49.025.99 其他材料 标准查询与下载

BS EN 3094:2017 航空航天系列. 密封剂. 试验方法. 申请时间的确定

Aerospace series. Sealants. Test method. determination of the application time

EN 3094:2017 航空航天系列密封剂试验方法使用时间的测定

Aerospace series - Sealants - Test method - determination of the application time

BS 3L 500:2011+A1:2017 变形镁基合金的检验、测试和验收程序

Procedure for inspection, testing and acceptance of wrought magnesium base alloys

ASTM D2532-17 飞机涡轮润滑剂低温下粘度和粘度变化的标准试验方法

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 3 h and a 72 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 14 000 mm2 /s at –40 °C and from 7000 mm2 /s to 17 500 mm2 /s at –51 °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. 1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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

17/30354462 DC BS 3L 500 AMD1 变形镁基合金的检验、测试和验收程序

BS 3L 500 AMD1. Procedure for inspection, testing and acceptance of wrought magnesium base alloys

ASTM D2532-16 飞机涡轮润滑剂低温下粘度和粘度变化的标准试验方法

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

GSO ASTM D5972:2016 航空燃料凝固点的标准测试方法（自动相变法）

1.1 This test method covers the determination of the temperature below which solid hydrocarbon crystals form in aviation turbine fuels. 1.2 This test method is designed to cover the temperature range of 80 to 20C; however, 2003 Joint ASTM /IP Interlaboratory Cooperative Test Program mentioned in has only demonstrated the test method with fuels having freezing points in the range of 42 to 60C. 1.3 The values stated in SI units are to be regarded as the standard. 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 warning statements, see 7.1, 7.3, and 7.5.

Standard Test Method for Freezing Point of Aviation Fuels ( Automatic Phase Transition Method )

SAE AMS5798H-2016 镍合金 耐腐蚀耐热 焊丝 47.5Ni 22Cr 1.5Co 9.0Mo 0.60W 18Fe（UNS N06002）

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

Nickel Alloy@ Corrosion and Heat-Resistant@ Welding Wire 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18Fe (UNS N06002)

SAE AMS2774E-2016 热处理锻造镍合金和钴合金零件

This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts made of wrought nickel or cobalt alloys, of raw materials during fabrication, and of fabricated assemblies in which wrought nickel or cobalt alloys are the primary structural components.

Heat Treatment Wrought Nickel Alloy and Cobalt Alloy Parts

ASTM D5972-16 航空燃料凝固点的标准试验方法 (自动相变法)

5.1 The freezing point of an aviation fuel is the lowest temperature at which the fuel remains free of solid hydrocarbon crystals. These crystals can restrict the flow of fuel through the fuel system of the aircraft. The temperature of the fuel in the aircraft tank normally decreases during flight depending on aircraft speed, altitude, and flight duration. The freezing point of the fuel must always be lower than the minimum operational fuel temperature. 5.2 Petroleum blending operations require precise measurement of the freezing point. 5.3 This test method produces results which have been found to be equivalent to Test Method D2386 and expresses results to the nearest 0.18201;°C, with improved precision over Test Method D2386. This test method also eliminates most of the operator time and judgment required by Test Method D2386. 5.4 When specification requires Test Method D2386, do not substitute this test method or any other test method. 1.1 This test method covers the determination of the temperature below which solid hydrocarbon crystals form in aviation turbine fuels. 1.2 This test method is designed to cover the temperature range of −808201;°C to 208201;°C; however, 2003 Joint ASTM/IP Interlaboratory Cooperative Test Program mentioned in 12.4 has only demonstrated the test method with fuels having freezing points in the range of −428201;°C to −608201;°C. 1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 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 warning statements, see 7.1, 7.3, and 7.5.

