49.025.99 其他材料 标准查询与下载

ASTM D2532-10 航空涡轮发动机用润滑剂在低温条件下的粘度和粘度变化的标准试验方法

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 3-h and a 72-h standing period at low temperature. 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 units for Kinematic Viscosity are mm2/s. For user reference, 1 mm2/s = 10-6 m2/s = 1 cSt. 1.3 WARNINGMercury 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 websitehttp://www.epa.gov/mercury/faq.htmfor 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 6.

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

BS 2B 100:2009 锻造铜合金的检查、测试和验收程序

This British Standard specifies procedures for the inspection, testing and acceptance of wrought copper alloys for aerospace purposes. The standard is applicable to material specifications in the British Standard Aerospace B series and also to other British Standard material specifications for wrought copper alloys which are suitable for aerospace use.

Procedure for inspection, testing and acceptance of wrought copper alloys

SAE AMS1424J-2009 飞机用SAE 1型除冰/自动防结冰液

This specification covers a deicing/anti-icing material in the form of a fluid. The fluid is generally used heated either diluted with water, or as supplied, for the removal of, and time-limited protection against, deposits of frost, ice, and snow on exterior aircraft surfaces prior to takeoff. Consult aircraft manufacturer's maintenance manual and service letters to determine any restrictions relating to the use of deicing/anti-icing fluids for type and model of aircraft being treated. Refer also to SAE ARP 4737. The manufacturer shall determine and report the lowest operational use temperature (LOUT) for the recommended dilutions of their fluid(s). The LOUT for an SAE Type I fluid is the lowest temperature at which the fluid has been tested and certified in accordance with the appropriate aerodynamic acceptance tests (3.5.3) while maintaining the 10 °C (18 °F) freezing point buffer (see SAE ARP 4737).

Deicing/Anti-Icing Fluid, Aircraft, SAE Type 1

SAE AMS7850D-2009 钶(铌)薄板,带材,板材及薄片材

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 AMS5597F-2009 1950°F (1066°C)溶解热处理条件下自耗电极或真空感应融化的抗腐蚀耐热52.5Ni 19Cr 3.0Mo 5.1Cb (Nb) 0.90Ti 0.50Al 18Fe镍合金带,片和板

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, such as cases and ducts, requiring high strength at cryogenic temperatures and for short-time use up to 1000 °F (538 °C), particularly 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, 52.5Ni 19Cr 3.0Mo 5.1Cb (Nb) 0.90Ti 0.50Al 18Fe, Consumable Electrode or Vacuum Induction Melted, 1950°F (1066°C) Solution Heat Treated

BS 2B 24:2009 铜-锡磷合金棒材和型材规范

This British Standard specifies requirements for copper-tinphosphorous alloy supplied in the form of rods, including hollow rods, and sections.

Specification for copper-tin-phosphorous alloy rods and sections

BS 2HR 207:2009 镍-铁-铬-钼-铝-钛热阻合金板材、薄板材和带材规范(镍/钴 43.5、铬 16.5、钼 3.3、铝 1.2、钛 1.2、其余部分为铁)

This British Standard specifies requirements for nickel-iron-chromiummolybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip.

Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)

BS 2HR 206:2009 镍-钴-铬-钼-钛-铝热阻的合金板材、片材和带材规范（镍基合金，钴 20、钼 5.9、钛 2.1、铝 0.5）

This British Standard specifies requirements for nickel-cobaltchromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip.

Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)

BS 2HR 204:2009 镍-铬-铁-钼-钴-钨耐热合金厚板材、薄板材和带材用规范(镍基、Cr 21.7、Fe 18.5、Mo 9、Co 1.5、W 0.6)

This British Standard specifies requirements for nickel-chromium-ironmolybdenum- cobalt-tungsten heat-resisting alloy plate, sheet and strip.

