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

EN 4474:2016 航空航天系列-热镀铝涂层-涂覆方法

This European 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.

Aerospace series - Aluminium pigmented coatings - Coating methods

ASTM F1864-16 光学和红外透明材料和涂料的防尘蚀性的标准测试方法

5.1 All materials on exterior aircraft surfaces are subject to abrasion from airborne particles of various sizes and shapes. Transparent materials are particularly vulnerable to abrasion, since their performance is based on their ability to transmit light with a minimal amount of scatter. Scratches, pitting, and coating removal and delamination as a result of abrasion may increase scatter, reduce transmission, and degrade the performance of transparent materials. Visually transparent materials are required for pilot and air crew enclosures, such as canopies, windshields, and viewpoints. Materials transparent in the IR region (8 to 12 μm) are required for tracking, targeting, and navigational instrumentation. 5.2 This test method is intended to provide a calibrated and repeatable means of determining the relative abrasion resistance of materials and coatings for optical and IR transparent materials and coatings. The test parameters for this test method can be directly related to dust cloud densities and velocities to which transparent materials are exposed in the field. 1.1 This test method covers the resistance of transparent plastics and coatings used in aerospace windscreens, canopies, and viewports to surface erosion as a result of dust impingement. This test method simulates flight through a defined particle cloud environment by means of independent control of particle size, velocity, impact angle, mass loading, and test duration. 1.2 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.

Standard Test Method for Dust Erosion Resistance of Optical and Infrared Transparent Materials and Coatings

GSO ISO 8081:2015 航空航天工艺铝合金化学转化膜通用

  Scope is not provided for this standard

Aerospace process -- Chemical conversion coating for aluminium alloys -- General purpose

GSO ISO 8080:2015 航空航天 钛及钛合金阳极处理 硫酸工艺

  Scope is not provided for this standard

Aerospace -- Anodic treatment of titanium and titanium alloys -- Sulfuric acid process

SAE AMS2535B-2015 用于微电路的涂层、气相沉积聚单氯对二甲苯

This specification covers requirements for poly-monochloro-para-xylylene coatings. Primarily for use as a secondary moisture barrier coating on hybrid microcircuit substrates and on active monolithic devices. Additionally, the coating immobilizes undesirable particles remaining in sealed microcircuits and enhances to some degree the strength of fine wire interconnections.

Coating, Vapor Deposited Poly-Monochloro-Para-Xylylene for Microcircuits

SAE AMS3180G-2015 工业级甲苯

This specification covers, industrial-grade toluene in the form of a liquid.

Toluene, Industrial Grade

DIN EN 4826:2015 航空航天系列-规定抗拉强度<=1450MPa的钢材、铜合金、镍合金和铝合金零件和紧固件的锌镍（12%至16%Ni）镀层

Aerospace series - Zinc-Nickel (12 % to 16 % Ni) plating of steels with specified tensile strength <= 1 450 MPa, copper alloys, nickel alloys and aluminium alloys for parts and fasteners; German and English version EN 4826:2014

SAE AMS2430T-2015 喷丸 自动

This specification covers the requirements for automatic shot peening of surfaces of parts by impingement of media, including metallic, glass, or ceramic shot.

Shot Peening@ Automatic

BS EN 4826:2014 航空航天系列. 零件和紧固件用抗拉强度小于或者等于1450 MPa的镀锌镍 (12 %-16 % 镍) 钢, 铜合金, 镍合金以及铝合金

Aerospace series. Zinc-Nickel (12 %-16 % Ni) plating of steels with specified tensile strength 1 450 MPa, copper alloys, nickel alloys and aluminium alloys for parts and fasteners

EN 4826:2014 航空航天系列 规定抗拉强度<= 1450 MPa 的钢、铜合金、镍合金和铝合金的零件和紧固件的锌镍（12% 16% Ni）电镀

This European Standard specifies the plating of a Zinc-Nickel (12 % to 16 %) alloy on mechanical parts and fasteners in steels (Rm

Aerospace series - Zinc-Nickel (12 % - 16 % Ni) plating of steels with specified tensile strength <= 1450 MPa, copper alloys, nickel alloys and aluminium alloys for parts and fasteners

SAE AMS2472G-2014 铝合金硫酸工艺阳极处理 染色涂层

This specification establishes the requirements for dyed anodic coatings on aluminum alloys.

