AIPS_05_02-003空客油漆规范翻译.docx

AIRBUSAIPS05-02-003Issue 4Page 1 of 21December 2010AIPSAirbus Process SpecificationApplication of external paint systemsPublished and distributed by AIRBUS S.A.S.ENGINEERING DIRECTORATE31707 BLAGNAC CedexFRANCECopyright reservedRef. No AIPS 05-02-003Doc Master: Uncontrolled copy when printed (19540)空中客车AIPS05-02-003版本4第1页（共21页）2010年12月AIPS空客工艺规范外部油漆系统应用程序由空客北欧航空公司出版和发行工程理事会31707 BLAGNAC Cedex法国著作权所有参考文件编号 AIPS 05-02-003文档控制: 印刷时非受控副本 (19540)Contents 1 Scope 2 Normative references 3 Definition, applicability and limitations 4 Engineering requirements 5 Technical qualification 6 First part qualification 7 Series production inspection 8 Rework 9 Environment, health and safety Annex A (Informative) Annex B(Normative) Annex C(Informative) Annex D (Normative) Annex E (Informative)内容1 范围2 引用标准3 定义、适用性和局限性4 工程（技术）要求5 技术鉴定6 首件鉴定7 批产检验8 返工9 环境、健康和安全附录A (告知性)附录B (规范性)附录C (告知性)附录D (规范性)附录E (告知性)1 Scope This Airbus Process Specification defines the Engineering requirements for application of external paint systems. This specification does not give detailed instructions; these are given in the Process Instructions (PI) / Airbus Process Instruction (AIPI) and the Work Instructions. This specification shall not be used as an inspection document. It shall be applied when mentioned in the relevant standard, material specification or Definition Dossier. 1 范围该空客工艺规范定义了外部油漆系统应用程序的工程要求。该规范并未给出详细说明；而是在工艺指导书(PI)/空客工艺指导书(AIPI)和作业指导书中给出。该规范不得作为一个检验文档。它适用于在相关标准、材料规范或定义档案中被提及时。2 Normative references Only normative references cited in the text are listed hereafter. The latest issue of the publication referenced shall be used. ABS5044 Clad sheets and strips Aluminium alloy 2024 standard surface quality thickness 0,2mm to 6,00mm AIMS04-04-001 Corrosion inhibiting primer AIMS04-04-002 Non corrosion inhibiting primer AIMS04-04-007 Abrasion resistant paint AIMS04-04-012 External paint system: wash primer, primer and top coat AIMS04-04-013 External paint system: primer + top coat AIMS04-04-014 External paint system: primer, intermediate coat + top coat AIMS04-04-017 External aluminised elastomeric top coat AIMS04-04-023 UV resistant external varnish AIMS04-04-025 External decorative paint AIMS04-04-026 Wing coating system AIMS04-04-027 Wear resistant coatings for areas with low chemical impact AIMS04-04-031 Chromate free external paint system: primer + top coat applied on basic primer AIMS04-04-032 Chromate free external paint system: primer + intermediate coat + top coat applied on basic primer AIMS04-04-033 Chromate free external paint system : Primer + Basecoat + Clearcoat on basic primer AIMS04-04-034 External paint system: chromate free primer + wing coating AIMS04-04-036 Chromate free external paint system primer: Primer + Matt top coat applied on basic primer AIMS04-04-037 Chromate free external paint system: Primer + Intermediate coat + Basecoat + Clearcoat on basic primer AIPS02-01-001 Chromic Acid Anodising (CAA) AIPS02-01-003 Tartaric Sulphuric Anodising of aluminium alloys for corrosion protection and paint pre- treatment AITM2-0011Drying time AITM2-0027Determination of colour differences AM2435External painting quality criteria EN9103 Aerospace series-Quality management systems -Variation management of key characteristics ISO1518 Paints and varnishes Scratch test ISO2409 Paints and varnishes Cross cut test ISO2431 Paints and varnishes Determination of flow time by use of flow cups ISO2808 Paints and varnishes Determination of film thickness ISO2812/1 Paints and varnishes Determination of resistance to liquids ISO2813 Paints and varnishes Measurement of specular gloss of non-metallic paint film at 20, 60 and 852 引用标准只有该文档中援引的引用标准会在下方列出。