49.025.99 其他材料 标准查询与下载

SAE AMS5870E-2012 溶解热处理耐腐蚀和耐高温的60.5Ni 23Cr 14Fe 0.35Ti 1.4Al镍合金薄板材,带材和板材

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 requiring corrosion and oxidation resistance up to 2200 degrees F (1204 degrees 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 60.5Ni 23Cr 14Fe 0.35Ti 1.4Al Solution Heat Treated

SAE AMS4427C-2012 溶解和沉积热处理4.0Y 2.3Nd 0.7Zr (WE43B - T6)砂模镁合金铸件

This specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for parts requiring a combination of light weight, high yield strength up to 570 °F (298 °C), and relatively high corrosion resistance, but usage is not limited to such applications.

Magnesium Alloy Castings, Sand 4.0Y 2.3Nd 0.7Zr (WE43B - T6) Solution and Precipitation Heat Treated

SAE AMS4418H-2012 溶解和沉淀热处理2.5Ag 2.1Di 0.70Zr (QE22A-T6)镁合金砂铸件

This specification covers a magnesium alloy in the form of sand castings. These casting have been used typically for parts requiring high yield strength up to 400 degrees F (204 degrees C), but usage is not limited to such applications.

Magnesium Alloy, Sand Castings 2.5Ag - 2.1Di - 0.70Zr (QE22A-T6) Solution and Precipitation Heat Treated (UNS M18220)

SAE AS1613B-2012 射线照相术图像质显示器

This document has been declared "Stabilized" and will no longer b subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. Newer technology may exist. This Aerospace Standard establishes an identification system and provides design and tolerance information in describing two series of image quality indicators currently used in radiography of aerospace components, especially in electronic component evaluation and radiographic film and paper classification.

Image Quality Indicator, Radiographic

SAE AIR4279A-2012 升温时间

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. An analysis was made of the effects of various surface conditions on the het up time of steel bars which are heated in atmosphere furnaces to the temperature range used for steel hardening or normalizing. The purpose was to examine whether a standard heating time for a given section thickness is acceptable.

Heat Up Time

SAE AIR6211-2012 跑道和滑行道除冰/防滑化学品用冰渗透试验方法

This test method provides stakeholders (runway deicing chemical manufacturers, deicing/anti-icing chemical operators and airport authorities) with a relative ice penetration capacity of runway deicing/anti-icing chemicals, by measuring the ice penetration as a function of time. Such runway deicing/anti-icing chemicals are often also used on taxiways and other paved areas. This test method does not quantitatively measure the theoretical or extended time of ice penetration capability of ready-to-use runway deicing/anti-icing chemicals in liquid or solid form.

Ice Penetration Test Method for Runways and Taxiways Deicing/Anti-icing Chemicals

SAE AMS5553G-2012 退火的低(最大0.02)碳镍制薄板材和带材

This specification covers nickel in the form of sheet and strip. These products have been used typically for parts requiring excellent corrosion resistance, and/or strong magnetic properties, but usage is not limited to such applications.

Nickel, Sheet and Strip, Low (0.02 max) Carbon, Annealed

SAE AS6449A-2012 氧气,饮用水,液体和其他系统等流体配件的固体薄膜润滑剂

This document establishes the requirements for a dry film lubricant AS6449 lubricant for use on breathing oxygen system and potable water system components, for a temperture range of -90 °F to +300 °F. This document also establishes the Non-Destructive Test (NDT) procedures and criteria for coated production parts. This document requires qualified products and product applicators.

Solid Film Lubricant for Fluid Fittings in Oxygen, Potable Water, Hydraulic, and Other Systems

SAE AMS1424K-2012 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 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 18 °F (10 °C) freezing point buffer (see SAE ARP 4737).

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

SAE AMS7725E-2012 高密度烧结的钨合金型材

This specification covers four classes of tungsten heavy metal in the form of sintered and annealed shapes. This material has been used typically for parts, such as counterbalance weights or projectiles, for which mechanical properties are tested from the sintered and annealed shapes and that require high weight per unit volume, but usage is not limited to such applications.

Tungsten Alloy Shapes, Sintered, High Density

SAE AIR6172-2012 跑道和滑行道除冰/防冰化学制剂的冰去除试验方法

This test method provides stakeholders (runway deicing chemical manufacturers, deicing/anti-icing chemical operators and airport authorities) with relative ice undercutting capacity of runway deicing chemicals, by measuring the area of ice undercut pattern as a function of time. Such runway deicing chemicals are often also used on taxiways. This test method does not quantitatively measure the theoretical or extended time of ice undercutting capability of ready-to-use runway deicing/anti-icing chemicals in liquid or solid form.

