49.025.99 其他材料 标准查询与下载

SAE AMS5920A-2013 真空感应加真空自耗电极融化溶解热处理工作增强和老化,改进强度耐蚀耐热钴镍合金圆棒材19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe

This specification covers a corrosion and heat-resistant, work strengthened and aged cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter. These bars have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 170 ksi (1172 MPa) for use up to 850 °F (454 °C) in applications requiring high ductility to promote toughness and resistance to cracking under shock loading conditions, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice corrosion, and stress-corrosion cracking.

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

SAE AMS5919A-2013 改良强度真空感应加真空自耗点击融化溶解热处理和加工加强耐腐蚀和耐高温19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe钴镍合金圆条

This specification covers a corrosion and heat-resistant, work strengthened cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter. These bars have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 170 ksi (1172 MPa) for use up to 850 °F (454 °C) in applications requiring high ductility to promote toughness and resistance to cracking under shock loading conditions, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice corrosion, and stress-corrosion cracking.

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

SAE AMS4533D-2013 溶解和沉淀热处理(TF00,原AT)98Cu 1.9Be铜铍合金条和棒

This specification covers a copper-beryllium alloy in the form of bars and rods. These products have been used typically for parts requiring a combination of high strength, wear resistance, and corrosion resistance and where thermal conductivity, electrical conductivity and low magnetic susceptibility may be important, but usage is not limited to such applications.

Copper-Beryllium Alloy, Bars and Rods 98Cu 1.9Be Solution and Precipitation Heat Treated (TF00, formerly AT)

SAE AMS2667G-2013 小型加压配件用铜焊银钎料

This specification covers the engineering requirements for producing brazed joints in parts fabricated from austenitic corrosion and heat resistant steels, carbon or low-alloy steels, copper alloys, and the properties of such joints. This process has been used typically for producing joints brazed between flexible metal hose, pressure fillings, pipe and tube joints, and similar parts, such as bellows and rigid end fittings where one end of the joint is not accessible for inspection, but usage is not limited to such applications.

Brazing, Silver For Small Pressurized Fittings

SAE AMS4534C-2013 溶解热处理,冷加工和沉淀热处理(TH04,原HT)98Cu 1.9Be铜铍合金条和棒

This specification covers a copper-beryllium alloy in the form of bars and rods. These products have been used typically for parts requiring a combination of high strength, wear resistance, and corrosion resistance, and where thermal conductivity, electrical conductivity and low magnetic susceptibility may be important, but usage is not limited to such applications.

Copper-Beryllium Alloy, Bars and Rods 98Cu 1.9Be Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (TH04, formerly HT)

EN 3102:2013 航空航天系列.密封剂.试验方法.低温韧性的测定

This European Standard defines the test method for the determination of the operability of a cured sealant during and after submission to a bending load at low temperatures (low-temperature flexibility).

Aerospace series - Sealants - Test methods - Determination of low-temperature flexibility

BS EN 3862:2013 航空航天系列.非金属材料.材料标准.化学方法热处理碱石灰浮法玻璃

Aerospace series. Non-metallic materials. Glass transparencies. Material standard. Chemically tempered soda lime float glass

BS EN 3866:2013 航空航天系列.非金属材料.玻璃软片.试验方法.绞孔和表面波纹的测定

Aerospace series. Non-metallic materials. Glass tranparencies. Test methods. Determination of ream and surface ripple

BS EN 3863:2013 航空航天系列.非金属材料.玻璃透明胶片.试验方法.平整度的测定

Aerospace series. Non-metallic materials. Glass transparencies. Test methods. Determination of flatness

BS EN 3861:2013 航空航天系列.非金属材料.玻璃透明胶片.材料标准.热钢化碱石灰浮法玻璃

Aerospace series. Non-metallic materials. Glass transparencies. Material standard. Thermally tempered soda lime float glass

SAE AMS2281B-2013 高温高压应用的微量元素控制的镍合金,钴合金和铁合金锻件

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. This specification establishes maximum permissible limits for elements not normally specified but which may occur in trace amounts in wrought nickel, cobalt, and iron alloy products. Control provided by this specification has been used typically for highly-stressed rotating parts, such as turbine discs, where control of trace elements is required to maitain elevated-temperature tensile, stress-rupture, creep, and low-cycle

Trace Element Control Nickel Alloy, Cobalt Alloy, and Iron Alloy Wrought Products for High-Temperature, High-Stressed Applications

SAE AMS5583E-2013 沉积可硬化拉伸强度至170 ksi (1172 MPa)真空融解热处理72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe,耐腐蚀耐高温镍合金无缝管件

This specification covers a corrosion and heat resistant nickel alloy in the form of seamless tubing. This tubing has been used typically for fluid-conducting lines requiring high strength up to 1100 degrees F (593 degrees C), but usage is not limited to such applications. Parts may be formed and then heat treated to improve strength at elevated temperatures.