应使用引用刊物的最新版本。ABS5044 涂层板和带铝合金2024标准表面质量厚度0.2毫米到6.00毫米AIMS04-04-001 防腐蚀底漆AIMS04-04-002 非防腐蚀底漆AIMS04-04-007 耐磨性油漆AIMS04-04-012 外部油漆系统: 蚀洗用底漆，底漆及表面涂层AIMS04-04-013 外部油漆系统: 底漆及表面涂层AIMS04-04-014 外部油漆系统:底漆,中间涂层+表面涂层AIMS04-04-017 外部铝化弹性表面涂层AIMS04-04-023 抗紫外线外部清漆AIMS04-04-025 外部装饰油漆AIMS04-04-026 机翼涂层系统AIMS04-04-027 低化学影响区域的耐磨性镀层AIMS04-04-031 无铬酸盐外部油漆系统:底漆+用于基础底漆上的表面涂层AIMS04-04-032 无铬酸盐外部油漆系统:底漆+中间涂层+用于基础底漆上的表面涂层AIMS04-04-033 无铬酸盐外部油漆系统:底漆+底涂层+基础底漆上的透明涂层AIMS04-04-034 外部油漆系统:无铬底漆+机翼涂层AIMS04-04-036 无铬酸盐外部油漆系统:底漆+用于基础底漆上的马特表面涂层AIMS04-04-037 无铬酸盐外部油漆系统:底漆+中间涂层+底涂层+基础底漆上的表面涂层AIPS02-01-001 铬酸阳极氧化(CAA)AIPS02-01-003 用于防腐和油漆预处理的铝合金酒石酸阳极氧化AITM2-0011 干燥时间AITM2-0027 颜色差异的测定AM2435 外部涂覆质量标准EN9103 航空航天系统质量管理体系关键特性的动态管理ISO1518 油漆和清漆划痕试验ISO2409 油漆和清漆划格（横断）测试ISO2431 油漆和清漆使用流杯测定流动时间ISO2808 油漆和清漆膜厚的测定ISO2812/1 油漆和清漆防水性测定ISO2813 油漆和清漆20,60和85非金属油漆涂膜光泽率的测量3 Definition, applicability and limitations 3.1 Definition 3.1.1 External paint system The combination of individual paint products that are applied one after the other and that gives protection to the aircraft structure as well as providing the Customer livery. 3.1.2 Paint shop A production facility that is only intended for surface preparation and paint application. 3.1.3 Basic protections on aircraft The protection of metallic parts on which the external paint scheme is applied may consist either of an anodised layer or a chemical conversion coating alone or an electrolytic pre treatment plus a primer. The protection of composite parts on which external surfaces the external paint scheme is applied may consist in application of a previous primer or primer plus pore filler. 3.1.4 Developer A company that is responsible for the development of a process related to this AIPS. 3.1.5 User The user is responsible for the application of a specific process qualified to this AIPS on external surfaces of Airbus aircraft. The user might be the developer of the process, an airline, a commercial company or an Airbus site. 3 定义、适用性和局限性3.1 定义3.1.1 外部油漆系统被一个接着另一个地使用，保护飞机结构以及提供顾客徽记或专色的单个油漆产品的组合。3.1.2 油漆车间只用于表面处理和油漆施工的生产设施。3.1.3 飞机上的基础保护应用外部油漆方案的金属零件的保护可单独由一层阳极化层或一层化学转化镀层组成，也可由一个电解预处理加上底漆组成。外表面应用外部油漆方案的复合材料零件的保护可由使用预先底漆或底漆+孔隙填充组成。3.1.4 开发者负责开发该空客工艺规范相关工艺的公司。3 1 5 用户用户对这份空客飞机外表面空客工艺规范规定的特殊工艺的使用负责。用户可能是工艺开发人员,航空公司,商业公司或一个空客现场。3.2 Applicability and limitations 3.2.1 Applicability This Airbus specification is applicable when invoked by the drawing directly or through another document for the purpose given in the scope. When processing to AIPS 05-02-003 is required, it shall be invoked on the drawing by the words “Application of external paint systems to AIPS 05-02-003”. The process described in this document is applicable for all aircraft programs and all types of application of any external paint system as defined hereafter: - External paint schemes (chromate loaded): wash primer paint system (AIMS 04-04-012), primer and top coat (AIMS 