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

DS/EN 2436-004:2006 航空航天系列 油漆和清漆 耐腐蚀无铬酸盐双组份冷固化底漆 第004部分：具有表面处理公差的高耐腐蚀性和耐流体性

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

DS/EN 4508:2006 航空航天系列《色漆和清漆》《防滑涂料试验方法》《滑动摩擦性能的测定》

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

TIA PN 3-0095-AD2 [E]-1-2006 增强的密码算法

Project Number 3-0095-AD2 [E]-1, proposed addendum of a TIA

Enhanced Cryptographic Algorithms To be published as TIA-946-2[E]

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

BS 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.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 - For exterior use with surface preparation tolerance

DS/EN 2436-003:2006 航空航天系列 色漆和清漆 耐腐蚀无铬酸盐双组份冷固化底漆 第003部分：高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

DS/EN 2434-005:2006 航空航天系列色漆和清漆双组分冷固化聚氨酯面漆第005部分：军事应用的高柔韧性和耐化学试剂性

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

DS/EN 2435-001:2006 航空航天系列色漆和清漆耐腐蚀铬酸盐二组分冷固化底漆第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

DS/EN 2435-002:2006 航空航天系列色漆和清漆耐腐蚀铬酸盐二组分冷固化底漆第002部分：高耐腐蚀性

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

DS/EN 2435-003:2006 航空航天系列色漆和清漆耐腐蚀铬酸盐二组分冷固化底漆第003部分：高耐腐蚀性和耐流体性

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

DS/EN 2435-004:2006 航空航天系列色漆和清漆耐腐蚀铬酸盐二组分冷固化底漆第004部分：高耐腐蚀性和耐流体性，具有表面制备公差

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

DS/EN 2435-005:2006 航空航天系列色漆和清漆耐腐蚀铬酸盐二组分冷固化底漆第005部分：军用高耐蚀性

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

DS/EN 2436-001:2006 航空航天系列色漆和清漆耐腐蚀无铬酸盐双组份冷固化底漆第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

SAE ARP4252A-2006 表面清洁度的仪器测定法

This Aerospace Recommended Practice is intended as a guide toward standard practices for the determination of surface cleanliness that are applicable to field operation. Some of these methods can also be used to determine quality assurance that a surface has been properly prepared and maintained. The instrumental methods are: Wettabaility, Surface Potential Difference (SPD), Ellipsometry, and Optically Stimulated Electron Emission (OSEE). Each instrument is described with respect to measurement techniques, limitations, and advantages and types of available instruments. Elementary theoretical prinicples and examples of the use of each instrument are also giv

Instrumental Methods of Determining Surface Cleanliness

TIA-1096-2006 电信.电话终端设备连接器.终端设备和电话网络连接要求

The technical criteria in this standard are intended to protect the telephone network from the harms defined by the Federal Communications Commission (FCC) Part 68, Section 3 rules in Title 47 of the Code of Federal Regulations (47 CFR 68.3). This standard specifies physical dimensions, mechanical characteristics, and contact material requirements fo

Telecommunications Telephone Terminal Equipment Connector Requirements for Connection of Terminal Equipment to the Telephone Network

BS 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.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 - High corrosion resistance

BS 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 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 - Corrosion resistant chromated two component cold curing primer - Part 001: Minimum requirements

BS 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

BS EN 2436-004:2006 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.带有表面处理公差的强耐腐蚀性和耐流体性

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 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 with surface preparation tolerance

BS 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固化环氧底漆的耐腐蚀性.军用强耐腐蚀性

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

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