V11 航空与航天用金属铸锻材料 标准查询与下载

SAE AMS4963C-2012 改进强度热处理退火6.0Al 4.0V钛合金棒材,线材,锻件和环材

This specification covera a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts to be rough machined prior to solution and precipitation heat treatment and for parts requiring high strength-to-weight ratios at or near room temperature, 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; SAE ARP 983 recommends practices to minimize such conditions.

Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Annealed, Heat Treatable, Modified Strength

SAE AMS4973G-2012 溶解热处理和稳定钛合金锻件8Al 1Mo 1V

This specificaiton covers a titanium alloy in the form of forgings and forging stock. This alloy has been used typically for parts requiring strength up to 800 degree F (427 degree C), but usage is not limited to such applications.

Titanium Alloy Forgings 8Al 1Mo 1V Solution Heat Treated and Stabilized

SAE AMS6303H-2012 0.65Si 1.25Cr 0.50Mo 0.85V (0.25-0.30C)耐热性低合金钢棒和铸件

This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, and forging stock. These products have been used typical for parts, such as turbine discs, compressor discs, and fasteners, for service up to 1050 °F (566 °C), but usage is not limited to such applications.

Steel Bars and Forgings, Low Alloy, Heat Resistant 0.65Si 1.25Cr 0.50Mo 0.85V (0.25-0.30C)

SAE AMS4881D-2012 冷浸淬火与回火78Cu 11Al 5.1Ni 4.8Fe,马氏体镍-铝-铜砂模和连续铸件

This specification covers a nickel-aluminum bronze alloy in the form of sand or centrifugal castings. These castings have been used typically for parts requiring a combination of high strength and hardness with some ductility and toughness, but usage is not limited to such applications.

Nickel-Aluminum-Bronze, Martensitic, Sand and Continuous Castings, 78Cu 11Al 5.1Ni 4.8Fe, Quench Hardened and Tempered Annealed

SAE AMS2368C-2012 锻件和锻坯除外的锻造钛原材料的样品和测试

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 AMS6481C-2012 轴承应用双精度型真空融化用保证飞机质量渗氮处理3Cr 1Mo 0.2V (0.29 - 0.36C)钢筋,铸件和管件

This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for nitrided parts such as bearings, operating under heavy loads and high speeds at moderate temperatures, and subject to very rigid inspection standards, and requiring highest surface hardness, high core toughness, and less distortion than parts made from steel requiring quenching to case harden, but usage is not limited to such applications

Steel Bars, Forgings, and Tubing, Nitriding 3Cr 1Mo 0.2V (0.29 - 0.36C) Premium Aircraft-Quality for Bearing Applications Double Vacuum Melted

SAE AMS4909J-2012 超低间隙退火,5Al 2.5Sn板材,带材和片材钛合金

This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to -423 °F (-253 °C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause those products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy, Sheet, Strip, and Plate 5Al 2.5Sn, Extra Low Interstitial Annealed

SAE AMS4002-2012 通过拉伸和老化(2013-T6511)的无缝拔制1.8Cu 1.0Mg 0.8Si 0.20Cr 熔解热应力消除铝合金管道系统

This specification covers an aluminum alloy in the form of seamless, drawn tubing.

Aluminum Alloy Tubing, Seamless, Drawn 1.8Cu 1.0Mg 0.8Si 0.20Cr Solution Heat Treated, Stress-Relieved by Stretching, and Aged (2013-T6511)

DIN EN 4659 Berichtigung 1:2012 航空航天系列.FE-PM1507型钢(X1CrNiMoAlTi12-11-2).真空感应融化和自耗电极冶炼.溶液处理和沉淀处理.铸件.a或D≥200 mm.Rm≥1650 MPa.德文和英文版本EN 4659-2010, DIN EN 4659-2012-01的勘误表

Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D 200 mm - R_m 1 650 MPa; German and English

BS EN 3456:2012 航空航天系列.TI-P64001(Ti-6Al-4V)型钛合金.退火.热轧薄板材和带材.a 6 mm

Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled - a 6 mm

SAE AMS4471-2012 熔模铸造,溶解和沉积热处理4.6Cu 3.4Ti 1.4B 0.75Ag 0.27Mg (A205.0/TiB2/3p-T7P)铸造铝合金复合材料

This specification covers a dilute aluminum/TiB2 metal matrix composite in the form of investment castings.