04-04-013), intermediate coat paint system (AIMS 04-04-014), wing coating system (AIMS 04-04-026), - Chromate free external paint scheme: primer + top coat applied on basic primer (AIMS 04-04-031), primer + intermediate coat + top coat applied on basic primer (AIPS 04-04-032), chromate free primer + wing coating (AIMS 04-04-034), primer + basecoat + clearcoat on basic primer (AIMS 04-04-033), primer + intermediate coat + basecoat + clearcoat on basic primer (AIMS 04-04-037), primer + Matt top coat applied on basic primer (AIMS 04-04-036) - Elastomeric paint (AIMS 04-04-017), - External varnish (AIMS 04-04-023), - External decorative paint (AIMS 04-04-025), -Abrasion resistant paint (AIMS 04-04-007), - Wear resistant coatings (AIMS 04-04-027). The process is also valid for the application of external top coat to parts where external surfaces have been painted in a full paint scheme at an earlier detail or assembly stage. 3.2 适用性和局限性3.2.1 适用性该空客规范是为了范围中指出的目的，图纸直接援引或通过另一个文档援引时适用。 当需要用到AIPS 05-02-003工艺时，引用时应在图纸上注明“外部油漆系统应用程序 AIPS 05-02-003”。该文档中描述的工艺适用于所有飞机项目和以下定义的任何外部油漆系统的所有类型应用程序:外部油漆方案(含铬酸盐): 蚀洗用底漆油漆系统(AIMS 04-04-012)、底漆和表面涂层(AIMS 04-04-013),中间涂层油漆系统(AIMS 04-04-014)，机翼涂层系统(AIMS 04-04-026),无铬酸盐外部油漆方案: 底漆+用于基础底漆上的表面涂层(AIMS 04-04-031), 底漆+中间涂层+用于基础底漆上的表面涂层(AIPS 04-04-032), 无铬底漆+机翼涂层(AIMS 04-04-034), 底漆+底涂层+基础底漆上的透明涂层(AIMS 04-04-033), 底漆+中间涂层+底涂层+基础底漆上的表面涂层(AIMS 04-04-037), 底漆+用于基础底漆上的马特表面涂层(AIMS 04-04-036)弹性油漆(AIMS 04-04-017),外部清漆 (AIMS 04-04-023),外部装饰油漆(AIMS 04-04-025),耐磨性油漆(AIMS 04-04-007),耐磨性涂层(AIMS 04-04-027)。该工艺对于那些在早期细化阶段或装配阶段已经在外表面涂覆了一个完整油漆方案的零件使用外部表面涂层同样有效。3.2.2Limitations 3.2.2.1 This process specification does not apply to the application of functional coatings e.g. antistatic, anti-erosion and antislip emergency / walkway paint. 3.2.2.2 This process shall not be applied to components not being painted or which may be damaged by the process without previous masking (antennas, cameras, probes, lights, windows). 3.2.2.3 Unless otherwise specified in each IPS, environmental conditions for the application of paint systems shall be defined per Annex A. 3.2.2.4 The exterior painting process shall be carried out only after surface preparation performed as defined in the relevant AIPS.3.2.2 局限性3.2.2.1该工艺规范不适用于功能性镀层，如抗静电、抗侵蚀和防滑紧急/走道油漆的使用。3.2.2.2该工艺不得用于没有喷涂的零部件或可能由于缺少提前遮蔽的工艺过程而受损的零部件 (天线、相机、探针、灯光、窗户等)。3.2.2.3除非在每个IPS（工艺规范）中另有说明，使用油漆系统的环境条件应按照附录A确定。3.2.2.4外用涂覆工艺只能在按照相关空客工艺规范进行表面处理后执行。4 Engineering requirements Engineering requirements are minimum requirements specified by Responsible Engineering to ensure optimal performance of the manufacturing process. All Engineering requirements have to be met and controlled in production. 4.1Performance Requirements 4.1.1 Adhesion on test panels Before the beginning of testing, a drying time of 168h at 23C, (55 5)% RH shall be observed. A cross cut test shall be performed after the drying time in accordance with ISO 2409. The specimens shall be divided into two sets with an equal number of specimens in each set. One test (set?) shall be tested in its initial condition at (232)C and the remaining set shall be tested after immersion in demineralized water for 14 days at (232)C in accordance with ISO 2812 part 1. The requirements are grade 0 for the initial condition and grade 1 after water immersion. 