Ice Undercutting Test Method for Runways and Taxiways Deicing/Anti-icing Chemicals

SAE AMS-G-81827A-2012 负载量高使用温度范围广的飞机润滑脂

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 covers the requirements for one grade of grease for use as a lubricant on heavily loaded sliding steel surfaces.

Grease, Aircraft, High Load Capacity, Wide Temperature Range

SAE AIR6170-2012 跑道和滑行道除冰/防冰化学制剂的融冰试验方法

This test method provides stakeholders (runway deicing chemical manufacturers, deicing/anti-icing chemical operators and airport authorities) with relative ice melting capacity of runway deicing chemicals, by measuring the amount of ice melted as a function of time. Such runway deicing chemicals are often also used in taxiways. This test method does not quantitatively measure the theoretical or extended time ice melting capability of ready-to-use runway deicing/anti-icing chemicals in liquid or solid form.

Ice Melting Test Method for Runways and Taxiways Deicing/Anti-icing Chemicals

SAE AMS3751C-2012 空心玻璃微球形体

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 covers hollow glass microspheres. Primarily as a filler material in syntactic foam shapes or parts for dielectric applications.

Microspheres, Hollow Glass

SAE AMS3722B-2012 蜂窝状纸、125 1b(55 kg)纸

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 covers paper base honey comb material having a cell size of 0.440 in. (11.18 mm). Unless otherwise ordered, size 0.440 in. (11.18 mm) will be supplied. Primarily for use as a core in sandwich construction of light weight partitions, space fillers, and non-structural parts. This product is not intended for aircraft structural or exterior applications.

Paper Honeycomb, 125 lb (55 kg) Paper

SAE AMS4446C-2012 溶解和沉淀热处理镁合金砂型铸件8.7Al 0.70Zn 0.26Mn

This Specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for parts operating up to 300 °F (149 °C), and requiring moderate strength and excellent corrosion resistance, but usage is not limited to such applications.

Magnesium Alloy, Sand Castings 8.7Al 0.70Zn 0.26Mn Solution and Precipitation Heat Treated

BS 3L 500:2011 锻镁基合金的检验试验和验收程序

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

SAE ARP5605A-2011 实心复合层压制品无损检验的参考标准

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 of technical requirements. Newer technology may exist. This recommended practice establishes a generic composite reference standard that will accommodate nondestructive inspections (NDI) on the full array of glass fiber and carbon fiber laminates found on aircraft. The purpose of this Aerospace Recommended Practice (ARP) is to describe the design and production of solid composite laminate calibration standards to be used in ultrasonic, resonant, and tap test NDI equipment calibration for accomplishment of damage assessment and post-repair inspections. It is intended that these standards be adopted by aircraft Original Equipment Manufacturers within procedures contained on their Nondestructive Testing Manuals. Depending on the nature of the inspection, it may be necessary to compensate for variations in material properties through the use of correction factors or by adjusting for these differences on the part or structure being inspected. When using these standards consideration must be given to surface coatings such as paint or lighting protection plies. This is a reference standard construction document and not an inspection document. Inspection procedures, from OEM or users' maintenance manuals, must accompany the use of these reference standards for each unique family of composite laminate construction.

Solid Composite Laminate NDI Reference Standards

ASTM E1560-11 洁净室刮水器非挥发性残留物重量测定的标准试验方法

The NVR obtained by this test method is that amount which is available for release by wipers in normal use. Evaporation of the solvent at the stated temperature is to quantify the NVR that can be expected to exist at room temperature, since the slight difference between room temperature and test temperature has not been shown to result in significant variances. This test method may be more aggressive than necessary for the evaluation of wipers that will be restricted to dry use only. Numerous other methods are being used to determine NVR. This test method is not intended to replace test methods used for other applications.1.1 This test method covers the determination of solvent extractable nonvolatile residue (NVR) from wipers used in assembly, cleaning, or testing of spacecraft, but not from those used for analytical surface sampling of hardware. 1.2 The NVR of interest is that which can be extracted from cleanroom wipers using a specified solvent that has been selected for its extractive qualities. Alternative solvents may be selected, but since their use may result in different values being generated, they must be identified in the procedure data sheet. 1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.3.1 Exception8212;The inch-pound units are included for information only. 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.

Standard Test Method for Gravimetric Determination of Nonvolatile Residue From Cleanroom Wipers

SAE AMS3090B-2011 多硫化物密封剂兼容紧固件热凝固干膜润滑剂

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 covers a dry film lubricant in the form of lubricating solids dispersed in a resin binder and suitable solvents to produce a sprayable liquid. This product has been used typically for lubrication of fasteners in the area of aircraft fuel tanks where contact with fuel tank sealants is likely, but usage is not limited to such applications.

Lubricant, Dry Film, Heat Cured, For Fasteners Polysulfide Sealant Compatible