V10 航空、航天材料基础标准 标准查询与下载

SAE AMS4191J-2009 铝合金 6.3Cu 0.3Mn 0.18Zr 0.15Ti 0.10V (2319)焊条

This specification covers an aluminum 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 aluminum alloys of similar composition where the joint is capable of being heat treated to a strength level comparable to that of the parent metal, but usage is not limited to such applications.

Aluminum Alloy, Welding Wire 6.3Cu 0.3Mn 0.18Zr 0.15Ti 0.10V (2319)

DIN EN 4474:2009 航空航天系列.铝涂层.涂层方法.德文和英文版本EN 4474-2009

This standard defines the coating methods and characteristics of aluminium pigmented coatings to EN 4473 which may be applied to fasteners in titanium, titanium alloys, heat resisting nickel base or cobalt base alloys and corrosion resisting steels excluding high strength steels above 1 550 MPa.

Aerospace series - Aluminium pigmented coatings - Coating methods; German and English version EN 4474:2009

BS EN 4632-002:2008 航空航天系列.航空航天结构用焊接及铜焊组件.材料的可焊接性和可铜焊接性.第002部分:均质铝及铝合金组件

This standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace industry. 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.  indicate a value of the mechanical strength coefficient of the welded joint for each welding process, when it could be extracted from bibliographic references referring to it. The joint coefficient is expressed as a ratio of the tensile strength of the welded joint to the tensile strength of the base alloy. It is applicable without restriction for the manufacturing of new parts or for repair.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002: Homogeneous assemblies aluminium and aluminium alloys

BS EN 4632-001:2008 航空航天系列.航空航天结构用焊接及铜焊组件.材料的可焊接性和可铜焊接性.一般要求

This standard defines weldability and brazeability degrees for metallic materials used in aerospace construction, for processes and techniques involving welding and brazing but excluding soldering. It also defines rules to be observed to determine the degree of weldability and brazeability. It is applicable without any restriction for the manufacturing of new parts and repair parts.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - General requirements

BS EN 2950:2008 航空航天系列.试验方法.可锻耐热合金半成品和零件.结构和故障图,宏观和显微检查用条件.结构和不合格品图集

The present document defines the conditions for the macrographic and micrographic examination of heat resisting alloy semi-finished and parts. It includes an atlas of commonly encountered and structural defects. The present document shall be applied in conjunction with the material standards specifying the criteria of acceptance. The present document is not intended to apply to cast or powder metallurgy products.

Aerospace series - Test method - Wrought heat resisting alloys Semifinished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects

SAE AMS2480H-2009 磷化处理底漆

This specification covers the engineering requirements for producing a zinc phosphate coating on ferrous alloys and the properties of the coating. This process has been used typically to produce a coating which will ensure satisfactory paint adherence, but usage is not limited to such applications.

Phosphate Treatment Paint Base

SAE AMS3753B-2009 空心碳微球体

This specification covers carbon in the form of hollow microspheres. This product has been used typically as a filler material in syntactic foam shapes, but usage is not limited to such applications.

Microspheres, Carbon, Hollow

SAE AMS3158C-2009 LOX相容性水基荧光渗透剂溶液

This specification covers a stable, noncorrosive, water-soluble, highly-penetrating, fluorescent solution which may, but need not, be diluted with an appropriate amount of water for use. This product has been used typically for use in fluorescent penetrant inspection of parts and assemblies for detection of surface discontinuities and imperfections, particularly on parts, such as those in oxygen systems, which must not be exposed to oils, but usage is not limited to such applications.

Solution, Fluorescent Penetrant, Water Base for LOX Compatibility

DIN EN 4632-001:2009 航空航天系列.航空航天结构用焊接及铜焊组件.材料的可焊接性和可铜焊接性.第001部分:一般要求.德文版本和英文版本EN 4632-001-2008

This standard defines weldability and brazeability degrees for metallic materials used in aerospace construction, for processes and techniques involving welding and brazing but excluding soldering. It also defines rules to be observed to determine the degree of weldability and brazeability. It is applicable without any restriction for the manufacturing of new parts and repair parts.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 001: General requirements; German and English version EN 4632-001:2008

GJB 6762-2009 航天发射场低温推进剂泄回准则

本标准规定了航天发射场低温推进剂泄回的流程、状态准备、泄回、泄回后的处置工作准则、注意事项和要求。 本标准适用于航天发射场组织实施低温推进剂泄回。

Bleed-off criterion for cryogenic propellants in spacecraft launching complex

SAE ARP6012-2009 JAUS 合规性和互操作性政策

The SAE Joint Architecture for Unmanned Systems (JAUS) is a technology enabler for air, ground, water surface, and underwater unmanned systems. SAE JAUS is platform independent and thus provides a standard for interfacing with different types of vehicles, sensors, operator control stations, and payloads. The SAE AS-4 Unmanned Systems Technical Committee defines a set of standards for use in unmanned systems. While each standard can be used individually, specific guidance is required for combining them. This recommendation provides this guidance and defines the concept of "interoperability profiles" (Section 5). An Interoperability Profile is the result of a strategic application of standards in a layered approach. The desired result is for any two systems that implement the same Interoperability Profile to interoperate in a useful way. 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 AMS2466B-2009 高压镁合金碱性硬质阳极涂层

This specification covers the requirements for a hard anodic coating on magnesium alloys. This coating has been used typically to provide corrosion resistance and abrasion resistance to cast magnesium alloys, but usage is not limited to such applications.