4 工程要求工程要求是责任工程（技术员）为确保生产工艺的最佳性能而规定的最低要求。所有工程要求必须得到满足并在生产中受控。4.1 性能要求4.1.1 测试板上的附着力在测试开始前，应该在23C、(555)%相对湿度下观察168小时的干燥时间。应该在干燥时间后按照ISO 2409进行划格（横断）测试。试样应分成两组，每组包含相同数量的试样。一组试样应在其初始条件(232) C下测试，剩下的一组试样应按照ISO 2812 第1部分的描述，在(232) C下浸入软化水14天后进行测试。要求是初始条件为等级0，浸水后为等级1。4.1.2 Thickness on test panels After drying for 24 hours, the thickness of each coat shall be measured per ISO 2808 on test pieces. The thickness of each paint layer shall be within the specified requirements for that layer over the entire panel area. Measurements shall be carried out to validate that this requirement has been met. Thickness shall be checked on test samples using destructive (composite samples) or not destructive methods (metallic samples) for composite parts if a suitable non-destructive method to measure directly on the part does not exit(exist?) or is not available. For each primer (basic primer and refresher coat of external primer), a minimum thickness of 15 m shall be applied in order to achieve the corrosion resistance requirement.4.1.2 测试板上的厚度在干燥24小时后，应该在试片上按照ISO 280测量每个镀层的厚度。对于整个面板区域上的漆层，每个漆层的厚度不应超过规定要求。应进行测量以确认满足该要求。对于复合材料零件，如果一个合适的在零件上直接测量的非破坏性方法不存在或不可用，则应使用破坏性(复合材料样件)或非破坏性方法(金属样件)在试样上检查厚度。 对于每层底漆(基础底漆和外部底漆的刷新涂层)，最小厚度应为15m以达到耐腐蚀的要求。The thickness of each paint layer shall be in accordance with the relevant AIMS. For example : Primer: 15 to 25 m Intermediate coat: 8 to 12 m Top coat: 50 to 130 m according to the colour. For information, the following are dry film thicknesses for Master colours:Table 1: Dry film thicknessMaster ColourFor information only,thickness when appliedon chromated primerWHITE M 8001100 130 mWHITE M 8002 (Matterhorn)50 70 mWHITE M 800380 100 mGREY M 900150 70 mGREY M 900260 80 mGREY M 9004 (Wing coating)30 40 mFor other colours, dry film thicknesses are given in paint suppliers documentation.Basecoat: 30 to 90 m according to the colour Clearcoat: 30 to 80 m according to the colour For the anti-abrasion paint, the thickness shall not exceed 200 m. For top coat and decorative paint, the thickness will be applied to reach the hiding power according to the different colours. In any case, the total thickness of the complete paint scheme (including notably detailed primer(s), decorative paints and clearcoat) shall not exceed 330 m on the whole aircraft (including radome). If this requirement is not assessed, a derogation shall be raised. Specific case: mica paint: A maximum of 5 measured points where the thickness is between 330 m and 400 m shall be accepted on condition that these points shall have at least an adjacent area within the tolerance. 每个漆层的厚度应符合相关的空客材料规范。例如:底漆:15到25m中间涂层:8到12m表面涂层:根据色彩50到130m。以下是主要颜色的干膜厚度以供参考:表格1：干膜厚度主要颜色仅供参考,当用在铬酸盐底漆上时的厚度WHITE白 M 8001100 130 mWHITE M 8002 (Matterhorn)50 70 mWHITE M 800380 100 mGREY灰 M 900150 70 mGREY M 900260 80 mGREY M 9004 (Wing coating机翼镀层)30 40 m对于其它颜色，干膜厚度在油漆供应商的证明文件中给出。底涂层: 根据颜色30到90m透明涂层: 根据颜色30到80m 对于耐磨性油漆，厚度不得超过200m。对表面涂层和装饰性油漆，厚度将根据不同颜色用于达到遮盖的效果。无论如何，完整油漆方案的总厚度 (尤其包括精细底漆、装饰性油漆和透明涂层) 在整个飞机(包括整流罩)不得超过330m。如果没有评估该要求，应该提出一个变通的要求。具体案例:云母漆:最多5个测量点的厚度在330m和400m之间应被接受，只要这些点至少有一个相邻区域在公差范围内。