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

BS EN 2435-005:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.军用强耐腐蚀性

This standard defines the requirements for a two component, chromated epoxy, high corrosion resistant primer. The coating shall be suitable for use on chromic acid anodised or conversion coated aluminium alloys and other suitably prepared substrates.

Aerospace series - Paints and varnishes - Corrosion resistant chromated two component cold curing primer - High corrosion resistance for military application

BS EN 2435-004:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.有表面制备公差的强耐腐蚀性和耐流动性

This standard defines the requirements for a two component, chromated epoxy or polyurethane, high corrosion resistant primer with a high degree of resistance to aggressive hydraulic fluids and improved tolerance to the standard of surface preparation which can be used with or without a finish for aerospace applications. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process A or B or C or D and ISO 3270. 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 - Corrosion resistant chromated two component cold curing primer - High corrosion and fluid resistance with surface preparation tolerance

BS EN 2434-005:2006 航空航天系列.涂料和清漆.双组分冷固化聚氨酯光洁度.军用高柔性和强耐化学试剂性

This standard specifies the requirements for a two component flexible polyurethane topcoat to be applied over EN 2435-005 or EN 2436-006 primer mainly for exterior aerospace applications. The primer and the finish tested to this specification will be from the same manufacturer applied in accordance with (i.a.w.) their instruction/Table 1.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - High flexibility and chemical agent resistance for military application

BS EN 2436-003:2006 航空航天系列.涂料和清漆.耐腐蚀不含铬酸盐的双组分冷固化底漆.强耐腐蚀性和耐流体性

This standard specifies the requirements for a two component, cold curing, chromate-free epoxy or polyurethane, high corrosion and fluid resistant primer which can be used with or without a finish for aerospace applications. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and ISO 3270. 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 - Corrosion resistant chromate-free two component cold curing primer - High corrosion and fluid resistance

BS EN 2436-002:2006 色漆和清漆.无铬酸盐耐腐蚀双组分冷固化底漆.第002部分:高抗蚀性

This standard specifies the requirements for a two component, cold curing, chromate-free epoxy or polyurethane, high corrosion resistant primer which can be used with or without a finish for aerospace applications. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and ISO 3270. 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.

Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 002: High corrosion resistance

BS EN 2436-001:2006 航空航天系列.油漆和清漆.不含铬酸盐的耐腐蚀双组分冷固化底漆.第001部分:基本要求

This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, corrosion resistant primer which can be used with or without a finish for aerospace applications. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process A and ISO 3270. 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 - Corrosion resistant chromate-free two component cold curing primer - Part 001: Basic requirements

EN 4508:2006 航空航天系列.耐滑层试验方法.滑动摩擦特性的测定

This standard specifies the procedure for determination of the sliding friction behaviour of an anti slip coating.

Aerospace series - Paints and varnishes - Test method for anti slip coatings - Determination of the sliding friction behaviour

EN 2436-004:2006 航空航天系列.涂料和清漆 耐腐蚀加铬酸盐双组分冷固化底漆.第004部分:有表面预加工公差的强耐腐蚀性和耐液体性

This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, high corrosion and fluid resistant primer with improved tolerance to the standard of surface preparation which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process D and ISO 3270. 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 requir

Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 004: High corrosion and fluid resistance with surface preparation tolerance

EN 2436-002:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.第002 部分:强耐腐蚀性

This standard specifies the requirements for a two component, cold curing, chromate-free epoxy or polyurethane, high corrosion resistant primer which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and ISO 3270. 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 - Corrosion resistant chromate-free two component cold curing primer - Part 002: High corrosion resistance

EN 2436-005:2006 航空航天系列.涂料和清漆.耐腐蚀不含铬酸盐的双组份冷固化底漆.第005部分:用于外部带有表面处理公差的涂料和清漆

This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, corrosion resistant primer which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process D and ISO 3270. 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 - Corrosion resistant chromate-free two component cold curing primer - Part 005: For exterior use with surface preparation tolerance

EN 2436-006:2006 航空航天系列.涂料和清漆.不含铬酸盐的双组分冷加工环氧底漆的耐腐蚀性.第006部分:军用强耐腐蚀性

This document specifies the requirements relating to:Aluminium alloy AL-P2618A Forging stock for aerospace applications.

Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing epoxy primer - Part 006: High corrosion resistance for military application

EN 2435-005:2006 航空航天系列.涂料和清漆.含铬酸盐的双组分冷加工底漆的耐腐蚀性.第005部分:军用强耐腐蚀性

This standard defines the requirements for a two component, chromated epoxy, high corrosion resistant primer.The coating shall be suitable for use on chromic acid anodised or conversion coated aluminium alloys and other suitably prepared substrates.

Aerospace series - Paints and varnishes - Corrosion resistant chromated two component cold curing primer - Part 005: High corrosion resistance for military application

EN 2435-003:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.第003 部分:耐强腐蚀和耐液体侵蚀性

This standard defines the requirements for a two component, chromated epoxy or polyurethane, high corrosion resistant primer with a degree of resistance to aggressive hydraulic fluids which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and ISO 3270. 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 - Corrosion resistant chromated two component cold curing primer - Part 003: High corrosion and fluid resistance

EN 2435-001:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.第001部分:最低要求

This standard specifies the minimum requirements for a two-component, chromated epoxy or polyurethane,corrosion resistant primer which can be used with or without a finish 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 ISO 3270. The ability of the material to be used for a specific application (e.g. alternative substrate, 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 - Corrosion resistant chromated two component cold curing primer - Part 001: Minimum requirements

EN 2436-003:2006 航空航天系列.涂料和清漆.耐腐蚀不含铬酸盐的双组分冷固化底漆.第003部分:强耐腐蚀性和耐流体性

This standard specifies the requirements for a two component, cold curing, chromate-free epoxy or polyurethane, high corrosion and fluid resistant primer which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and ISO 3270. 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 - Corrosion resistant chromate-free two component cold curing primer - Part 003: High corrosion and fluid resistance

EN 2436-001:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.第001部分:基本要求

This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, corrosion resistant primer which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process A and ISO 3270. 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 - Corrosion resistant chromate-free two component cold curing primer - Part 001: Basic requirements

EN 2435-004:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.第004部分:有表面制备公差的耐强腐蚀性和液体侵蚀性

This standard defines the requirements for a two component, chromated epoxy or polyurethane, high corrosion resistant primer with a high degree of resistance to aggressive hydraulic fluids and improved tolerance to the standard of surface preparation which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process A or B or C or D and ISO 3270. 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 sup

Aerospace series - Paints and varnishes - Corrosion resistant chromated two component cold curing primer - Part 004: High corrosion and fluid resistance with surface preparation tolerance

EN 2435-002:2006 航空航天系列.涂料和清漆.耐腐蚀加铬酸盐双组分冷固化底漆.第002部分:强耐腐蚀性

This standard defines the requirements for a two component, chromated epoxy or polyurethane, high corrosion resistant primer with a degree of resistance to aircraft fluids which can be used with or without a finish for aerospace applications.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and ISO 3270. 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 - Corrosion resistant chromated two component cold curing primer - Part 002: High corrosion resistance

EN 2434-005:2006 航空航天系列.涂料和清漆.双组分冷固化聚氨酯光洁度.第005部分:军用高柔性和耐化学试剂性

This standard specifies the requirements for a two component flexible polyurethane topcoat to be applied over EN 2435-005 or EN 2436-006 primer mainly for exterior aerospace applications.The primer and the finish tested to this specification will be from the same manufacturer applied in accordance with (i.a.w.) their instruction/Table 1.

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 005: High flexibility and chemical agent resistance for military application

NF L06-831:2006 航空航天系列.金属零件.表面承压.钢丸、玻璃珠和瓷珠

Aerospace series - Metallic parts - Inducement compressive surface stresses - Steel shot, glass beads and ceramic beads.