SAE AMS4601-2011 固溶热处理,冷加工和自然老化(2219-T31/T-351)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 \mCD)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 and Naturally Aged (2219-T31/T-351)