Hard Anodic Coating of Magnesium Alloys Alkaline Type, High Voltage

SAE AMS2759/1E-2009 最小弹性强度低于220 ksi(1517 MPa)的碳和低合金钢零件的热处理

This specification, in conjunction with the general requirements for steel heat treatment covered in AMS 2759, establishes the requirements for heat treatment of carbon and low-alloy steel parts to minimum ultimate tensile strengths below 220 ksi (1517 MPa). Parts are defined in AMS 2759.

Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa)

ASTM F1110-09 夹层腐蚀的标准试验方法

The data generated by this test method shall be used to determine whether aircraft structural aluminum alloys are liable to be corroded or damaged by application of the test material during routine maintenance operations. Interpretation of the sandwich corrosion test results is based on a comparison of the appearance of faying surfaces of three sets of coupons. One set of test coupons is exposed with reagent water only in the faying surfaces, to establish the baseline (controls) against which the panels exposed to the test material are compared. Disregard corrosion at cut edges of the test coupons. The relative corrosion severity rating system is provided in order to allow a numerical classification of the test results and to eliminate the necessity for elaborate weight loss measurements. Pitting corrosion, which is rated 4—extensive (severe) corrosion, may involve only a negligible weight loss. Relative corrosion severity rating system: Appearance/Corrosion: 0—No visible corrosion and no discoloration present 1—Very slight corrosion or very slight discoloration, and/or up to 5 % of areaA corroded 2—Discoloration and/or up to 10 % of areaA corroded 3—Discoloration and/or up to 25 % of areaA corroded 4—Discoloration and/or more than 25 % of areaA corroded, and/or pitting present A ”Area” refers to area under the filter paper, or if no filter paper is used, the area where the test material was applied. 1.1 This test method defines the procedure for evaluating the corrosivity of aircraft maintenance chemicals, when present between faying surfaces (sandwich) of aluminum alloys commonly used for aircraft structures. This test method is intended to be used in the qualification and approval of compounds employed in aircraft maintenance operations. 1.2 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information. 1.3 This standard may involve hazardous materials, operations, and equipment. 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. Specific hazard statements appear in Section 9.

Standard Test Method for Sandwich Corrosion Test

ANSI/ASTM D2624:2009 航空和馏分燃料电导率试验方法

Test Methods for Electrical Conductivity of Aviation and Distillate Fuels

SAE AMS2471G-2008 铝合金的阳极化处理.未染色镀层的硫酸处理

This specification establishes the engineering requirements for undyed anodic coatings on aluminum alloys. This process has been used typically to increase corrosion resistance and to provide surfaces which will promote adherence of paint and other organic finishes, but usage is not limited to such applications. AMS 2472 should be specified for coatings colored by dyeing. This process is not suitable for parts which contain joints or recesses in which the anodizing solution may be retained.

Anodic Treatment of Aluminum Alloys Sulfuric Acid Process, Undyed Coating

SAE AMS3042E-2008 干燥粉末使用湿方法的非荧光磁性粒子

This specification covers nonfluorescent magnetic particles in the form of dry powder intended to be suspended in oil or conditioned water vehicle for use in the wet method, magnetic particle inspection. These particles have been used typically as the inspection medium in a wet magnetic particle inspection system in accordance with ASTM E 1444, using either an oil or a conditioned water vehicle, but usage is not limited to such application.

Magnetic Particles, Nonfluorescent, Wet Method, Dry Powder

SAE AMS3044F-2008 干燥粉末使用湿方法的荧光磁性粒子

This specification covers fluorescent magnetic particles in the form of dry powder. These particles have been used typically as the inspection medium in wet, fluorescent magnetic particle inspection system as defined in ASTM E 1444 using either an oil or conditioned-water vehicle, but usage is not limited to such application.

Magnetic Particles, Fluorescent, Wet Method, Dry Powder

SAE AS5502B-2008 航空航天密封剂用标准要求

This document establishes standard requirements for aerospace sealants, which may be incorporated as part of Aerospace Material Specifications (AMS) for such products. This document provides for commonality of methods and procedures for responsibility for inspection, source inspection, classification of tests, establishment of/and qualification to qualified products lists, approval, reports, resampling and retesting, packaging, and marking.

Standard Requirements for Aerospace Sealants

SAE AMS2753C-2008 液体盐浴铁素体硝基渗碳无氰化物浴

This specification covers the requirements for an epsilon-iron nitride case on ferrous parts produced by immersion in a low-temperature, agitated, fused salt bath.1.2 ApplicationNitrocarburized surfaces have been used typically for increasing the resistance to wear and fatigue on ferrous alloys including carbon steels, low-alloy steels, tool steels, and corrosion-resistant steels, cast irons, and ferrous powder metalproducts, but usage is not limited to such applications.1.2.1 This process is not recommended for use on parts that have been plated with silver, copper, zinc, or cadmium or on parts having copper alloy inserts.1.3 Safety - Hazardous MaterialsWhile the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is thesole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.

Liquid Salt Bath Ferritic Nitrocarburizing Non-Cyanide Bath