Anodic Treatment of Aluminum Alloys Sulfuric Acid Process@ Dyed Coatings

KS W 4041-2014 航天用磁性材料的检验流程

Inspection Process of Magnetic for Aerospace Use

HB/Z 416-2014 航空铝合金构件搅拌摩擦焊工艺

本指导性技术文件规定了航空铝合金结构件搅拌摩擦焊的人员、环境、材料、焊件接头、设备与工装、工艺性鉴定、工艺参数的选择与确定、接头等级、文件管理、工艺控制、质量控制以及安全要求等。 本指导性技术文件适用于厚度不大于12mm且为常用铝合金牌号和状态的航空铝合金结构件对接、搭接接头搅拌摩擦焊。其他系列铝合金的结构件对接、搭接接头搅拌摩擦焊也可参照本指导性技术文件。

Process of friction stir welding for aluminum alloy aero-structural components

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

SAE AMS2469J-2014 铝和铝合金的硬质阳极涂覆

This specification establishes the requirements for a hard anodic coating on aluminum and aluminum alloys.

Hard Anodic Coating on Aluminum and Aluminum Alloys

SAE AMS2422F-2014 镀金

This specification covers the engineering requirements for electrodeposition of gold and the properties of the deposit.

Plating, Gold

NF L16-021*NF EN 4594:2014 航空航天系列. 涂料和清漆. 双组分冷固化聚氨酯罩面漆. 超音速耐腐蚀性

La présente Norme européenne spécifie les exigences d'une couche de finition polyuréthane, à deux composants, degré moyen de résistance à l'érosion due aux effets de la pluie, disponible dans une gamme de couleurs et de niveaux de brillance, applicable sur une peinture primaire pour applications aérospatiales sur des zones où l'érosion par la pluie à des vitesses supersoniques peut constituer un problème par ex. bord d'attaque et entrées d'air.Les propriétés spécifiées dans la présente norme sont obtenues sur des éprouvettes en alliage d'aluminium définies conformément à l'EN 3837 Procédure A et l'EN 23270 et peintes avec un primaire selon l'EN 2435.L'aptit

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Supersonic erosion resistance

NF L16-022*NF EN 4595:2014 航空航天系列. 涂料和清漆. 双组分冷固化聚氨酯罩面漆. 亚音速耐腐蚀性

La présente Norme européenne spécifie les exigences d'une couche de finition polyuréthane, à deux composants, degré moyen de résistance à l'érosion liée aux effets de la pluie, disponible dans une gamme de couleurs et de niveaux de brillance, applicable sur une peinture primaire pour applications aérospatiales sur des zones où l'érosion par la pluie à des vitesses subsoniques peut constituer un problème par ex. bord d'attaque et entrées d'air.Les propriétés spécifiées dans la présente norme sont obtenues sur des éprouvettes en alliage d'aluminium définies conformément à l'EN 3837 Procédure A et l'EN 23270 et peintes avec un primaire selon l'EN 2435.L'aptitu

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Subsonic erosion resistance

SAE AMS1527D-2014 压力喷洒式泡沫乳状水混溶的飞机外表面用清洁剂

This specification covers a water-miscible, foam-on, pressure spraying cleaner in the form of a liquid.

Cleaner for Aircraft Exterior Surfaces, Water-Miscible, Foam-On, Pressure-Spraying

SAE AMS2411H-2013 高温设施用镀银工艺

This specification covers the requirements for silver deposited on metal parts with a nickel strike between the basis metal and the silver deposit.

Plating, Silver, for High Temperature Applications