4.1.3 Radioelectrical performance (only applicable for radome) One of the key function of the radome is its radioelectrical transparency in relation to the electromagnetic signals transmitted and received by the different antennas. Radioelectrical performances of the radomes depend on the nature, the composition and the thickness of the paints. Whatever the paint type, the transparency attenuation due to external paint scheme applied in the final paintshops (i.e.: not including detailed primers, pore-filler, anti-erosion paint and antistatic paint) shall be inferior to: - 4% for Single Aisle (Evolution 2) radome, - 4% for Long Range/WideBody (Evolution 2) radome, - 3,4% for A380 Basic radome. The specific transparency attenuations for all types of external paints are given in Annex B. For each airline livery/paint scheme, specific attenuation of each layer shall be calculated and summed up to check that the above requirement is met. If necessary (in particular when several colors are applied on the radome), paint application by juxtaposition will be preferred to overlapping in order to meet the above requirement.4.1.3 无线电性能 (仅适用于整流罩)整流罩的一个关键功能就是其涉及使用不同天线传输和接收电磁信号的无线电透明性。整流罩的无线电性能依赖于其性质、构成和油漆厚度。无论何种类型的油漆，在最终油漆车间使用外部油漆方案造成的透明度衰减量 (即:不包括精细底漆,孔隙填充剂,抗腐蚀油漆和抗静电油漆)应低于:-单通道(进化2)整流罩4%,-远程/宽体(进化2)整流罩4%,-A380基础整流罩3,4%。所有类型外部油漆的具体透明度衰减量在附录B中给出。每个航空公司徽标/油漆方案，应该计算和总结每一层的具体衰减量，以检查以上要求得到满足。如果有必要(特别是当在整流罩上使用多个颜色时)，将倾向于使用并列喷漆重叠操作，以满足上述要求。4.2Other requirements 4.2.1Appearance of dry film After drying, the paint system shall be uniform in appearance and free from surface defects as defined in Annex C. The external painting quality criteria are specified in AM2435, including specular gloss and orange peel criteria. 4.2.2Colour difference The colour shade of the painted surface shall be in accordance with the Airbus master colours (M9001, M9002, M9004, M8001, M8002, M8003) or for the other colours as agreed with the customer by visual comparison. The requirements for the Master colour are as following : M8001 E 0.70 M8002 E 0.35 M8003 E 0.30 M9001 E 0.50 M9002 E 0.40 M9004 E 0.704.2 其它要求4.2.1 干膜外观干燥后，油漆系统应按照附录C中的规定统一外观和避免表面缺陷。外部油漆质量标准在AM2435中有规定，包括光泽度和橙皮皱（橘皮状表面缺损）标准。4.2.2 颜色差异油漆面的色度应当依照空客主要颜色(M9001，M9002，M9004，M8001，M8002，M8003)或其它颜色按照与客户约定通过视觉比较。主要颜色的要求如下:M8001E0.70M8002E0.35M8003E0.30M9001E0.50M9002E0.40M9004E0.704.3Key Characteristic Key Characteristics according to EN9103 are defined by responsible engineering based on a risk analysis for parts manufactured by this process. Key characteristics shall be defined on product level and if necessary also on process level. They shall be subject to variation control by production organization according to EN9103. Key Characteristics do not relieve the production organization from meeting all engineering requirements defined in this document.4.3 关键特性依据EN9103的关键特性是由责任工程（技术员）基于对该工艺中生产零件的风险分析而定义的。关键特性应当在产品级别进行定义，如果有必要还可以在工艺级别定义。关键特性应当依据EN9103受生产组织的动态控制。关键特性不能免除生产组织满足该文件中定义的所有工程要求的责任。Table 2: Key Characteristic (concluded) 表格2：关键特性（总结）Product Key Characteristic产品关键特性Process Key Characteristic 工艺关键特性No. 编号Designation名称Requirement/Limit 要求/限制Sub.-No.子编号Designation名称Requirement/Limit要求/限制1Paint adhesion油漆附着性See 4.1.1 ofAIPS05-02-0031.1Surface cleaning and activation of substrate 表面清洗和基质激活Acc. To AIPS09-04-0011.2Drying times, overcoating times, flash-off times, masking times 干燥时间，涂装时间，晾干时间，遮蔽时间Acc. To relevant IPS and AIPI05-02-0032Full performanceProperties 全性能属性See relevantAIMS 见相关AIMS2.1Storage conditions储存条件As defined in relevant IPS and AIP