V11 航空与航天用金属铸锻材料 标准查询与下载

SAE AMS6529C-2012 专门航空器品质清洁规格化钢棒0.95Cr 0.20Mo(0.38-0.43C) (SAE 4140)

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars. These bars have been used typically for parts required to meet stringent magnetic inspection criteria, 0.75 inch (19.0 mm) and under in nominal thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered, and also for parts of greater thickness requiring proportionately lower hardness, but usage is not limited to such applications.

Steel, Bars 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140) Special Aircraft-Quality Cleanliness Normalized (UNS G41400)

SAE AMS6514H-2012 自耗电极真空熔化退火18.5Ni 9.0Co 4.9Mo 0.65Ti 0.10Al钢制马钉钢,棒材,锻件,管材和环材

This specification covers a premium aircraft-quality steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring through hardening, without liquid quenching, to a yield strength of 270 psi (1862 MPa) and higher and where such parts may require welding during fabrication, but usage is not limited to such applications.

Steel, Maraging, Bars, Forgings, Tubing, and Rings 18.5Ni - 9.0Co - 4.9Mo - 0.65Ti - 0.10Al Consumable Electrode Vacuum Melted, Annealed (UNS K93120)

SAE AMS4455G-2012 溶解和沉积热处理10A1(AM100A-T6)镁合金熔模铸件

This specification covers a magnesium alloy in the form of investment castings. These castings have been used typically for small intricate parts, which may operate up to 300 °F (149 °C) and are cast to approximate final dimensions, where the intricacy of the part is such that high fluidity of the molten metal is required, but usage is not limited to such applications.

Magnesium Alloy, Investment Castings 10Al (AM100A-T6) Solution and Precipitation Heat Treated (UNS M10100)

SAE AMS6484D-2012 0.80Cr 1.8Ni 0.25Mo (0.38 - 0.43C)SAE 4340规范的和回火钢筋,钢锻件和管件

This specification covers an aircraft-quality, low-alloy steel in the form of bars, fogings, mechanical tubing, and forging stock. These products have been used typically for parts, 3.5 inches (89 mm) and under in nominal thickness at time of heat treatment, requiring a through-hardening steel capable of developing a minimum hardness of 40 HRC when properly hardened and tempered and also for parts of greater thickness requiring proportionately lower hardness, 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; SAE ARP 1110 recommends practices to minimize such conditions.

Steel, Bars, Forgings, and Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) Normalized and Tempered (UNS G43406)

SAE AMS6415T-2012 0.80Cr 1.8Ni 0.25Mo (0.38 0.43C)钢制棒材,铸件和管材 (SAE 4340)

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, 3.5 inches (89 mm) and under in nominal thickness at time of heat treatment, requiring a through-hardening steel capable of developing a minimum hardness of 40 HRC when properly hardened and tempered and also for parts of greater thickness but requiring proportionately lower hardness, 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; SAE ARP 1110 recommends practices to minimize such conditions.

Steel, Bars, Forgings, and Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) (UNS G43406)

DIN EN 2213:2012 航空航天系列. FE-PL1505 (15CrMoV6) 型钢. 空气熔炼. 淬火和回火. 棒材. De ≤ 16 mm. 980 MPa ≤ Rm ≤ 1180 MPa; 德文和英文版本EN 2213-2012

Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - D_e 16 mm - 980 MPa R_m 1 180 MPa; German and English version EN 2213:2012

SAE AMS4442G-2012 镁合金砂模铸件3.2稀土族2.5Zn 0.70Zr (EZ33A-T5)沉积热处理

This specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for parts operating in service up to 500 °F (260 °C), but have good pressure tightness, but usage is not limited to such applications.

Magnesium Alloy Sand Castings 3.2 Rare Earths - 2.5Zn - 0.70Zr (EZ33A-T5) Precipitation Heat Treated (UNS M12330)

SAE AMS4453F-2012 溶解和沉淀热处理9.0Al 2.0Zn (AZ92A-T6)镁合金熔模铸造

This specification covers a magnesium alloy in the form of investment castings. These castings have been used typically for intricate parts cast to approximate final dimensions, but usage is not limited to such applications.

Magnesium Alloy, Investment Castings 9.0Al 2.0Zn (AZ92A-T6) Solution and Precipitation Heat Treated

SAE AMS4452E-2012 溶解和沉淀热处理镁合金熔模铸件8.7Al 0.70Zn 0.22Mn (AZ 91C-T6)

This specification covers a magnesium alloy in the form of investment castings. These castings have been used typically for small, intricate parts requiring good strength with good ductility and weldability, but usage is not limited to such applications.

Magnesium Alloy, Investment Castings 8.7Al 0.70Zn 0.22Mn (AZ 91C-T6) Solution and Precipitation Heat Treated

SAE AMS6409D-2012 标准化和回火的专用航空器质量清洁钢棒,铸件和管0.80Cr 1.8Ni 0.25Mo (0.38-0.43C)(SAE 4340)

This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts required to meet stringent magnetic particle inspection criteria, having sections 3.5 inches (89 mm) and under in nominal thickness at time of heat treatment, and requiring a through-hardening steel capable of developing a minimum hardness of 40 HRC when properly hardened and tempered and also for parts of greater thickness but requiring proportionately lower hardness, 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; ARP 1110 recommends practices to minimize such conditions. These products are not recommended for use in parts heat treated to a hardness greater than 46 HRC (ultimate tensile strength over 220 ksi (1517 MPa)) or where the high transverse properties of remelted steel are required.

