AECMA 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.油漆和清漆 .pdf

《AECMA 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.油漆和清漆 .pdf》由会员分享，可在线阅读，更多相关《AECMA 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.油漆和清漆 .pdf（5页珍藏版）》请在麦多课文档分享上搜索。

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 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reprod

8、uction or networking permitted without license from IHS-,-,-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-component, chromated epoxy or polyurethane, corrosion resistant primer which can be used with or witho

9、ut 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. The ability of the material to be used for a specific application (e.g. alternative substrate, specific

10、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 undated reference, provisions from other publications. These normative references are cited at the app

11、ropriate 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 when incorporated in it by amendment or revision. For undated references the latest edition of the publ

12、ication 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 humidities for conditioning and testing Aerospace series - Fluids for assessment of non-metallic materials Aer

13、ospace 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 2379 EN 3837 EN 3840 3 Definitions None applicable. 4 Classification The primers are classified according

14、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 B : polyurethane - (reaction between an hydroxyl functional resin and a polyisocyanate activator). grou

15、ps). 1) In preparation at the date of publication of this standard Previous page is blank Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CEN PRENr2435

16、-01 94 = 3404589 0064350 643 Description block PRIMER Page 4 prEN 2435-01 : 1994 Identity block 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

17、 Composition The primer consists of : - a base containing one or several corrosion inhibitors 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 pro

18、portions, by volume or by weight, in accordance with the manufacturers instructions. 5.2 Required 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 a

19、re obtained for a primer paint applied with a dry film thickness of (20 f 5) ,um and dried at (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 a

20、cceptance, only the tests marked (*), in the tables in annex A, need to be carried out. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CEN PREN*2435-0

21、1 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 compared t

22、o 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 I 1) The

23、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 Requirements

24、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 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under li

25、cense with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CEN PREN*2435-OL 94 W 3404589 00643.52 416 Test Temp OC according Characteristics 1% HR to EN 3840 /time (hl Requirements Page 6 prEN 2435-01 : 1994 Test pieces according to EN 3837 Metal Treatment Tab

26、le 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 35 * Water behaviour Resistance to fluids using tri-N-butyl phosphate (EN 2379 Group 2) 2 31-13 36 701-124 - Cr

27、oss-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 ne

28、utral salt spray 351-11 O00 - No corrosion more than 2 rnm from the scratch - No blistering nor detachment Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-