49.025.99 其他材料 标准查询与下载

SAE AIR4938A-2014 复合材料和胶合件结构技术工人/专业培训文件

This is a general curriculum that has been developed to identify the minimum knowledge and skill requirements of a composite and/or metal bond repair technician/specialist. This revision changes the document from an all-inclusive curriculum into a modular set of curricula. Teaching levels have been assigned to the curriculum to define the knowledge, skills and abilities graduates will need to make composite repairs. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter - lecture and laboratory. These minimums may be exceeded, and may include an increase in the total number of training hours and/or increases in the

Composite and Bonded Structure Technician/Specialist Training Document

NF L17-099*NF EN 3102:2014 航空航天系列. 密封剂. 试验方法. 低温柔韧性的测定

La présente norme européenne définit la méthode d'essai pour la détermination de l'opérabilité d'un produit d'étanchéité pendant ou après l'application d'une charge de pliage à basses températures (flexibilité à basse température).

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

SAE AMS5834D-2014 真空感应阳极消耗熔解热处理,冷拉,以及老化20Cr - 15Ni - 40Co - 7.0Mo - 16Fe耐腐蚀和耐高温钴合金圆线

This specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.140 inch (3.56 mm) and under in nominal diameter supplied in straight lengths. (See 8.5.) This wire has been used typically for springs and torsion bars requiring a combination of high strength up to 800 °F (427 °C), excellent corrosion resistance, and good fatigue properties, but usage is not limited to such applications. The alloy is nonmagnetic.

Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Cold Drawn, and Aged

SAE AMS5833D-2014 溶解热处理和冷拉20Cr - 15Ni - 40Co - 7.0Mo - 16Fe耐高温耐腐蚀钴合金圆线

Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Solution Heat Treated and Cold Drawn

SAE AMS4362G-2014 5.5Zn 0.45Zr (ZK60A-T5)沉淀热处理的镁合金锻件

This specification covers a magnesium alloy in the form of die forgings, hand forgings, and forging stock.

Forgings, Magnesium Alloy, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated

SAE AMS4424L-2014 溶液和沉淀热处理的砂型铸造镁合金铸件6.0Al - 3.0Zn (AZ63-T6)

This specification covers a magnesium alloy in the form of sand castings.

Magnesium Alloy Castings, Sand 6.0Al - 3.0Zn (AZ63-T6) Solution and Precipitation Heat Treated

SAE AMS4437F-2014 镁合金铸件,砂模8.7Al - 0.70Zn (AZ91C-T6) 熔解热处理和老化

Magnesium Alloy Castings, Sand 8.7Al - 0.70Zn (AZ91C-T6) Solution Heat Treated and Aged

DIN EN 3866:2014 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.德文和英文版本EN 3866-2013

Aerospace series - Non-metallic materials - Glass tranparencies - Test methods - Determination of ream and surface ripple; German and English version EN 3866:2013

ASTM D2532-14 飞行器涡轮机润滑剂承受低温后粘度和粘度变化的标准试验方法

5.1 Aircraft turbine lubricants, upon standing at low temperatures for prolonged periods of time, may show an increase in kinematic viscosity. This increase may cause lubrication problems in aircraft engines. Thus, this test method is used to ensure that the kinematic viscosity does not exceed the maximum kinematic viscosity in certain specifications for aircraft turbine lubricants. 1.1 This test method covers the determination of the kinematic viscosity of aircraft turbine lubricants at low temperature, and the percent change of viscosity after a 38201;h and a 728201;h standing period at low temperature. 1.1.1 The range of kinematic viscosities covered by this test method is from 7700 mm2/s to 148201;0008201;mm2/s at –408201;°C and from 7000 mm2/s to 178201;5008201;mm2/s at –518201;°C. The precision has only been determined for those materials, kinematic viscosity ranges, and temperatures as shown in the precision section. Kinematic viscosities and percent change of viscosity may be measured and reported at other temperatures and other thermal soak period intervals as agreed by the contracting parties. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.2.1 The SI unit used in this test method for Kinematic Viscosity is mm2/s. For user reference, 1 mm2/s = 10-6 m2/s = 1 cSt. 1.3 WARNING—Mercury has been designated by many regulatory agencies as a hazardous material that can cause central nervous system, kidney and liver damage. Mercury, or its vapor, may be hazardous to health and corrosive to materials. Caution should be taken when handling mercury and mercury containing products. See the applicable product Material Safety Data Sheet (MSDS) for details and EPA’s website—http://www.epa.gov/mercury/faq.htm—for additional information. Users should be aware that selling mercury and/or mercury containing products into your state or country may be prohibited by law. 1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements, see Section 7.

Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants

SAE AMS5388J-2013 53.3Ni-16.5Cr-17Mo-4.5W-5.8Fe-0.40V (CW-12MW)耐腐蚀和耐热镍合金熔模毛胚铸件

Nickel Alloy, Corrosion and Heat Resistant, Investment Castings 53.3Ni - 16.5Cr - 17Mo - 4.5W - 5.8Fe - 0.40V (CW-12MW), As-Cast

SAE AMS7882B-2013 结块和烧结的碳化钨钴铬粉末

This specification covers tungsten carbide-cobalt chrome in the form of powder.

Tungsten Carbide-Cobalt Chrome Powder, Agglomerated and Sintered

SAE AMS5390F-2013 47.5Ni-22Cr-1.5Co-9Mo-0.6W-18.5Fe(N-12MV)耐热和耐腐蚀的镍合金熔模毛胚铸件

Nickel Alloy, Corrosion and Heat Resistant, Investment Castings, 47.5Ni - 22Cr - 1.5Co - 9Mo - 0.6W - 18.5Fe (N-12MV) As-Cast

SAE AMS5391G-2013 真空铸造的耐热和耐腐蚀镍合金熔模毛胚铸件73Ni-13Cr-4.5Mo-2.3Cb-0.75Ti-6.0Al-0.010B-0.10Zr

Nickel Alloy, Corrosion and Heat Resistant, Investment Castings, 73Ni - 13Cr - 4.5Mo - 2.3Cb - 0.75Ti - 6.0Al - 0.010B - 0.10Zr Vacuum Cast, As-Cast

SAE AMS5377G-2013 真空铸造的73Ni-12Cr-4.5Mo-2.0Cb-0.70Ti-0.05C-6.0Al-0.010B-0.10Zr耐腐蚀和耐热镍合金熔模毛胚铸件

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

Nickel Alloy, Corrosion and Heat Resistant, Investment Castings 73ni - 12cr - 4.5mo - 2.0cb - 0.70ti - 0.05c - 6.0al - 0.010b - 0.10zr, Vacuum Cast, As-Cast

SAE AMS3006H-2013 酒精-水混合物

This specification covers mixtures of methyl alcohol and/or ethyl alcohol with water in the form of liquids.

Alcohol-Water Mixtures

SAE AMS5396E-2013 耐热和耐腐蚀镍合金熔模铸件65Ni-28Mo-5.5Fe-0.4V(N-12MV)

Nickel Alloy, Corrosion and Heat Resistant, Investment Castings, 65Ni - 28Mo - 5.5Fe - 0.4V (N-12MV), As-Cast

NF L17-709*NF EN 3864:2013 航空航天系列. 非金属材料. 玻璃透明度. 试验方法. 断裂模量测定

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

SAE AMS7850E-2013 钶 (铌) 薄板材, 带材, 板材以及箔材

This specification covers columbium in the form of sheet, strip, plate, and foil. This material has been used typically for parts requiring exposure to ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating. Although produced in the cold rolled condition, this material is intended to be used in the annealed condition.

Columbium (Niobium) Sheet, Strip, Plate, and Foil

SAE AMS7879F-2013 硬质合金-钴粉,铸件和压碎

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

Tungsten Carbide-Cobalt Powder, Cast and Crushed

SAE AMS4426B-2013 溶液和沉淀热处理的镁合金磨光铸件5.1Y-3.0Re-0.70Zr(WE54-T6)

This specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for parts requiring high yield strength up to 570 degrees F (299 degrees C) and excellent corrosion resistance, but usage is not limited to such applications.

Castings, Sand, Magnesium Alloy 5.1Y - 3.0Re - 0.70Zr (WE54 - T6) Solution and Precipitation Heat Treated