V16 热加工工艺 标准查询与下载

SAE AMS2431/6C-2007 玻璃珠冲压设备

This specification, in conjunction with the general requirements covered in SAE AMS 2431 establishes the requirements for glass shot to be used for peening of metal parts.

Peening Media Glass Shot

SAE AMS2400W-2007 镀镉

This specification covers the requirements for electrodeposited cadmium on metal parts. This process has been used typically to provide corrosion resistance to metal parts, but usage is not limited to such applications.

Plating, Cadmium

SAE AMS2427D-2007 离子蒸镀铝涂层

This specification covers the engineering requirements for ion vapor deposition (IVD) of aluminum on steel, titanium, and aluminum alloys and the properties of the deposit. This process has been used typically to provide a corrosion-resistant coating to parts operating at service temperatures up to 925 °F (496 °C) and requiring freedom from hydrogen embrittlement and solid metal embrittlement, but usage is not limited to such applications.

Aluminum Coating Ion Vapor Deposition

SAE AMS2451/11A-2007 钴镀涂

This specification covers the requirements for brush plating of cobalt by electrodeposition. This process has been used typically to improve corrosion and wear resistance of steel parts and to repair damaged, worn, or mismachined parts, but usage is not limited to such applications. This process is particularly useful for plating localized areas on-site, especially on large parts or assemblies, and for minimizing masking.

Plating, Brush, Cobalt

SAE AMS2772D-2007 铝合金原料的热处理

This specification covers requirements and recommendations for the heat treatment of wrought aluminum alloy raw materials by producers. It supersedes AMS-H-6088 and replaces MIL-H-6088. Aluminum alloy tempers are described in SAE AS1990 and ANSI H35.1 This specification may be used for alloys other than those specified herein providing temperatures, times, and quenchant are specified.

Heat Treatment of Aluminum Alloy Raw Materials

SAE AMS2411F-2007 高温设备用银的电镀

This specification covers the engineering requirements for silver deposited on metal parts with a nickel strike between the basis metal and the silver deposit. This process has been used typically to prevent galling or seizing of surfaces of parts, such as fasteners, made of low-alloy steel, corrosion and heat resistant steel, and nickel alloys for use up to 1400 °F (760 °C).

Plating, Silver for High Temperature Applications

NF L06-387:2007 航空航天结构用焊接和铜焊的组装件.用电子束焊接金属材料接缝.焊接的组装件质量

Welded and brazed assemblies for aerospace constructions - Joints of metallic materials by electron beam welding - Quality of welded assemblies.

GJB 2502.2-2006 航天器热控涂层试验方法 第2部分:太阳吸收比测试

本部分规定了航天器热控涂层太阳吸收比测试的目的、范围和精度、原理、设备及要求、条件、试样、程序、数据处理及报告等要求。 本部分适用于航天器热控涂层太阳吸收比的测试。

Test method for thermal control coatings of spacecraft Part 2: Measurement of solar absorptance

GJB 2502.9-2006 航天器热控涂层试验方法 第9部分:原子氧试验

本部分规定了航天器热控涂层原子氧试验的目的、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层的原子氧冲蚀试验。

Test method for thermal control coatings of spacecraft Part 9: Atomic oxygen test

GJB 2502.1-2006 航天器热控涂层试验方法 第1部分:总则

本部分规定了航天器热控涂层的术语、一般要求和试验方法一览表。 本部分适用于航天器热控涂层的试验。

Test method for thermal control coatings of spacecraft Part 1: General

GJB 2502.4-2006 航天器热控涂层试验方法 第4部分：气动环境试验

本部分规定了航天器外部热控涂层气动冲刷和气动加热环境试验的目的、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层的气动环境试验。

Test method for thermal control coatings of spacecraft Part 4: Aerodynamical environment test

GJB 2502.5-2006 航天器热控涂层试验方法 第5部分:真空-紫外辐照试验

本部分规定了航天器热控涂层真空-紫外辐照环境试验的目的、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层的真空-紫外辐照试验。

Test method for thermal control coatings of spacecraft Part 5: Ultraviolet irradiation test in vacuum

GJB 2502.6-2006 航天器热控涂层试验方法 第6部分:真空-质子辐照试验

本部分规定了航天器热控涂层真空-质子辐照环境试验的目的、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层的真空-质子辐照试验。

Test method for thermal control coatings of spacecraft Part 6: Proton irradiation test in vacuum

GJB 2502.7-2006 航天器热控涂层试验方法 第7部分:真空-电子辐照试验

本部分规定了航天器热控涂层对空间真空-电子辐照环境试验的目的、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层的真空-电子辐照试验。

Test method for thermal control coatings of spacecraft Part 7: Electron irradiation test in vacuum

GJB 2502.3-2006 航天器热控涂层试验方法 第3部分:发射率测试

本部分规定了航天器热控涂层半球发射率和法向发射率测试的目的、范围和精度、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层发射率的测试。

Test method for thermal control coatings of spacecraft Part 3: Measurement of emissivity

GJB 2502.10-2006 航天器热控涂层试验方法 第10部分:综合辐照试验

本标准规定了航天器热控涂层综合辐照环境试验的目的、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层的综合辐照试验。

Test method for thermal control coatings of spacecraft Part 10: Combined irradiation test

GJB 2502.8-2006 航天器热控涂层试验方法 第8部分:热循环试验

本部分规定了航天器热控涂层热循环试验的目的、原理、设备及要求、条件、试样、程序、数据处理和报告等要求。 本部分适用于航天器热控涂层的热循环试验。

Test method for thermal control coatings of spacecraft Part 8: Thermal cycle test

GJB 2704A-2006 航天器热控涂层通用规范

本规范规定了航天器热控涂层（以下简称热控涂层）的通用要求。 本规范适用于卫星、飞船、空间站、深空探测器等航天器的热控涂层。

General specification for thermal control coatings of spacecraft

SAE AMS2447C-2006 热喷雾高速氧化/燃烧过程镀涂

This specification covers the requirements for applying thermal spray coatings applied using the high velocity oxygen fuel (HVOF) combustion process. This specification is not intended to be used for duples coatings, i.e., the application of the coating over a previously applied coating. This process has been used typically to provide coatings of lower porosity and higher adhesive, and/or cohesive, strength than generally attainable with typical plasma spray processes for applications requiring wear, heat, and corrosion resistance and for dimensional restoration, but usage is not limited to such applications.

Coating, Thermal Spray High Velocity Oxygen/Fuel Process

SAE AMS2678-2006 真空下炉内部分钎焊

This specification covers the requirements and procedures for the brazing of parts in a very low pressure gas which referred to as "vacuum" herein.

Furnace Brazing of Parts in a Vacuum Atmosphere