ASD-STAN PREN 2435-01-1994 Aerospace Series Paints and Varnishes Corrosion Resistant Chromated Two Component Cold Curing Primer Part 01 Minimum Requirements (Edition P 1)《航空航天系列 油.pdf

上传人:explodesoak291 文档编号:451037 上传时间:2018-11-23 格式:PDF 页数:5 大小:203.63KB
下载 相关 举报
ASD-STAN PREN 2435-01-1994 Aerospace Series Paints and Varnishes Corrosion Resistant Chromated Two Component Cold Curing Primer Part 01  Minimum Requirements (Edition P 1)《航空航天系列 油.pdf_第1页
第1页 / 共5页
ASD-STAN PREN 2435-01-1994 Aerospace Series Paints and Varnishes Corrosion Resistant Chromated Two Component Cold Curing Primer Part 01  Minimum Requirements (Edition P 1)《航空航天系列 油.pdf_第2页
第2页 / 共5页
ASD-STAN PREN 2435-01-1994 Aerospace Series Paints and Varnishes Corrosion Resistant Chromated Two Component Cold Curing Primer Part 01  Minimum Requirements (Edition P 1)《航空航天系列 油.pdf_第3页
第3页 / 共5页
ASD-STAN PREN 2435-01-1994 Aerospace Series Paints and Varnishes Corrosion Resistant Chromated Two Component Cold Curing Primer Part 01  Minimum Requirements (Edition P 1)《航空航天系列 油.pdf_第4页
第4页 / 共5页
ASD-STAN PREN 2435-01-1994 Aerospace Series Paints and Varnishes Corrosion Resistant Chromated Two Component Cold Curing Primer Part 01  Minimum Requirements (Edition P 1)《航空航天系列 油.pdf_第5页
第5页 / 共5页
亲,该文档总共5页,全部预览完了,如果喜欢就下载吧!
资源描述

1、CEN PREN*2435-OL 94 3404589 0064148 T95 Edition approved for publication 1994-06-30 AECMA STANDARD NORME AECMA AECMA NORM Comments should be sent within six months after the date of publication to AECMA Technopolis - 1 75, rue Jean-Jacques Rousseau 921 38 Issy-les-Moulineaux Cedex - FRANCE prEN 2435

2、-01 Edition P 1 June 1994 EDITE PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1) 47.36.98.76 UDC : Descriptors : ENGLISH VERSION Aerospace series Paints and varnishes Corrosion resistant chr

3、omated two component cold curing primer Part O1 : Minimum requirements Srie arospatiale Luft- und Raumfahrt Peintures et vernis Anstrichstoffe Peinture primaire anti-corrosion chromate deux composants polymrisant temprature ambiante Partie O1 : Exigences minimales Korrosionsbestndiger Zweikomponente

4、n Grundanstrich, kalthrtend Chromathaltig Teil O1 : Mindestanforderungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Arospatial). It is published on green paper for the needs of AECMA-Members. it has been

5、 technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-

6、identification of the standard. After examination and signature of the AECMA Standard Checking Centre INPSI and formal agreement of the Officiai Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Nota -

7、Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX C 7 Chairman Mr Bottrell aecrna 1994 CEN PREN*2435-01 94 m 3404587 0064149 921 = Page 3 prEN 2435-01 : 1994 1 Scope This standard specifies the minimum requirements for a two

8、-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 IS0 3270. T

9、he 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. 2 Normative references This European Standard incorporates by dated or

10、 undated reference, provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only

11、when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 1518 IS0 2409 IS0 3270 Paints and varnishes - Scratch test Paints and varnishes - Cross-cut test Paints varnishes and their raw materials - Temperatures and humidit

12、ies for conditioning and testing Aerospace series - Fluids for assessment of non-metallic materials Aerospace series - Paints and varnishes - Nature and method for preparation of surface of test specimens in aluminium alloys 1) Aerospace series - Paints and varnishes - Technical specification EN 237

13、9 EN 3837 EN 3840 3 Definitions None applicable. 4 Classification The primers are classified according to the nature of the most typical chemical reaction that occurs between the two components : Type A : chromated epoxy - (reaction between an epoxy resin and an activator with amino functional Type

14、B : polyurethane - (reaction between an hydroxyl functional resin and a polyisocyanate activator). groups). 1) In preparation at the date of publication of this standard Previous page is blank CEN PRENr2435-01 94 = 3404589 0064350 643 Description block PRIMER Page 4 prEN 2435-01 : 1994 Identity bloc

15、k EN2435-01 A 5 Required characteristics Requirements concerning delivery, qualification, batch acceptance, sampling, test methods and other requirements specific to the material are defined in EN 3840. 5.1 Composition The primer consists of : - a base containing one or several corrosion inhibitors

16、associated, or not, with pigments and fillers dispersed in a mixture of resins and solvents ; - an activator solution ; and, if need be, a thinner. These components shall be mixed in simple whole number proportions, by volume or by weight, in accordance with the manufacturers instructions. 5.2 Requi

17、red characteristics 5.2.1 General The required characteristics are listed in the tables in annex A in accordance with the technical specification EN 3840. Unless otherwise specified, these characteristics are obtained for a primer paint applied with a dry film thickness of (20 f 5) ,um and dried at

18、(23 f 2) OC/(50 f 5) % HR for (1 70+ :) h before testing. 5.2.2 Qualification tests For qualification, all tests mentioned, in the tables in annex A, shall be carried out. 5.2.3 Acceptance tests For batch acceptance, only the tests marked (*), in the tables in annex A, need to be carried out. CEN PR

