49.025.15 有色金属合金综合 标准查询与下载

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

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

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De 200 mm

BS EN 4373:2007 航空航天系列.NI-PD9001(NiCu31)型耐热合金.退火无缝管.D≤75mm、a≤3mm

This standard specifies the requirements relating to: Heat resisting alloy NI-PD9001 (NiCu31) — Annealed, seamless tube D ≤ 75 mm, a ≤ 3 mm for aerospace applications.

Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D ≤ 75 mm, a ≤ 3 mm

SAE AMS4501E-2008 自由氧化冷轧的铜片材,带材和板材

This specification covers one type of copper in the form of sheet, strip, and plate

Copper Sheet, Strip, and Plate, Oxygen-Free, Light Cold Rolled

SAE AMS5709H-2008 自耗电极或真空感应熔炼的1975℉(1079℃)溶解、稳定、沉淀处理的58Ni19.5Cr13.5Co4.3Mo3.0Ti1.4Al0.05Zr0.006B镍合金耐腐蚀、耐热棒材和锻件

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and forging stock. These products have been used typically for parts, such as pins, nuts, and turbine blades, requiring high strength up to 1500 ?F (816 ?C) and oxidation resistance up to 1750 ?F (954 ?C), but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat-Resistant, Bars and Forgings 58Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1975 °F (1079 °C) Solution, Stabilization, and Precipitation Heat Treated UNS N

SAE AMS5704J-2008 自耗电极或真空感应熔炼、1825～1900℉(996～1038℃)溶解、稳定、沉淀热处理的57Ni19.5Cr13.5Co4.3Mo3.0Ti1.4Al0.05Zr 0.006B锻件用耐腐蚀、耐热镍合金

This specification covers a corrosion and heat resistant nickel alloy in the form of forgings and forging stock. These forgings have been used typically for rotating parts, such as compressor blades, discs, hubs, shafts, and spacers requiring high strength up to 1500 ?F (816 ?C) and oxidation resistance up to 1750 ?F (954 ?C), but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Forgings 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1825 to 1900 Degrees F (996 to 1038 Degrees C) Solution, Stabilization, and Precipitatio

LST EN 4379-2008 航天系列 耐热合金 NI-PH3601（NiCr22Mo9Nb） 固溶处理，锻造 200 毫米

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ? 200 mm

NF L10-712*NF EN 4373:2008 航空航天系列.耐热合金 NI-PD9001 (NiCu31).退火、无缝管.D≤75 mm、a≤3mm

Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D < or = 75 mm, a < or = 3 mm.

DS/EN 4379:2007 航天系列 耐热合金 NI-PH3601（NiCr22Mo9Nb） 固溶处理，锻造 De <= 200 mm

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

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De <= 200 mm

LST EN 4373-2007 航空航天系列-耐热合金NI-PD9001（NiCu31）-退火、无缝管

Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D ? 75 mm, a ? 3 mm

DS/EN 4373:2007 航空航天系列 耐热合金 NI-PD9001（NiCu31） 退火无缝管 D <= 75 mm, a <= 3 mm

This standard specifies the requirements relating to:Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D

Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D <= 75 mm, a <= 3 mm

DIN EN 4384:2007 航空航天系列.NI-CH1303(NiCo20Cr20Mo5Ti2Al)型耐热合金.非热处理.再熔炼坯料

This standard specifies the requirements relating to: Heat resisting alloy N I-CH1303 (NiCo20Cr20Mo5Ti2AI) Non heat treated Rernelting stock for aerospace applications.

Aerospace series - Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) - Non heat treated - Remelting stock; German and English version EN 4384:2007

SAE AMS-L-18331A-2007 铅合金生铁

This specification covers pigs of one type of lead alloy used in the making of forming dies.

Lead Alloy Pig

NF L11-001*NF EN 3668:2007 航空航天系列.NI-PH2301(NiCr21Fe18Mo9)型耐热合金.非热处理.锻坯.液压用.a或D≤250mm

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

EN 4373:2007 航空航天系列.NI-PD9001(NiCu31)型耐热合金.退火无缝管.D≤75 mm,a≤3 mm

This standard specifies the requirements relating to: Heat resisting alloy NI-PD9001 (NiCu31)-Annealed, seamless tube D 75 mm, a 3 mm for aerospace applications.

Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D <= 75 mm, a <= 3 mm

SAE AMS4396E-2007 3.2稀土族2.5锌0.72锆镁合金焊丝(EZ33A)

This specification covers a magnesium alloy in the form of welding wire. This wire has been used typically as filler metal for gas-metal-arc and gas-tungsten-arc welding of magnesium alloys of similar composition, but usage is not limited to such applications.

Magnesium Alloy Welding Wire 3.2 Rare Earths 2.5Zn 0.72Zr (EZ33A)

SAE AMS5589E-2007 1775°F (968°C)溶解热处理的52.5Ni 19Cr 3.0Mo 5.1Cb 0.90Ti 0.50Al 18Fe自耗电极或真空感应熔炼的耐腐蚀耐高温镍合金无缝管材

This specification covers a corrosion and heat resistant nickel alloy in the form of seamless tubing. This tubing has been used typically for fluid lines and components requiring resistance to creep and stress-rupture up to 1300 °F (704 °C) and oxidation resistance up to 1800 °F (982 °C), particularly those parts which are formed or welded and then heat treated to develop desired properties, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat-Resistant, Seamless Tubing 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode Remelted or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated Composition similar to UNS N07718

SAE AMS5599G-2007 62Ni 21.5Cr 9.0Mo 3.7 Cb (Nb)溶解热处理耐腐蚀和耐高温的镍合金薄板材、带材和厚板材

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in inch/pound units. These products have been used typically for parts requiring corrosion and oxidation resistance up to 2000 °F (1095 °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 62Ni - 21.5Cr - 9.0Mo - 3.7 Cb (Nb) Solution Heat Treated UNS N06625

LST EN 3668-2007 航空航天系列 耐热合金 NI-PH2301（NiCr21Fe18Mo9） 非热处理 锻件

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

SAE AMS5713J-2007 53Ni 19Cr 11Co 9.8Mo 3.2Ti 1.6Al 0.006B溶解和沉淀热处理真空熔炼的耐腐蚀和耐高温镍合金棒材、锻件和环形材

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 to 1600 °F (871 °C) 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 - 1.6A1 - 0.006B Vacuum Melted, Solution and Precipitation Heat Treated UNS N07041

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