Cast Aluminum Alloy Composite 4.6Cu 3.4Ti 1.4B 0.75Ag 0.27Mg (A205.0/TiB2/3p-T7P) Investment Cast, Solution and Precipitation Heat Treated

SAE AMS4482-2012 溶解和沉淀热处理4.6Cu 3.4Ti 1.4B 0.75Ag 0.27Mg (A205.0/TiB2/3p-T7P)铸造铝合金复合材料砂铸件

This specification covers a dilute aluminum/TiB2 metal matix composite in the form of sand castings.

Cast Aluminum Alloy Composite 4.6 Cu - 3.4Ti - 1.4B - 0.75Ag - 0.27Mg (A205.0/TiB2/3p-T7P) Sand Cast, Solution and Precipitation Heat Treated

SAE AMS6511A-2012 退火双重真空融解18Ni 8.5Co 3.2Mo 0.20Ti 0.10Al马钉钢筋,铸件,管道和环材

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 yield strengthof 200 ksi (1379 MPa) and where such parts may require welding during fabrication, but usage is not limited to such applications.

Steel, Maraging, Bars, Forgings, Tubing, and Rings 18Ni - 8.5Co - 3.2Mo - 0.20Ti - 0.10Al Double Vacuum Melted, Annealed (UNS K92710)

SAE AMS7496K-2012 闪光焊低合金碳素钢环材

This specification covers flash welded rings fabricated from carbon and low-alloy steels. This product has been used typically for parts such as flanges and rings, but usage is not limited to such applications.

Rings, Flash Welded Carbon and Low-Alloy Steels

SAE AMS6515A-2012 退火双重真空融解18.5Ni 12.0Co 4.9Mo 1.40Ti 0.10Al马钉钢筋,铸件,管道和环材

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.

Steel, Maraging, Bars, Forgings, Tubing, and Rings 18.5Ni 12.0Co 4.9Mo 1.40Ti 0.10Al Double Vacuum Melted, Annealed

SAE AMS5637H-2012 溶解热处理,冷拔和应力消失125 ksi(862 MPa)抗张强度耐蚀钢棒材和线材18Cr 9.0Ni(SAE 30302)

This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides. These products have been used typically for small parts, such as bolts, screws, and clevis pins, requiring corrosion resistance up to 700 degrees F (371 degrees C) and which may be fabricated by heading or by machining from bars or wire and roll threading, but usage is not limited to such applications.

Steel, Corrosion Resistant, Bars and Wire 18Cr 9.0Ni (SAE 30302) Solution Heat Treated, Cold Drawn and Stress Relived 125 ksi (862 MPa) Tensile Strength

SAE AMS4040N-2012 退火铝衣合金4.4Cu 1.5Mg 0.60Mn (2024 -O and 1-1/2% 铝衣合金)铝合金片材和板材

This specification covers an aluminum alloy in the form of sheet and plate clad on both sides with a different aluminum alloy. 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 become susceptible to stress-corrosion cracking after heat treatment; ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024-O with 1 ?% Alclad); Annealed (UNS A82024)

SAE AMS4194D-2012 溶解热处理和冷加工铝衣合金,4.4Cu 1.5Mg 0.60Mn,铝合金片材和板材

This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T361 temper. These products have been used typically for high strength parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and maximum corrosion resistance and whose fabrication does not involve welding, but usage is not limited to such applications.

Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024 -T361 Sheet/Plate with 1?% Alclad) Solution Heat Treated, 6% Cold Worked and Naturally Aged (UNS A82024)

SAE AMS4041R-2012 溶解热处理,冷加工和自然老化的带铝衣合金的铝合金薄板和板材,4.4Cu 1.5Mg 0.60Mn (2024 -T3薄板/-T351 板材带1-1/2%铝衣合金)

This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T3/-T351 temper. These products have been used typically for high strength parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and maximum corrosion resistance and whose fabrication does not involve welding, but usage is not limited to such applications.

Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024, -T3 Sheet/-T351 Plate with 1?% Alclad) Solution Heat Treated, Cold Worked and Naturally Aged (UNS A82024)

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)