V10 航空、航天材料基础标准 标准查询与下载

SAE AMS3696C-2012 -55至+85℃(-65至+185°F)空气动力整流罩复合物

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 two-component air-curing, aluminum-powder -filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife. Primarily for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of material to produce the required smoothness on aerodynamic surfaces subject to service temperatures from -55 to +85 degrees C (-65 to +185 degrees F).

Aerodynamic Fairing Compound, -55 to +85°C (-65 to +185°F)

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

KS W 5000-2011 航空照明设施图形符号

이 표준은 공항 항공등화시설의 종류를 나타내는 도면에 사용하는 그림 기호(이하 심벌이라 한

Graphical symbols for aeronautical lighting systems

NF L10-215*NF EN 2491:2011 航天系列.二硫化钼干膜润滑剂.涂敷法.

Aerospace series - Molybdenum disulphide dry lubricants - Coating methods.

DIN EN 2535:2011 航空航天系列.镉的真空沉积;德文和英文版本EN 2535-2011

The European Standard defines the deposit method for cadmium layers according to the vacuum deposition process, for use in aerospace construction.

Aerospace series - Vacuum deposition of cadmium; German and English version EN 2535:2011

BS EN 2535:2011 航空航天系列.镉的真空淀积

This European Standard defines the method for depositing cadmium layers according to the vacuum deposition process, for use in aerospace construction. According to this process, cadmium metal is vaporised under vacuum and deposited directly on the base material with an interlayer. The coating produced in this way is ductile and electrically conductive. This standard should be applicable whenever referenced.

Aerospace series. Vacuum deposition of cadmium

SAE AIR1168/9A-2011 自然环境,气体,液体和固体的热物理性质

This AIR is arranged in the following four sections: 2A - properties of the natural environment; 2B - properties of gases; 2C - properties of liquids; and 2D - properties of solids.

Thermophysical Properties of the Natural Environment, Gases, Liquids, and Solids

QJ 10014.5-2011 空间材料安全性与相容性 第5部分：系统/部件材料与推进剂反应性测定方法

本部分规定了测定材料与航天液体推进剂相互作用的试验设备和方法。 本部分适用于测定系统/部件材料与推进剂的反应性。本部分适于测定材料和推进剂间的反应。这些材料在推进剂贮存、转注和飞行系统的设计、建造和运行中使用。本方法是长期推进剂相容性半定性的快速筛选测试。如果材料和推进剂接触超过12个月，则应在使用条件下进行长期测试以定量分析材料随时间的退化。

Space systems.Safety and compatibility of materials.Part 5:Determination of reactivity of system/component materials with aerospace propellants

QJ 20013-2011 空间材料出气特性测试方法

本标准规定了非金属材料出气特性原位测试方法，包括测试原理、测试装置、样品、测试准备、测试程序和数据处理等。 本标准适用于航天器使用的可能会对航天器造成污染的非金属材料出气特性的测试。其他材料（包括复合材料）出气特性测试可参照执行。

Test method for outgassing characteristics of spacecraft materials

HB/Z 5069-2011 电镀铜工艺及质量检验

本指导性技术文件规定了电镀铜的主要工艺材料要求、工艺程序、主要工序说明、电镀铜溶液的配制、质量检验、不合格镀层的退除与返修等内容。本指导性技术文件适用于结构钢、不锈钢、耐热钢、高温合金及TC1、TC2、TC6和TC11钛合金零(组)件电镀铜及铜镀层的质量验收。其他钛合金零件电镀铜可以参照使用。

Process and quality inspection for electroplated copper coatings

QJ 10014.4-2011 空间材料安全性与相容性.第4部分:材料在加压气氧或富氧环境中向上燃烧性能测定方法

本部分规定了常温下宇航材料在加压气氧（GOX)或富氧环境中燃烧性能的测定方法。本方法也可通过在超出使用压力的压力下测试（见第4章），提供材料的补充信息。本方法的标准压力范围为常压至69MPa。

Space systems.Safety and compatibility of materials.Part 4:Determination of upward flammability of materials in pressurized gaseous oxygen or oxygen-enriched environment

HB/Z 120-2011 钛合金钨极氩弧焊工艺及质量检验

本指导性技术文件规定了TA1、TA2、TA3、TA6、TA7、TA15、TA16、TA21、TC1、TC2、TC3、TC4等钛合金材料的自动、手工钨极氩弧焊和真空充氩钨极氩弧焊工艺及质量检验。本指导性技术文件适用于TA1、TA2、TA3、TA6、TA7、TA15、TA16、TA21、TC1、TC2、TC3、TC4等钛合金薄件材料的自动、手工钨极氩弧焊和真空充氩钨极氩弧焊。其他牌号钛合金材料的钨极氩弧焊亦可参照执行。

TIG technology and quality test of titanium alloys

QJ 10014.2-2011 空间材料安全性与相容性.第2部分:导线的绝缘材料和附件材料燃烧性能测定方法

本部分规定了测定导线的绝缘材料和附件材料分别暴露在静态环境中（方法A)和气体流通环境中(方法B)的外部点火源燃烧性能的两种测定方法。

Space systems.Safety and compatibility of materials.Part 2:Determination of flammability of electrical-wire insulation and accessory materials

