V11 航空与航天用金属铸锻材料 标准查询与下载

SAE AMS4958D-2013 3Al 8V 6Cr 4Mo 4Zr自耗电极熔炼、溶液热处理和无中心接地的钛合金棒材和杆材

This specification covers a titanium alloy in the form of bars and rod 1.000 inch (25.40 mm) and under in nominal diameter. These products have been used typically for coil springs requiring low solid height, high tensile strength, and corrosion resistance, but usage is not limited to such applications.

Titanium Alloy, Bars and Rod, 3Al 8V 6Cr 4Mo 4Zr, Consumable Electrode Melted, Solution Heat Treated and Centerless Ground or Peeled and Polished

SAE AMS4475-2013 溶液热处理镀铝铝合金卷材4.4Cu 1.5Mg 0.60Mn (铝衣合金2024l-T4卷材)

Aluminum Alloy, Coiled Sheet, Alclad 4.4Cu 1.5Mg 0.60Mn (Alclad 2024l -T4 Coiled Sheet) Solution Heat Treated

SAE AMS5604G-2013 溶液热处理和沉淀硬化的抗腐蚀钢薄板材、带材和板材16.5Cr 4.0Ni 4.0Cu 0.30Cb

This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate. These products have been used typically for parts requiring corrosion resistance and high strength up to 600 °F (316 °C) and where such parts may require welding during fabrication, but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP1110 recommends practices to minimize such conditions.

Steel, Corrosion Resistant, Sheet, Strip, and Plate 16.5Cr 4.0Ni 4.0Cu 0.30Cb, Solution Heat Treated, Precipitation Hardenable

SAE AMS2243K-2013 耐腐蚀和耐热的钢管公差

This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat resistant steel ordered to inch dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID).

Tolerances Corrosion and Heat Resistant Steel Tubing

SAE AMS5643/H1150-2013 溶解热处理,沉积热处理耐腐蚀钢棒材、线材、锻材、管材和环材16Cr 4.0Ni 0.30Cb (Nb) 4.0Cu

this specification covers a corrosion-resistant steel product in the solution and precipitation heat treated (H115) condition.

Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing and Rings 16Cr 4.0Ni 0.30Cb (Nb) 4.0Cu Solution and Precipitation Heat Treated (H1150)

SAE AMS5349E-2013 硬化和回火易切削的13Cr耐腐蚀熔模钢铸件

This specification covers a corrosion resistant steel in the form of investment castings. These castings have been used typically for small parts for use up to 1000 °F (538 °C), but usage is not limited to such applications. Corrosion resistance is lower than that of AMS 5350, but machinability is better.

Steel, Corrosion Resistant, Investment Castings 13Cr Free Machining; Hardened and Tempered

SAE AMS5666G-2013 退火的耐腐蚀和耐热的镍合金棒材、锻材、挤制件和环材62Ni 21.5Cr 9.0Mo 3.65Cb (Nb)

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, extrusions, flash welded rings, and stock for forging or flash welded rings. These products have been used for parts requiring both corrosion and oxidation resistance up to 2000 degrees F (1093 degrees C) and where such parts may require welding during fabrication, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, Extrusions, and Rings 62Ni 21.5Cr 9.0Mo 3.65Cb (Nb) Annealed

SAE AMS5923-2013 轴承用耐腐蚀钢棒材、线材和锻材17Cr 0.52Mo (0.95 - 1.20C) (440C)

This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.

Steel, Corrosion-Resistant, Bars, Wire, and Forgings 17Cr 0.52Mo (0.95 - 1.20C) (440C) for Bearing Applications

SAE AMS7855D-2013 再结晶钶(铌)合金棒材、杆材和线材10W 2.5Zr

This specification cover as columbium alloy in the form of bars, rods, or wire. This material has been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.

Columbium (Niobium) Alloy Bars, Rods, and Wire 10W 2.5Zr Recrystallized

SAE AMS7851D-2013 再结晶的钶(铌)合金箔片、片材、带材和板材10W-2.5Zr

This specification covers a columbium (niobium) alloy in the form of foil, sheet, strip, or plate. This material has been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.

Columbium (Niobium) Alloy Foil, Sheet, Strip and Plate, 10W 2.5Zr Recrystallized

SAE AMS4949A-2013 表面粘结的层压钛片材

This specifocation covers titanium in the form of laminated sheet. This materials has been used typically for shims in which thickness is adjusted by removal of laminations as required, but usage is not limited to such applications.

Titanium, Sheet, Laminated, Surface Bonded

SAE AMS7852C-2013 钶(铌)合金片材、带材和板材.10Hf 1.0Ti

This specification covers a columbium (niobum) alloy in the form of sheet, strip, and plate. This material has been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.

Columbium (Niobium) Alloy Sheet, Strip, and Plate, 10Hf 1.0Ti

SAE AMS5541G-2013 退火的防腐和耐热镍合金片材和带材73Ni 15.5Cr 2.4Ti 0.70A1 7.0Fe

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet and strip. These products have been used typically for parts requiring high strength up to 1500 °F (816 °C) and oxidation resistance up to 1800 °F (982 °C), but usage is not limited to such applications. Parts may be formed and then heat treated to improve strength at elevated temperatures.

Nickel Alloy, Corrosion and Heat Resistant, Sheet and Strip 73Ni 15.5Cr 2.4Ti 0.70A1 7.0Fe Annealed

SAE AMS4160H-2013 退火铝合金挤压制品1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-O)

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing.

Aluminum Alloy, Extrusions 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-O), Annealed

DIN EN 4526:2013 航空航天系列.金属材料.试验方法.片材和带材的锐边缺口拉伸试验.德文和英文版本EN 4526-2013

Aerospace series - Metallic materials - Test methods - Sharp edge-notch tensile testing for sheet and strip; German and English version EN 4526:2013

DIN EN 4631:2013 航空航天系列.X4CrNiMo16-5-1(1.4418)型钢.空气熔炼.淬火和回火.棒材.D_e≤200 mm.900MPa≤R_m≤1050 MPa.德文和英文版本EN 4631-2013

Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - D_e 200 mm - 900 MPa R_m 1 050 MPa; German and English version EN 4631:2013

DIN EN 4628:2013 航空航天系列.X4CrNiMo16-5-1(1.4418)型钢.空气熔炼.淬化和回火.棒材.De≤150 mm.1500 MPa≤Rm≤1300 MPa.德文和英文版本EN 4628-2013

Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De 200 mm - 1150 MPa Rm 1300 MPa; German and English version EN 4628:2013

DIN EN 4629:2013 航空航天系列.X4CrNiMo16-5-1(1.4418)型钢.空气融化.退火.锻坯.D_e≤300 mm.德文和英文版本EN 4629-2013

Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Softened - Forging stock - D_e 300 mm; German and English version EN 4629:2013

SAE AMS6516A-2013 真空感应融化、真空电弧重熔型、规范化和退火沉淀可硬化的钢棒材和锻件1Cr 10Ni 7Co 2Mo 1.3W 0.1V (0.28-0.32C)

This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock. These products have been used typically for heat treated parts requiring a combination of high strength, high toughness, and weldability, but usage is not limited to such applications.

Steel, Bars and Forgings 1Cr 10Ni 7Co 2Mo 1.3W 0.1V (0.28 - 0.32C) Vacuum Induction Melted, Vacuum Arc Remelted, Normalized and Annealed Precipitation Hardenable

BS EN 4632-006:2013 航空航天系列.航空航天结构用材料的可焊接性和可钎焊性.钛合金的均质装配件

Aerospace series. Weldability and brazeability of materials in aerospace constructions. Homogeneous assemblies of titanium alloys