Nickel Alloy, Corrosion and Heat Resistant, Seamless Tubing 72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe, Vacuum Melted Solution Heat Treated, Precipitation Hardenable to 170 ksi (1172 MPa) Tensile Strength

SAE AMS5582F-2013 溶解热处理,沉淀硬化至155 ksi (1069 MPa)抗张强度的镍合金耐蚀和耐热无缝管,72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe

This specification covers a precipitation hardenable, corrosion and heat resistant nickel alloy in the form of seamless tubing. This tubing has been used typically for fluid lines requiring high strength up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1800 degrees F (980 degrees C), but usage is not limited to such applications. Parts may be formed and then heat treated to improve strength at elevated temperatures.

Nickel Alloy, Corrosion and Heat Resistant, Seamless Tubing, 72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe, Solution Heat Treated, Precipitation Hardenable to 155 ksi (1069 MPa) Tensile Strength

EN 3861:2013 航空航天系列.非金属材料-玻璃幻灯片.材料标准热钢化苏打石灰浮法玻璃

This European Standard specifies the requirements relating to universally available and high light transmission, thermally tempered float glass plies, for aerospace applications.

Aerospace series - Non-metallic materials - Glass transparencies - Material standard - Thermally tempered soda lime float glass

EN 3862:2013 航空航天系列.非金属材料-玻璃幻灯片.材料标准化学钢化苏打石灰浮法玻璃

This European Standard specifies the requirements relating to universally available and high light transmission, chemically tempered float glass plies, for aerospace applications.

Aerospace series - Non-metallic materials - Glass transparencies - Material standard - Chemically tempered soda lime float glass

EN 3866:2013 航空航天系列.非金属材料.玻璃tranparencies测试方法.决心令和表面的涟漪

This European Standard defines a qualitative method for the determination of the ream and surface ripple in glass transparencies for aircraft applications.

Aerospace series - Non-metallic materials - Glass tranparencies - Test methods - Determination of ream and surface ripple

EN 3863:2013 航空航天系列.非金属材料.玻璃幻灯片.测试方法测定平面度

This European Standard defines the requirements for the determination of the flatness of monolithic glass transparencies for aircraft applications. The method is designed to eliminate the effect of the glass deflecting under its own weight, thus eliminating false results.

Aerospace series - Non-metallic materials - Glass transparencies - Test methods - Determination of flatness

SAE AMS5536N-2012 47.5Ni 22Cr 1.5Co 9.0Mo 0.60W 18.5Fe溶液热处理的耐腐蚀和耐热镍合金片材、带材和板材

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 oxidation resistance up to 2200 °F and relatively high strength up to 1500 °F, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 47.5Ni 22Cr 1.5Co 9.0Mo 0.60W 18.5Fe, Solution Heat Treated

SAE AMS7875E-2012 碳化铬加镍铬合金粉末75Cr2C3+25(80Ni20Cr合金)

This specification covers a blend of chromium carbide and a nickel-chromium alloy in the form of powder. This product has been used typically for producing plasma spray coatings to provide wear and fretting resistant surfaces, but usage is not limited to such applications.

Powder, Chromium Carbide Plus Nickel-Chromium Alloy, 75Cr₂C₃ + 25(80Ni-20Cr Alloy)

SAE AMS7718G-2012 50Ni 50Fe镍铁合金磁棒材,棒条体,管材和铸件

This specification covers a magnetically soft nickel-iron alloy int he form of bars, rods, tubing, forgings, and forging stock. These products have been used typically for parts used in magnetic circuits requiring high magnetic permeability and high saturation induction with the fabricated parts to be annealed in dry hydrogen, but usage is not limited to such applications.

Nickel-Iron Alloy, Magnetic, Bars, Rods, Tubing, and Forgings 50Ni 50Fe