49.040 有关航空航天制造用镀涂和有关工艺 标准查询与下载

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)

SAE AMS3120H-2012 黑底甘油酞酸酯瓷漆

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 specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED". This specification covers a gloss, black baking enamel based on a glyceryl phthalate resin. Primarily a an exterior protective coating for metal surfaces.

Enamel, Glyceryl Phthalate, Black Baking

SAE AMS3125H-2012 发动机灰底甘油酞酸酯瓷漆

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 has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED". This specification covers a gloss, engine-gray baking enamel based on a glyceryl phthalate resin. Primarily as an exterior protective coating for metal surfaces.

Enamel, Glyceryl Phthalate, Engine Gray Baking

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 ARP4992B-2012 加工溶液的周期性试验规划

This SAE Aerospace Recommended Practice (ARP) describes a method for classifying the frequencies of analysis of solutions used in the processing of metals, such as electroplating, anodizing, and conversion coating and associated processes but usage is not limited to such applications. This document is intended to establish a periodic test plan that may be used by processors to satisfy the requirement of an Aerospace Material Specification (AMS) for a chemical processing solution periodic test plan as a control factor. This document does not fulfill the criteria for a formal statistical process control program.

Periodic Test Plan for Processing Solutions

SAE AMS2447D-2012 热喷雾高速氧化/燃烧过程镀涂

This specification covers the requirements for 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 AMS2431/5B-2011 表面硬化钢喷丸的介质

The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification AMS 2431.

Peening Media, Case Hardened Steel Peening Balls

LST EN 2491-2011 航空航天系列 二硫化钼干式润滑剂 涂层方法

Aerospace series - Molybdenum disulphide dry lubricants - Coating methods

LST EN 4593-2011 航空航天系列色漆和清漆太阳吸收率的测定

Aerospace series - Paints and varnishes - Determination of solar absorptance

LST EN 2535-2011 航天系列-镉的真空沉积

Aerospace series - Vacuum deposition of cadmium

SAE AMS2429D-2011 电镀,青铜氮化电镀法90Cu 10Sn

This specification covers the requirements for electrodeposited bronze plate and subsequent removal. This process has been used typically as a maskant to prevent nitriding of surfaces on which nitriding is neither required nor permitted, but usage is not limited to such applications.

Plating, Bronze Nitriding Stop-off 90Cu 10Sn

SAE AMS3108G-2011 底漆,赭色,酚醛

This document has been declared "Stabilized" and will no longer be subjected toperiodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED".

Primer, Ocher, Phenolic

SAE AMS2434D-2011 锡锌合金电镀

This specification covers the requirements for the electrodeposition of tin-zinc plating on metal parts and the properties of the deposit. This plating has been used typically as a corrosion resistant plating where cadmium cannot be used, as a replacement for tin plating where tin whisker growth is a concern, a coating for fasteners where thread lubricity is desirable, and for parts which are to be joined using tin-lead solders, but usage is not limited to such applications.

Plating, Tin-Zinc Alloy

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

DIN EN 4593:2011 航空航天系列.色漆和清漆.太阳能吸收率的测定;德文版本和英文版本EN 4593-2011

This European standard specifies the method of test for determining the solar absorptance of paints and varnishes.

Aerospace series - Paints and varnishes - Determination of solar absorptance; German and English version EN 4593:2011

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

BS EN 4593:2011 航空航天系列.色漆和清漆 太阳能吸收率的测定

This European Standard specifies the method of test for determining the solar absorptance of paints and varnishes. The test procedure determines the amount of energy reflected by the material in the range of wavelengths at which there is energy from the sun hitting the Earth’s surface, and with the aid of a standard solar spectrum it allows a calculation to determine the solar absorptance which can then be used to determine the efficiency of solar heat reflecting paints. The procedure is applicable to products intended for use in aerospace applications.

Aerospace series. Paints and varnishes. Determination of solar absorptance

BS EN 2491:2011 航空航天系列.二硫化钼干膜润滑油.涂覆法

This European Standard defines the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion resistant steel and nickel based alloys.

Aerospace series. Molybdenum disulphide dry lubricants. Coating methods