V10 航空、航天材料基础标准 标准查询与下载

SAE ARP6012A-2014 JAUS 合规性和互操作性政策

This document, the JAUS Compliance and Interoperability Policy (ARP6012), recommends an approach to documenting the complete interface of an unmanned system or component in regard to the application of the standard set. While non-SAE AS-4 JAUS documents are referenced in this ARP they are not within the scope of this document and should be viewed as examples only.

JAUS Compliance and Interoperability Policy

SAE AS6174A-2014 伪劣材料.正品合格材料的确保收购

This SAE Standard standardizes practices to: a. maximize availability of authentic materiel, b. procure materiel from reliable sources, c. assure authenticity and conformance of procured materiel, including methods such as certification, traceability, testing and inspection appropriate to the commodity/item in question, d. control materiel identified as fraudulent/counterfeit, e. and report suspect or confirmed fraudulent/counterfeit materiel to other potential users and Authority Having Jurisdiction.

Counterfeit Materiel; Assuring Acquisition of Authentic and Conforming Materiel

SAE AMS2471H-2014 铝合金的阳极化处理.未染色镀层的硫酸处理

This specification establishes the requirements for undyed anodic coatings on aluminum alloys. This process has been used typically to increase corrosion resistance and to provide surfaces that will promote adherence of paint and other organic finishes, but usage is not limited to such applications. AMS2472 should be specified for coatings colored by dyeing. This process is not suitable for parts that contain joints or recesses in which the anodizing solution may be retained.

Anodic Treatment of Aluminum Alloys Sulfuric Acid Process, Undyed Coating

BS ISO 16378:2013 空间系统.热控制材料热性能测量

Space systems. Measurements of thermooptical properties of thermal control materials

HB 8409-2013 复合材料制件工装设计要求

本标准规定了复合材料制件成型工装(简称模具)的分类、 设计依据、 设计原则、 设计流程以及设计 要求等。 本标准适用于树脂基复合材料制件模压成形、 热压罐成形、 RTM成形工装的设计y 缠绕成型、 RFI 成形、 VAR] 成型工装可参照使用。

Tooling Design Requirements for Composite Parts

SAE AS4792A-2013 含水磁粉检验用水质稳定剂

This SAE Aerospace Standard (AS) covers water conditioning agents used to facilitate aqueous wet-method magnetic particle inspection. Such conditioning agents, in powder or liquid form, provide suitable corrosion protection, wetting, and particle dispensability properties when mixed in water for application of magnetic particles on the surface of an object for magnetic particle inspection as described in AMS 3042, AMS 3044, ASTM E1444, and others. Water conditioning agents can consist of varying combinations of such components as dispersants, surfactants, corrosion inhibitors, and anti-foaming agents. Individual components may be added to the bath of a syst

Water Conditioning Agents for Aqueous Magnetic Particle Inspection

EN 4632-006:2013 航空航天系列.航空航天结构用材料的可焊接性和可钎焊性.第六部分:钛合金的均质装配件

This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace applications. It comprises a series of sheets, by materials or by material family, which: indicate the main titles, the typical chemical composition and the main characteristics, contain recommendations for welding and brazing, indicate a degree of weldability or brazeability for a given process under defined conditions. It is applicable without restriction for the manufacturing of new parts or for repair.

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys

SAE AS6462-2012 AS5553,伪造电子零件.废止,检测,减损和处置查证准则

AS5553, Counterfeit Electronic Parts; Avoidance, Detection, Mitigation, and Disposition Verification Criteria

SAE AMS2641B-2012 石油基,车辆磁粉探伤

This specification covers two types of refined hydrocarbon compounds in the form of liquids. This product has been used typically as a vehicle for the suspension of magnetic particles used in magnetic particle inspection procedures, but usage is not limited to such applications.

Vehicle, Magnetic Particle Inspection, Petroleum Base

SAE AMS2750E-2012 高温测定法

This specification covers pyrometric requirements for thermal processing equipment used for heat treatment. It covers temperature sensors, instrumentation, thermal processing equipment, system accuracy tests, and temperature uniformity surveys. These are necessary to ensure that parts or raw materials are heat treated in accordance with the applicable specification(s). This specification is not applicable to heating, or to intermediate thermal processing unless specifically referenced by a material or process specification.

Pyrometry

SAE AMS1538B-2012 镁合金用酸性脱氧剂

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 an acidic deoxidizer in the form of a liquid. This product has been used typically for removing oxides and corrosion from magnesium alloys.

Deoxidizer, Acidic, for Magnesium Alloys

SAE AMS1431D-2012 固体逃逸和滑行道除冰/防冻化合物

This specification covers a deicing and anti-icing compound in the form of a solid. Unless otherwise started, all specifications referenced herein are latest (current) revision. These compounds have been used typically at airports on aircraft maneuvering areas, such as aprons, runways, and taxiways, for the prevention and removal of frozen deposits of snow, frost, and ice, but usage is not limited to such applications.

Compound, Solid Runaway and Taxiway Deicing/Anti-Icing

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 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

BS EN 4704:2012 航空航天系列.用于防腐和涂料预处理方面的铝及变形铝合金的酒石硫磺酸阳极处理(TSA)

Aerospace series. Tartaric-Sulphuric-Acid anodizing of aluminium and aluminium wrought alloys for corrosion protection and paint pre-treatment (TSA)

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 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 AMS3697C-2012 -55至+150℃(-65至+300°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 +150 degrees C (-65 to +300 degrees F).

Aerodynamic Fairing Compound, -55 to +150°C (-65 to +300°F)

SAE AMS3694B-2012 -55至+130℃(-65至+270°F)柔性的空气动力校平复合物

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 resin-base material in the form of a paste or putty, suitable for application by spatula or putty knife. Primarily to fill aircraft skin depressions to a maximum depth of 0.250 in. (6.25 mm) and be capable of being painted with subsequent specified coatings. These materials are meant for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of flexible material to produce the required smoothness on aerodynamic surfaces. Suitable for maintaining adhesion to surfaces subject to service temperatures from -55 degrees to +130 degrees C (-65 degrees to +270 degrees F).

Aerodynamic Smoothing Compound, Flexible, -55 to +130°C (-65 to +270°F)