19、EN*2435-01 74 = 3404589 0064353 58T Units Base Activator Thinner Characteristics Test according to EN 3840 Units Requirements 8“ 9“ Flow time S * 10% Viscosity high shear rate Pa.s base + activator 2)l 3) IO* 20 * reference reference value 2) OC I value 2) value 2) 1) The deviation specified is as c

20、ompared to the reference value (see note 2) 2) The reference value is as established during qualification Table A.2 : Tests on liquid paint Sedimentation rating 5* I 30 base + activator + thinner I m1/4 h I reference value I g/l I base + activator + thinner 2) 49 I Volatile organic content (vc) I I

21、I 1) The deviation specified is as compared to the reference value (see note 2) 2) The reference value is as established during qualification 3) Test 8 shall be used for non-thixotropic paints and test 9 for thixotropic paints Table A.3 : Tests on wet film Test pieces according to EN 3837 Units Requ

22、irements Metal I Treatment Surface dry time e-+- Drying time - print free Procedure A2 I A 60 4 using a mass of 1000 g min h Procedure A2 I A 23 * I Through-dry time h 16 using a mass of 1500 g Procedure A2 1 A CEN PREN*2435-OL 94 W 3404589 00643.52 416 Test Temp OC according Characteristics 1% HR t

23、o EN 3840 /time (hl Requirements Page 6 prEN 2435-01 : 1994 Test pieces according to EN 3837 Metal Treatment Table A.4 : Tests on dry film 24 * Adhesion 231501- Classification I 1 Procedure A A2 2 1500 g metal not exposed I A2 I Procidure 29 * 1 Scratch resistance 1 231501- I Resistance to fluids 34

24、 35 * Water behaviour Resistance to fluids using tri-N-butyl phosphate (EN 2379 Group 2) 2 31-13 36 701-124 - Cross-hatch (IS0 2409) Classification I 1 - Scratch (IS0 1518) 2 1200 g metal not exposed - No blistering nor detachment (1 O x mag) - Scratch (IS0 151 8) L 1200 g metal not exposed - No blistering nor detachment (1 O x mag) A2 A2 Procedure A Procedure A Environment Corrosion tests 42 Resistance to neutral salt spray 351-11 O00 - No corrosion more than 2 rnm from the scratch - No blistering nor detachment

展开阅读全文
相关资源
  • ASD-STAN PREN 4022-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead Welded (Edition P1)《航空航天系列 钛合金制830管接头 90焊接穿壁弯头 第P1版[替代 ASD-STAN.pdfASD-STAN PREN 4022-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead Welded (Edition P1)《航空航天系列 钛合金制830管接头 90焊接穿壁弯头 第P1版[替代 ASD-STAN.pdf
  • ASD-STAN PREN 4021-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead (Edition P1)《航空航天系列 钛合金制830管接头 90穿壁弯头 第P1版[替代 ASD-STAN PREN 325.pdfASD-STAN PREN 4021-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead (Edition P1)《航空航天系列 钛合金制830管接头 90穿壁弯头 第P1版[替代 ASD-STAN PREN 325.pdf
  • ASD-STAN PREN 4018-2007 Aerospace series Pipe coupling 8 degree 30 in titanium alloy Elbows 90 degree with thrust wire nut (Edition P2)《航空航天系列 钛合金制830管接头 旋转螺母、带止推金属丝帽的90弯头 第P2版.pdfASD-STAN PREN 4018-2007 Aerospace series Pipe coupling 8 degree 30 in titanium alloy Elbows 90 degree with thrust wire nut (Edition P2)《航空航天系列 钛合金制830管接头 旋转螺母、带止推金属丝帽的90弯头 第P2版.pdf
  • ASD-STAN PREN 3256-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 45 Degree Swivel Nut Welded (Edition P 2 )《航空航天系列 钛合金制830管接头 旋转螺母、焊接式45弯头 第P2版[替代为 AS.pdfASD-STAN PREN 3256-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 45 Degree Swivel Nut Welded (Edition P 2 )《航空航天系列 钛合金制830管接头 旋转螺母、焊接式45弯头 第P2版[替代为 AS.pdf
  • ASD-STAN PREN 3254-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead Welded (Edition P 2)《航空航天系列 钛合金制830管接头 焊接式穿壁90弯头 第P2版[替代为 ASD-STAN.pdfASD-STAN PREN 3254-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead Welded (Edition P 2)《航空航天系列 钛合金制830管接头 焊接式穿壁90弯头 第P2版[替代为 ASD-STAN.pdf
  • ASD-STAN PREN 3253-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead (Edition P 2 )《航空航天系列 钛合金制830管接头 穿壁90弯头 第P2版[替代为 ASD-STAN PREN 402.pdfASD-STAN PREN 3253-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead (Edition P 2 )《航空航天系列 钛合金制830管接头 穿壁90弯头 第P2版[替代为 ASD-STAN PREN 402.pdf
  • ASD-STAN TR AMS2750-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdfASD-STAN TR AMS2750-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdf
  • ASD-STAN TR AMS2750 FRENCH-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdfASD-STAN TR AMS2750 FRENCH-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdf
  • ASD-STAN TR 9536-2008 Aerospace series Declarable Substances Recommended Practice《航空航天系列 需申报物质 建议做法》.pdfASD-STAN TR 9536-2008 Aerospace series Declarable Substances Recommended Practice《航空航天系列 需申报物质 建议做法》.pdf
  • ASD-STAN TR 9535-2008 Aerospace series Substance declaration (Edition 1)《航空航天系列 物质声明 第1版》.pdfASD-STAN TR 9535-2008 Aerospace series Substance declaration (Edition 1)《航空航天系列 物质声明 第1版》.pdf
  • 猜你喜欢
    相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ASD

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1