QJ 10014.3-2011 空间材料安全性与相容性.第3部分:材料和装配件放气产物测定方法

本部分规定了测定载人加压航天器用材料和装配件的挥发性放气产物成分和数量的方法。本测试方法不模拟航天器舱内在轨空气环境。

Space system.Safety and Compatibility of materials.Part 3:Determination of offgassing products from materials and assembled articles

SAE AMS7908C-2011 热均衡加压的铍近终焊料预成型标准等级

This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by hot isostatic pressing (HIP). This product has been used typically for parts requiring high strength-to-weight ratio and high modulus of elasticity, but usage is not limited to such applications.

Beryllium Near-Net Preforms Standard Grade Hot Isostatic Pressed

DIN EN 4638:2011 航空航天系列.喷砂介质.不含铁的褐色刚玉;德文版本和英文版本EN 4638-2010

Aerospace series - Blast media - Brown corundum, without iron; German and English version EN 4638:2010

DIN EN 4637:2011 航空航天系列.喷砂介质.白刚玉;德文和英文版本EN 4637-2010

Aerospace series - Blast media - White corundum; German and English version EN 4637:2010

ASTM E1216-11 微粒污染物胶带提取法采样的标准操作规程

The tape lift provides a rapid and simple technique for removing particles from a surface and determining their number and size distribution. By using statistically determined sample size and locations, an estimate of the surface cleanliness level of large areas can be made. The user shall define the sampling plan. The sampling plan shall consider the importance of surface geometry and surface orientation to gas flow, gravity, obstructions, and previous history of hardware. These factors influence particle fallout and entrapment of particles on the surface. The geometry of joints, recessed areas, fasteners, and the correspondence of particle-count data to area can be maintained. The selection of tape and the verification of its effect on the cleanliness of the hardware is very important. The tape adhesive should have sufficient cohesion to avoid transfer of the adhesive to the surface under test. The impact of adhesive transfer should be evaluated by laboratory testing before using the tape on the hardware. Since potential for adhesive transfer exists, cleaning to remove any adhesive might be required. In addition, the tape should have low outgassing characteristics, and as a minimum, it should meet the requirements of less than 1.0 % total mass loss (TML) and 0.1 % collected volatile condensable materials (CVCM), as measured by Test Method E595. Care should be exercised in deciding which surfaces should be tested by this practice. The tape can remove marginally adhering paint and coatings. Optical surfaces should not be tested until verification has been made that the surface coating will not be damaged. Rough surface finishes result in low removal efficiencies. Surface finishes up to approximately 3.20 μm (125 μin.) have been tested and found to give satisfactory results. This practice has been tested only on surfaces at room temperature. Evaluation of temperature effects must be conducted prior to using the test on surfaces other than room temperature. Only personnel experienced in microscopic particle-counting techniques should be used to count and size the particles.1.1 This practice covers procedures for sampling surfaces to determine the presence of particulate contamination, 5 μm and larger. The practice consists of the application of a pressure-sensitive tape to the surface followed by the removal of particulate contamination with the removal of the tape. The tape with the adhering particles is then mounted on counting slides. Counting and measuring of particles is done by standard techniques. 1.2 This practice describes the materials and equipment required to perform sampling of surfaces for particle counting and sizing. 1.3 The criteria for acceptance or rejection of a part for conformance to surface cleanliness level requirements shall be determined by the user and are not included in this practice. 1.4 This practice is for use on surfaces that are not damaged by the application of adhesive tape. The use of this practice on any surface of any material not previously tested or for which the susceptibility to damage is unknown is not recommended. In general, metals, metal plating, and oxide coatings will not be damaged. Application to painted, vapor deposited, and optical coatings should be evaluated before implementing this test. 1.5 This practice provides three methods to evaluate tape lift tests, as follows: Sections

Standard Practice for Sampling for Particulate Contamination by Tape Lift

SAE AMS2431/2E-2010 高硬度喷丸介质(ASH)铸钢丸(55至62 HRC)

The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS 2431. Cast steel shot, high hardness, have been used typically in peening metal surfaces to impart compressive stresses to these surfaces thereby increasing resistance to fatigue and stress-corrosion cracking, but usage is not limited to such applications. Generally, high hardness cast steel shot is used on parts of hardness 50 HRC or over.

Peening Media (ASH) Cast Steel Shot, High Hardness (55 to 62 HRC)

SAE AMS2431/1E-2010 一般硬度的喷丸介质(ASR)铸钢丸(45-52 HRC)

The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS 2431. Cast steel shot, regular hardness, confirming to this specification is intended for use in peening metal surfaces to impart compressive stresses to these surfaces thereby increasing resistanct to fatigue and stress-corrosion cracking. Generally, regular hardness cast steel shot is used on parts of hardness under 50 HRC.

Peening Media (ASR) Cast Steel Shot, Regular Hardness (45 to 52 HRC)