Standard Test Method for Freezing Point of Aviation Fuels (Automatic Phase Transition Method)

SAE AMS5679H-2015 镍合金 耐腐蚀和耐热 焊丝 73Ni 15.5Cr 2.2Cb 8.0Fe（UNS N06062）

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

Nickel Alloy@ Corrosion and Heat Resistant@ Welding Wire 73Ni - 15.5Cr - 2.2Cb - 8.0Fe (UNS N06062)

SAE AMS5786H-2015 镍合金 耐腐蚀和耐热 焊丝 62.5Ni 5.0Cr 24.5Mo 5.5Fe（UNS N10004）

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

Nickel Alloy@ Corrosion and Heat-Resistant@ Welding Wire 62.5Ni - 5.0Cr - 24.5Mo - 5.5Fe (UNS N10004)

SAE AMS5835D-2015 镍合金 耐腐蚀耐热 焊丝 72Ni 3.2Mn 20Cr 2.5Cb 0.48Ti 真空感应熔炼 环境控制包装（UNS N06082）

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

Nickel Alloy@ Corrosion and Heat-Resistant@ Welding Wire 72Ni - 3.2Mn - 20Cr - 2.5Cb - 0.48Ti Vacuum Induction Melted@ Environment Controlled Packaging (UNS N06082)

SAE AS5282A-2015 磁粉探伤用工具钢环

This SAE Aerospace Standard (AS) establishes requirements for the manufacture and certification of tool steel rings for magnetic particle inspection.

Tool Steel Ring for Magnetic Particle Inspection

SAE AMS7719E-2015 镍铁合金 磁性 板材和带材 50Ni 50Fe 冲压质量 半硬回火（UNS K95000）

This specification covers a magnetic nickel-iron alloy in the form of sheet and strip.

Nickel-Iron Alloy@ Magnetic@ Sheet and Strip 50Ni - 50Fe Stamping Quality@ Half-Hard Temper (UNS K95000)

SAE AMS7717E-2015 镍铁合金 磁性 薄板和带材 50Ni 50Fe 退火 成型等级（UNS K95000）

This specification covers a magnetically soft nickel-iron alloy in the form of sheet and strip.

Nickel-Iron Alloy@ Magnetic@ Sheet and Strip 50Ni - 50Fe Annealed@ Forming Grade (UNS K95000)

SAE AMS5879D-2015 镍合金 耐腐蚀和耐热 薄板 带材 和箔 62Ni 21.5Cr 9.0Mo 3.7Cb（Nb）冷轧和退火（UNS N06625/N06626）

This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness. (See 8.4).

Nickel Alloy@ Corrosion and Heat-Resistant@ Sheet@ Strip@ and Foil 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) Cold Rolled and Annealed (UNS N06625/N06626)

SAE AMS5701E-2015 镍合金 耐腐蚀和耐热 棒材 锻件 和环件 41.5Ni 16Cr 37Fe 2.9Cb（Nb） 1.8Ti 自耗电极重熔或真空感应熔炼 1800°（982°固溶热处理（ UNS N09706）

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.

Nickel Alloy@ Corrosion and Heat-Resistant@ Bars@ Forgings@ and Rings 41.5Ni - 16Cr - 37Fe - 2.9Cb (Nb) - 1.8Ti Consumable Electrode Remelted or Vacuum Induction Melted 1800 ��(982 �� Solution Heat Treated (UNS N09706)

SAE AMS4510H-2015 磷青铜 Sheet Strip and Plate 94.5Cu 4.0Sn 0.19P 弹簧回火（H08）（UNS C51000）

This specification covers a copper alloy (phosphor bronze) in the form of sheet, strip, and plate.

Phosphor Bronze@ Sheet@ Strip@ and Plate 94.5Cu - 4.0Sn - 0.19P Spring Temper (H08) (UNS C51000)

SAE AMS3679C-2015 绝缘，热，陶瓷纤维

This specification covers alumina-silica, glass, and other ceramic fiber thermal insulation in the form of felt and fabric flat sheets, rolls, or molded non-pliable blocks. Nominal thickness is 0.1 to 2.0 inches (3 to 51 mm) and nominal density is 2 to 24 pounds mass per cubic foot (32 to 384 kg/m)

Insulation, Thermal, Ceramic Fiber