Specification for nickel-chromium-iron-molybdenum-cobalt-tungsten heat-resisting alloy plate, sheet and strip (nickel base, Cr 21.7, Fe 18.5, Mo 9, Co 1.5, W 0.6)

BS 2B 23:2009 铜-铝-镍-铁合金棒材、条材、型材、锻坯和锻件规范

This British Standard specifies requirements for copper-aluminiumnickel- iron alloy supplied in the following forms: a) rods, bars and sections: as manufactured, designation B 23A; b) forging stock: as manufactured, designation B 23B; c) forgings: as manufactured, designation B 23C.

Specification for copper-aluminium-nickel-iron alloy rods, bars, sections, forging stock and forgings

BS 2HR 203:2009 镍-铬-钛热阻合金板材、薄板材和带材规范（镍基合金，铬20、19.5、钛0.4）

This British Standard specifies requirements for nickel-chromiumtitanium heat-resisting alloy plate, sheet and strip.

Specification for nickel-chromium-titanium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 0.4)

BS 2HR 205:2009 镍-铜热阻的合金薄板材和带材规范:退火的(镍基合金,铜31)

This British Standard specifies requirements for nickel-copper alloy sheet and strip.

Specification for nickel-copper alloy sheet and strip: annealed (nickel base, Cu 31)

BS 3HR 202:2009 镍-铬-钴-钛-铝的热阻合金薄板材和带材规范（镍基合金，铬 19.5、钴 18.0、钛 2.5、铝 1.5）

This British Standard specifies requirements for nickel-chromiumcobalt-titanium-aluminium heat-resisting alloy sheet and strip.

Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy sheet and strip (nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)

BS 3B 27:2009 铜-锌-铝-镍-硅合金管规范

This British Standard specifies requirements for copper-zincaluminium-nickel-silicon alloy supplied in the form of tube.

Specification for copper-zinc-aluminium-nickel-silicon alloy tube

BS 3HR 201:2009 镍-铬-钛-铝热阻合金板材、薄板材和带材规范(镍基合金,铬19.5、钛2.2、铝1.4)

This British Standard specifies requirements for nickel-chromiumtitanium-aluminium heat‑resisting alloy plate, sheet and strip.

Specification for nickel-chromium- titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 2.2, Al 1.4)

BS 2HR 208:2009 镍-铬-铁合金板材、片材和带材规范:退火的(镍基合金,铬 15.5、铁 8)

This British Standard specifies requirements for nickel-chromium-iron alloy plate, sheet and strip.

Specification for nickel-chromium-iron alloy plate, sheet and strip: annealed (nickel base, Cr 15.5, Fe 8)

SAE AMS4845H-2009 锡青铜铸件87.5Cu 10Sn 2Zn铸态,沙子和转筒

This specification covers a tin bronze in the form of sand and centrifugal castings. These casting have been typically for bearing requiring a combination of strength, toughness, and resistance to wear, but usage is not limited to such applications. The alloy has good machinability and corrosion resistance to sea water.

Tin Bronze Castings, Sand and Centrifugal, 87.5Cu 10Sn 2Zn, As Cast

SAE AMS5836C-2009 耐腐蚀和耐热镍合金72Ni-3.0Mn-20Cr-2.5Cb(Nb)焊丝

This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of parts fabricated from high nickel alloys or combinations of such alloys and corrosion-resistant or plain-carbon steels, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 72Ni 3.0Mn 20Cr 2.5Cb(Nb)

SAE AMS4701G-2009 无氧铜丝 99.95 (Cu+Ag)煅烧

This specification covers one type of copper in the form of wire. This wire has been used typically for copper brazing, high-conductivity bonding, and emergency lockwiring, but usage is not limited to such applications.

Copper Wire, Oxygen-Free, 99.95 (Cu+Ag) Annealed

SAE AMS5839B-2009 镍合金焊条59Ni 22Cr 2.0Mo 14W 0.35Al的耐腐蚀和耐热性

This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire. This wire has been used typically as filler metal for gas- metal-arc or gas-tungsten-arc welding of parts fabricated from alloy of similar composition, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 59Ni 22Cr 2.0Mo 14W 0.35Al