49.025.15 有色金属合金综合 标准查询与下载

SAE AS5706-2007 延伸距离的AS5643/1 S400型铜介质接口特性用试验规划/试验程序

This document establishes test plans/procedures for the AS5643/1 Slash Sheet. The AS5643/1 Slash Sheet establishes guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. It encompasses the data bus cable and its interface electronics for a system utilizing S400 over copper medium over extended lengths.

Test Plan/Procedure for AS5643/1 S400 Copper Media Interface Characteristics Over Extended Distances

BS EN 3671:2007 航空航天系列.NI-PH3601(NiCr22Mo9Nb)型耐热合金.非热处理.锻坯.a或D≤250mm

This standard specifies the requirements relating to: Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Non heat treated Forging stock a or D ≤ 250 mm for aerospace applications.

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Non heat treated - Forging stock - a or D 250 mm

DIN EN 3668:2007 航空航天系列.FE-PL1501(30CrMo12)型钢.非热处理的.锻件坯料.a或D≤250mm

This standard specifies the requirements relating to: Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9), non heat treated Forging stock a or D 250 mm for aerospace applications.#,,#

Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) - Non heat treated - Forging stock - a or D ≤ 250 mm; German and English version EN 3668:2006

EN 3671:2007 航空航天系列.NI-PH3601(NiCr22Mo9Nb)型耐热合金.非热处理.锻坯.a或D≤250mm

This standard specifies the requirements relating to: Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Non heat treated Forging stock a or D 250 mm for aerospace applications.

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Non heat treated - Forging stock - a or D <= 250 mm

DIN EN 4615:2007 航空航天系列.MG-C18002型镁合金.T4.砂型铸造

This standard specifies the requirements relating to: Magnesium alloy MG-C18002 T4 Sand casting for aerospace applications.

Aerospace series - Magnesium alloy MG-C18002 - T4 - Sand casting; German and English version EN 4615:2005

DIN EN 4616:2007 航空航天系列.型MG-C18002镁合金.T4.冷型铸造

This standard specifies the requirements relating to: Magnesium alloy MG-C18002 T4 Chill casting for aerospace applications.

Aerospace series - Magnesium alloy MG-C18002 - T4 - Chill casting; German and English version EN 4616:2005

DS/EN 3668:2007 航空航天系列 耐热合金 NI-PH2301（NiCr21Fe18Mo9） 非热处理 锻件 a 或 D <= 250 mm

This standard specifies the requirements relating to:Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9)Non heat treatedForging stocka or D

Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) - Non heat treated - Forging stock - a or D <= 250 mm

SAE AMS5964-2007 Ni 18Cr 2.8Mo 5.5Cb(Nb) 0.07Ti 1.50Al 10Fe 9Co 1W自耗电极再熔炼或真空感应炉熔炼的耐腐蚀和耐高温镍合金焊条

This specification covers a corrosion and heat-resistant nickel alloy in the form of welding wire.

Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire Ni - 18Cr - 2.8Mo - 5.5Cb(Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W Consumable Electrode Remelted or Vacuum Induction Melted UNS N07818

SAE AMS4500J-2007 软化退火的铜薄板材、带材和厚板材

This specification covers unalloyed copper in the form of sheet, strip, and plate. These products have been used typically for electrical components and for formed and drawn parts such as gaskets and washers, but usage is not limited to such applications.

Copper, Sheet, Strip, and Plate Soft Annealed UNS C11000

BS EN 3668:2007 航空航天系列 NI-PH2301（NiCr21Fe18Mo9）型耐热合金 非热处理的 锻坯 a或D≤250mm

Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) - Non heat treated - Forging stock - a or D 250 mm

BS EN 3668:2006 航空航天系列.NI-PH2301(NiCr21Fe18Mo9)型耐热合金.非热处理的.锻坯.a或D≤250mm

This standard specifies the requirements relating to: Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) Non heat treated Forging stock a or D ≤ 250 mm for aerospace applications.

Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) - Non heat treated - Forging stock - a or D ≤ 250 mm

EN 4379:2007 航空航天系列.NI-PH3601(NiCr22Mo9Nb)型耐热合金.溶解处理锻件.De≤200 mm

This standard specifies the requirements relating to: Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated, forging D ≤ 200 mm for aerospace applications.