Steel, Bars, Forgings, and Tubing 0.80Cr 1.8Ni 0.25Mo (0.38-0.43C) (SAE 4340) Special Aircraft Quality Cleanliness, Normalized and Tempered

SAE AS1576D-2012 3000 psi液压耐腐蚀钢和镍,焊接液压钛配件

This documents defines the requirements for weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3Al-2.5V titanium , 21Cr-6Ni-9Mn CRES and nickel alloy tubing. Fitting standards covered by this specification include non-separable welded elbow, tee, and reducer fittings, and reconnectable 24 degree cone fittings such as sleeves and unions.

Fittings, Welded, Hydraulic, Titanium, Corrosion Resistant Steel and Nickel, 3000 psi Hydraulic

SAE AMS4921M-2012 每70 ksi(483 MPa)屈服强度的商用钛棒材,线材,铸件和环材

This specification covers one grade of commercially-pure titanium in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring high corrosions resistance and moderate strength up to 400 °F (204 °C) and oxidation resistance up to 600 °F (316 °C), but usage is not limited to such applications.

Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength (UNS R50700)

SAE AMS6260R-2012 1.2Cr 3.2Ni 0.12Mo (0.07 - 0.13C) (9310)钢筋,锻件和管件

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for carburized parts, including gears, which require high minimum core hardness with a narrow range, but usage is not limited to such applications. The core is machinable after hardening.

Steel, Bars, Forgings, and Tubing 1.2Cr - 3.2Ni - 0.12Mo (0.07 - 0.13C) (9310) (UNS G93106)

SAE AMS5507G-2012 溶解热处理,17Cr 13Ni 2.5Mo (316L)耐高温和腐蚀钢片材,带材和板材

This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate. These products have been used typically for parts requiring both corrosion and heat resistance up to 1600 degrees F (871 degrees C) and for welding, but usage is not limited to such applications. At elevated temperatures, the strength of this steel is slightly higher than, and the oxidation resistance is similar to, that of 18-8 type steels.

Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 17Cr - 13Ni - 2.5Mo (316L) Solution Heat Treated (UNS S31603)

SAE AMS5870E-2012 溶解热处理耐腐蚀和耐高温的60.5Ni 23Cr 14Fe 0.35Ti 1.4Al镍合金薄板材,带材和板材

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring corrosion and oxidation resistance up to 2200 degrees F (1204 degrees C), particularly where such parts may require welding during fabrication, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip and Plate 60.5Ni 23Cr 14Fe 0.35Ti 1.4Al Solution Heat Treated

SAE AMS5811D-2012 真空感应融化,环境受控打包15Cr 30Ni 1.2Mo 2.2Ti 0.25Al 0.001B 0.30V (0.01-0.03C)耐高温和腐蚀钢焊丝

This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as filler metal for gas-metal-arc welding or gas-tungsten-arc of critical weldments of precipitation-hardenable, corrosion and heat resistant steels of similar composition where the weld area is required to have strength and corrosion resistance comparable to those of the parent metal, but usage is not limited to such applications. This filler metal provides joints with increased crack resistance over those using AMS 5805 wire when welding similar steels.

Steel, Corrosion and Heat Resistant, Welding Wire 15Cr 30Ni 1.2Mo 2.2Ti 0.25Al 0.001B 0.30V (0.01-0.03C), Vacuum Induction Melted, Environmental Controlled Packaging

NF L14-643*NF EN 3312:2012 航空系列.钛合金 TI-P64001 (Ti-6Al-4V).煅烧.锻件.De < 或 = 150 mm.

Aerospace series - Titanium alloy Ti-6AI-4V) - Annealed - Forgings - De < or = 150 mm.

SAE AMS6308E-2012 真空弧焊或电渣再熔化0.90Si 1.0Cr 2.0Ni 3.2Mo 2.0Cu 0.10V (0.07-0.13C)钢棒和铸件

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. These products have been used typically for highly-stressed carburized parts requiring high minimum case hardness and subject to very rigid magnetic particle inspection standards, but usage is not limited to such applications. These products are suitable for service up to 450 °F (232 °C).

Steel, Bars and Forgings 0.90Si - 1.0Cr - 2.0Ni - 3.2Mo - 2.0Cu - 0.10V (0.07 - 0.13C) Vacuum Arc or Electroslag Remelted (UNS K71040)

SAE AMS4427C-2012 溶解和沉积热处理4.0Y 2.3Nd 0.7Zr (WE43B - T6)砂模镁合金铸件

This specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for parts requiring a combination of light weight, high yield strength up to 570 °F (298 °C), and relatively high corrosion resistance, but usage is not limited to such applications.

Magnesium Alloy Castings, Sand 4.0Y 2.3Nd 0.7Zr (WE43B - T6) Solution and Precipitation Heat Treated

SAE AMS6525D-2012 自耗电极真空融化0.75Cr 9.0Ni 4.5Co 1.0Mo 0.09V (0.17-0.23C)钢筋,钢锻件,管件和环材

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for heat-treated parts, requiring toughness and through-hardening to high strength levels and where such parts may require welding during fabrication, but usage is not limited to such applications.

Steel, Bars, Forgings, Tubing, and Rings 0.75Cr - 9.0Ni - 4.5Co - 1.0Mo - 0.09V (0.17 - 0.23C) Consumable Electrode Vacuum Melted (UNS K91472)