V11 航空与航天用金属铸锻材料 标准查询与下载

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 AMS4784G-2012 高温,50Au 25Pd 25Ni,2015至2050℉(1102至1121℃)固相线-液相线范围金-钯-镍合金硬钎料

This specification covers a gold-palladium-nickel alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys where corrosion and oxidation resistant joints with good strength at elevated temperatures are required, but usage is not limited to such applications.

Gold-Palladium-Nickel Alloy, Brazing Filler Metal, High Temperature 50Au - 25Pd - 25Ni 2015 to 2050 °F (1102 to 1121 °C) Solidus-Liquidus Range (UNS P00500)

SAE AMS4101E-2012 溶解热处理拉伸沉淀热处理铝合金板4.4Cu 1.5Mg 0.60Mn (2124-T851)

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 up to 300 °F (149 °C), but usage is not limited to such applications.

Aluminum Alloy, Plate 4.4Cu 1.5Mg 0.60Mn (2124-T851) Solution Heat Treated, Stretched, and Precipitation Heat Treated

SAE AMS6487K-2012 自耗电极真空再熔化钢棒和钢铸件5.0Cr 1.3Mo 0.50V(0.38 0.43C)(H-11)

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 parts requiring through-hardening to a minimum hardness of 50 HRC in section thicknesses up to 12 inches (305 mm) with a combination of high strength, fatigue resistance, ductility, and thermal stability for operation between -100 to +1000 °F (-73 to +538 °C), but usage is not limited to such applications.

Steel, Bars and Forgings 5.0Cr 1.3Mo 0.50V (0.38 0.43C) (H-11) Consumable Electrode Vacuum Melted

SAE AMS6305F-2012 真空电弧再熔化耐热钢棒,钢铸件和钢管0.95Cr 0.55Mo 0.30V (0.40-0.50C)

This specification covers a premium aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, such as compressor discs, turbine discs, shafts, and fasteners for use in service up to 1000 °F (538 °C) and subject to stringent magnetic particle inspection standards, but usage is not limited to such applications.

Steel, Heat-Resistant, Bars, Forgings, and Tubing 0.95Cr 0.55Mo 0.30V (0.40 - 0.50C) Vacuum Arc Remelted

SAE AMS6304L-2012 耐热低合金钢棒,钢铸件和钢管0.95Cr 0.55Mo 0.30V (0.40-0.50C)

This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, such as shafts, and fasteners, in service up to 1000 °F (540 °C), but usage is not limited to such applications.

Low-Alloy Steel, Heat-Resistant, Bars, Forgings, and Tubing 0.95Cr 0.55Mo 0.30V (0.40-0.50C)

SAE AMS4122L-2012 5.6Zn 2.5Mg 1.6Cu 0.23Cr(7075-T6,7075-T651)溶液和沉淀热处理轧制或冷精整铝合金棒材,杆材和线材

This specification covers an aluminum alloy in the form of rolled or cold finished bars, rods, and wire, and of flash welded rings. These products have been used typically for parts requiring high strength where limited formability is acceptable. Certain design and processing procedures may cause these products to be susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy, Bars, Rods, and Wire Rolled or Cold Finished, and Rings, 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T6, 7075-T651) Solution and Precipitation Heat Treated

SAE AMS6255E-2012 双真空熔化钢棒材,钢铸件和钢管1.1Si 1.45Cr 1.0Mo 0.08Al (0.16-0.22C)

This specification covers a premium aircraft-quality, low alloy-steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used for critical carburized parts, such as bearings, gears, and shafts, requiring high minimum core hardness with in a narrow range, good resistance to elevated temperature up to 600 °F (316 °C), and subject to very rigid magnetic particle inspection standards, but usage is not limited to such applications.

Steel Bars, Forgings, and Tubing, 1.1Si 1.45Cr 1.0Mo 0.08Al (0.16-0.22C), Double Vacuum Melted

SAE AMS4429A-2012 溶解和沉淀热处理磨砂镁合金铸件2.8Nd 1.4Gd 0.4Zn 0.6Zr (EV31A-T6)

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 400 °F (204 °C) and relatively high corrosion resistant, but usage is not limited to such applications.

Magnesium Alloy Castings, Sand 2.8Nd 1.4Gd 0.4Zn 0.6Zr (EV31A - T6), Solution and Precipitation Heat Treated

SAE AMS6509-2012 双真空熔化规格化退火的钢棒和钢锻件3.5Cr 7.5Ni 16.3Co 1.75Mo 0.2W(0.09-0.13C)

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 carburized parts requiring high minimum core hardness with a narrow range, reduced distortion and subject to magnetic particle inspection standards, but usage is not limited to such applications.