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging Less than or equal to 200 mm

DIN EN 2731:2006 航空航天系列.镁合金钢 MG-C46001-T6.砂型铸造

This draft standard contains the AECMA-draft standard prEN 2731, edition April 1986.#,,#

Aerospace series - Magnesium alloy MG-C46001-T6 - Sand casting; German and English version EN 2731:2005

SAE AMS5712J-2006 1800°F (982°C) 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V消耗电极熔融和沉淀热处理的耐腐蚀和耐热钢棒材、线材、锻件、管材和环形材

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts, such as turbine rotors, shafts, bolts, dowels, and fittings, requiring high strength up 1600 °F (871 °C) after precipitation heat treatment and oxidation resistance up to 1800 °F (982 °C), but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable UNS N07041

SAE AMS5872E-2006 48Ni 20Cr 20Co 5.9Mo 2.2Ti 0.45Al消耗电极熔融和真空感应熔融溶液热处理的耐腐蚀和耐热镍合金薄板材、带材、厚板材

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 high strength up to 1500 °F (816 °C) and oxidation resistance up to 2000 °F (1093 °C), but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 48Ni - 20Cr - 20Co - 5.9Mo - 2.2Ti - 0.45Al Consumable Electrode or Vacuum Induction Melted Solution Heat Treated UNS N07263

SAE AMS5605E-2006 1800°F(982℃)溶液热处理可耗电极或感应熔化的镍合金片材、带材和板材41.5Ni 16Cr 37Fe 2.9Cb(Nb) 1.8Ti

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate 1.00 inch (25.4 mm) and under in nominal thickness. These products have been used typically for parts requiring good machinability and high strength at room and cryogenic temperatures and for short-time use up to 1000 degrees F (538 degrees C), particularly for those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 41.5Ni - 16Cr - 37Fe - 2.9Cb - 1.8Ti Consumable Electrode or Vacuum Induction Melted 1800 Degrees F (982 Degrees C) Solution Heat Treated UNS N09706

SAE AMS5747D-2006 溶液热处理和沉淀可硬化的耐腐蚀和耐热镍合金棒材、锻材和环材72Ni 15.5Cr 0.95Cb 2.5Ti 0.70Al 7.0Fe

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring high strength in the range 800 to 1100 °F (427 to 593 °C), but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe Solution Heat Treated, Precipitation Hardenable UNS N07750

SAE AMS4597-2006 溶液退火、冷精整和旋节硬化的铜镍锡合金棒材和杆材77Cu 15Ni 8Sn(TX TS)

This specification covers a copper-nickel-tin alloy in the form of bars and rods. These products have been used typically for parts requiring high strength, wear resistance and corrosion resistance at moderate temperatures, but usage is not limited to such applications.

Copper-Nickel-Tin Alloy, Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed, Cold Finished and Spinodal Hardened (TX TS)

SAE AMS5843E-2006 强度增强和老化的真空感应和真空可耗电极熔化溶液热处理的钴镍合金棒19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe

This specification covers a high strength, corrosion and heat resistant cobalt-chromium-nickel alloy in the form of bars. These bars have been used typically for applications requiring a combination of high strength up to 1100 degrees F (593 degrees C), good tension-tension fatigue strength, toughness, and ductility, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice-corrosion, stress-corrosion cracking, and elevated temperature relaxation.

Cobalt-Nickel Alloy, Corrosion and Heat Resistant, Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Work Strengthened, and Aged UNS R30159

SAE AMS5841E-2006 强度增强的真空感应和真空可耗电极熔化溶液热处理的钴镍合金棒19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe

This specification covers a high strength, corrosion and heat resistant cobalt-chromium-nickel alloy in the form of bars. These bars have been used typically for applications requiring a combination of high strength up to 1100 degrees F (593 degrees C), good tension-tension fatigue strength, toughness, and ductility, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice-corrosion, stress-corrosion cracking, and elevated temperature relaxation.

Cobalt-Nickel Alloy, Corrosion and Heat Resistant, Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated for Work Strengthening UNS R30159