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 AMS2417H-2010 电镀锌镍合金

This specification covers the requirements for electrodeposition of a zinc-nickel alloy and the properties of the deposit. Zinc-nickel plating has been used typically to provide corrosion resistant to steel parts which may operate at elevated temperatures shown 1.3, but usage is not limited to such applications. See 8.9 and 8.10

Plating, Zinc-Nickel Alloy

DS/EN 2434-002:2010 航空航天系列色漆和清漆双组分冷固化聚氨酯面漆第002部分：高耐化学性

This European Standard specifies the requirements for a two component polyurethane finish to be applied over a primer for interior and exterior aerospace applications, where maximum resistance to normal operational fluids is required.The properties specified in this European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to EN 2435-002. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 002: High chemical resistance

DS/EN 2434-004:2010 航空航天系列色漆和清漆双组分冷固化聚氨酯面漆第004部分：高柔韧性

This European Standard specifies the requirements for a two component polyurethane finish to be applied over a primer mainly for exterior aerospace applications, offering high flexibilityThe properties specified in this European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN 23270 and painted with primer to prEN 2435-002. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 004: High flexibility

DS/EN 4473:2010 航空航天系列紧固件用铝着色涂料技术规范

This European Standard defines the qualification test conditions for aluminium pigmented coatings applicable to fasteners in titanium, titanium alloys, nickel base alloys and corrosion resisting steels. The aluminium pigmented coatings are not applicable to fasteners in non-corrosion resistant steels.Temperature class: 315 °C Type I : Coating with chromate and a cetyl alcohol lubricant.Type II : Coating without chromate and an cetyl alcohol lubricant. Type III : Coating with chromate, no additional lubricant.Type IV : Coating without chromate, no additional lubricant.

Aerospace series - Aluminium pigmented coatings for fasteners - Technical specification

DS/EN 2434-001:2010 航空航天系列色漆和清漆双组分冷固化聚氨酯面漆第001部分：基本要求

This European Standard specifies the basic requirements for a two component polyurethane finish, available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to prEN 2435-02. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 001: Basic requirements

DS/EN 2434-003:2010 航空航天系列色漆和清漆双组分冷固化聚氨酯面漆第003部分：内部的柔性和高流体阻力

This European Standard specifies the requirements for a two component polyurethane finish, in a limited range of colours, to be applied over a primer for interior aerospace applications, offering flexibility and high resistance to fluid attack.The properties specified in this European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN 23270 and painted with primer to prEN 2435-03. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of t

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 003: Flexible and high fluid resistance for interior

DIN 65046-6:2010 航空航天.表面防护的试验方法.第6部分:化学镀层和电镀层.不适用于新设计

Aerospace - Test methods for surface protection; Paints and varnishes - Part 6: Chemical and electroplated coatings - Inactive for new design

DIN 65046-5:2010 航空航天.表面保护涂层的试验方法.油漆和清漆.第5部分:涂层阻力试验

Aerospace - Methods of test for surface protective coatings; Paints and varnishes - Part 5: Coating resistance tests

DIN 65046-2:2010 航空航天.表面保护涂层的试验方法.油漆和清漆.第2部分:试样,试样的制备,干燥

Aerospace - Methods of test for surface protective coatings; Paints and varnishes - Part 2: Specimens, preparation of specimens, drying

DIN 65046-3:2010 航空航天.表面保护涂层的试验方法.油漆和清漆.第3部分:按交货条件进行的试验

Aerospace - Methods of test for surface protective coatings; Paints and varnishes - Part 3: Tests in as-delivered condition

DIN 65046-1:2010 航空航天.表面保护层的试验方法.油漆和清漆.第1部分:概览和定义

Aerospace - Methods of test for surface protective coatings; Paints and varnishes - Part 1: Survey and identifications

DIN 65046-4:2010 航空航天.表面保护涂层的试验方法.油漆和清漆.第4部分:涂层试验

Aerospace - Methods of test for surface protective coatings; Paints and varnishes - Part 4: Testing of coatings

BS EN 4473:2010 航空航天系列.紧固件用铝着色涂膜.技术规范

This European Standard defines the qualification test conditions for aluminium pigmented coatings applicable to fasteners in titanium, titanium alloys, nickel base alloys and corrosion resisting steels. The aluminium pigmented coatings are not applicable to fasteners in non-corrosion resistant steels. Temperature class: 315 °C Type I : Coating with chromate and a cetyl alcohol lubricant. Type II : Coating without chromate and an cetyl alcohol lubricant. Type III : Coating with chromate, no additional lubricant. Type IV : Coating without chromate, no additional lubricant.

Aerospace series. Aluminium pigmented coatings for fasteners. Technical specification

EN 4473:2010 航空航天系列.紧固件用铝着色涂膜.技术规范

This European Standard defines the qualification test conditions for aluminium pigmented coatings applicable to fasteners in titanium, titanium alloys, nickel base alloys and corrosion resisting steels. The aluminium pigmented coatings are not applicable to fasteners in non-corrosion resistant steels. Temperature class: 315 ℃, Type I: Coating with chromate and a cetyl alcohol lubricant. Type II: Coating without chromate and an cetyl alcohol lubricant. Type III: Coating with chromate, no additional lubricant. Type IV: Coating without chromate, no additional lubricant.

Aerospace series - Aluminium pigmented coatings for fasteners - Technical specification

EN 2434-004:2010 航空航天系列.油漆和清漆.双组分冷固化聚氨酯精饰.高灵活性

This European Standard specifies the requirements for a two component polyurethane finish to be applied over a primer mainly for exterior aerospace applications, offering high flexibility The properties specified inThis European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN 23270 and painted with primer to prEN 2435-002. The ability of the material to be used for a specific application (e. g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 004: High flexibility

EN 2434-001:2010 航空航天系列.涂料和清漆.双组分冷固化聚氨酯光洁度.基本要求

This European Standard specifies the basic requirements for a two component polyurethane finish, available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications. The properties specified inThis standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to EN 2435-002. The ability of the material to be used for a specific application (e. g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 001: Basic requirements

EN 2434-002:2010 航空航天系列.涂料和清漆.双组分冷固化聚氨酯光洁度.第002部分:高耐化学性

This European Standard specifies the requirements for a two component polyurethane finish to be applied over a primer for interior and exterior aerospace applications, where maximum resistance to normal operational fluids is required. The properties specified inThis European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to EN 2435-002. The ability of the material to be used for a specific application (e. g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 002: High chemical resistance

EN 2434-003:2010 航空航天系列.涂料和清漆.双组分冷固化聚氨酯光洁度.内部柔韧性和高流动阻性

This European Standard specifies the requirements for a two component polyurethane finish, in a limited range of colours, to be applied over a primer for interior aerospace applications, offering flexibility and high resistance to fluid attack. The properties specified inThis European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN 23270 and painted with primer to EN 2435-003. The ability of the material to be used for a specific application (e. g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 003: Flexible and high fluid resistance for interior

LST EN 4637-2010 航天系列-爆炸介质-白刚玉

Aerospace series - Blast media - White corundum

LST EN 4638-2010 航空航天系列 喷砂介质 棕刚玉，无铁

Aerospace series - Blast media - Brown corundum, without iron