Steel Bars and Forgings 3.5Cr 7.5Ni 16.3Co 1.75Mo 0.2W (0.09-0.13C) Double Vacuum Melted, Normalized, Annealed

SAE AMS6526G-2012 自耗电极真空再熔化退火钢棒,钢铸件,钢管和钢环1.0Cr 7.5Ni 4.5Co 1.0Mo 0.09V(0.29-0.34C)

This specification covers a premium aircraft-quality, high-strength, 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 parts requiring through hardening to high strength levels and when 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; ARP 1110 recommends practices to minimize such conditions.

Steel, Bars, Forgings, Tubing and Rings, 1.0Cr 7.5Ni 4.5Co 1.0Mo 0.09V (0.29-0.34C), Consumable Electrode Vacuum Remelted, Annealed

SAE AMS6431N-2012 真空自耗电极再熔化钢棒,钢铸件和钢管1.05Cr 0.55Ni 1.0Mo 0.11V(0.45-0.50C)(D6AC)

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for ultra-high-strength structural applications requiring a through-hardening, weldable steel for use up to 600 °F (316 °C), but usage is not limited to such applications.

Steel, Bars, Forgings, and Tubing 1.05Cr 0.55Ni 1.0Mo 0.11V (0.45-0.50C) (D6AC) Vacuum Consumable Electrode Remelted

SAE AMS4186D-2012 在焊接,或当指定条件下,退火(7075-0)轧制或冷轧制5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-F)铝合金棒,条和线材

This specification covers an aluminum alloy in the form of bars, rods, and wire in the as fabricated (F) temper. When specified, product shall be supplied in the annealed (O) condition. These products have been typically used for parts requiring forming and as stock for flash welded rings which are to be subsequently solution and precipitation 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 solution and precipitation heat treatment; ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy Bars, Rods, and Wire, Rolled or Cold Finished, 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-F) As Fabricated, or when specified, Annealed (7075-0)

SAE AMS6267H-2012 1.2Cr 3.25Ni 0.12Mo (0.07-0.13C)(9310)电渣焊接法再融化或电极真空再融耗材钢棒,锻件或管件

This specification covers a premium 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 requiring high minimum core hardness with a narrow range and subject to stringent magnetic particle inspection standards, but usage is not limited to such applications.

Steel Bars, Forgings, and Tubing, 1.2Cr 3.25Ni 0.12Mo (0.07-0.13C) (9310) Electroslag Remelted or Consumable Electrode Vacuum Remelted

SAE AMS6930D-2012 6.0Al 4.0V溶解热处理和老化锻件和锻坯钛合金棒

This specification covers a titanium alloy in the form of bars, forgings, and stock for forging. These products have been used typically for parts which are machined after solution heat treatment and aging and are suitable for parts requiring high strength-to-weight ratios up to moderately elevated temperatures, but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion; SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy Bars, Forgings and Forging Stock 6.0Al 4.0V Solution Heat Treated and Aged

SAE AMS4456-2012 溶解热处理压力应力消除和过旧的铝合金手持锻件8.0Zn 1.0Cu 1.6Mg 0.12Zr (7037-T7452)

This specification covers an aluminum alloy in the form of hand forgings 11 inches (280 mm) and under in nominal thickness, and of forging stock.

Aluminum Alloy, Hand Forgings 8.0Zn 1.0Cu 1.6Mg 0.12Zr (7037-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged

SAE AIR4498A-2012 300M钢的奥氏体机舱淬火

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. The object of this program is to compare the properties of aus-bay quenched 300M steel with the properties of 300M steel oil quenched in the conventional manner.

AUS-Bay Quenching of 300M Steel

NF L10-584*NF EN 4656:2012 航空航天系列.FE-PM1507型钢(X1CrNiMoAlTi12-11-2).真空感应融化和自耗电极融化.溶液处理和沉淀处理.棒材.a或De≤200 mm Rm≥1520MPa

Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D < or = 200 mm - Rm > or = 1 520 MPa.

DIN EN 3355:2012 航空航天系列. 钛合金TI-P64001 (Ti-6Al-4V). 退火. 挤压型材. De ≤ 150 mm. 900 MPa ≤ Rm ≤ 1160 MPa; 德文和英文版本EN 3355-2012

Aerospace series - Titanium alloy TI-P64001 (Ti-6AI-4V) - Annealed - Extruded section - D_e 150 mm - 900 MPa R_m 1 160 MPa; German and English version EN 3355:2012

DIN EN 3312:2012 航空航天系列. Ti-6Al-4V型钛合金. 退火. 锻件. D<(下标)e> <小于 => 150 mm; 德文和英文版本EN 3312-2012

Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Forgings - D_e 150 mm; German and English version EN 3312:2012