BS EN 2436-003-2006 Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - High corrosion and fluid resistance《航空航天系列 涂料和清漆 .pdf
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1、 g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58component cold curing primer Part 003: High corrosion and fluid resistanceThe European Standard EN
2、2436-003:2006 has the status of a British StandardICS 49.040Paints and varnishes Corrosion resistant chromate-free two BRITISH STANDARD AEROSPACE SERIESBS EN2436-003:2006BS EN 2436-003:2006This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 Ju
3、ly 2006 BSI 2006ISBN 0 580 48874 8Cross-referencesThe British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility o
4、f the BSI Electronic Catalogue or of British Standards Online.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations.Summa
5、ry of pagesThis document comprises a front cover, an inside front cover, the EN title page, pages 2 to 10, an inside back cover and a back cover.The BSI copyright notice displayed in this document indicates when the document was last issued.Amendments issued since publicationAmd. No. Date Comments p
6、resent to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep UK interests informed; monitor related international and European developments and promulgate them in the UK.A list of organizations represented on this subcommittee can
7、be obtained on request to its secretary.National forewordThis British Standard is the official English language version of EN 2436-003:2006. The UK participation in its preparation was entrusted by Technical Committee ACE/65, Non-metallic materials for aerospace purposes (excluding textiles), to Sub
8、committee ACE/65/-/3, Paints, which has the responsibility to: aid enquirers to understand the text;EUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 2436-003June 2006ICS 49.040English VersionAerospace series - Paints and varnishes - Corrosion resistantchromate-free two component cold curing primer
9、- Part 003:High corrosion and fluid resistanceSrie arospatiale - Peintures et vernis - Peinture primaireanti-corrosion sans chromate deux composantspolymrisant temprature ambiante - Partie 003 : Hautersistance la corrosion et aux fluidesLuft- und Raumfahrt - Anstrichstoffe -Korrosionsbestndiger Zwei
10、komponenten-Grundanstrich,kalthrtend chromatfrei - Teil 003: Hohe Bestndigkeitgegen Korrosion und FlssigkeitenThis European Standard was approved by CEN on 9 March 2006.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanSt
11、andard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the Central Secretariat or to any CEN member.This European Standard exists in three official versions (English, French,
12、 German). A version in any other language made by translationunder the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, D
13、enmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania,Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISAT
14、IONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 2006 CEN All rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 2436-003:2006: E2 Contents Page Foreword3 0 Introduction4 1 Scope 4 2 Normative references 4
15、 3 Definitions 5 4 Classification5 5 Batch release and qualification testing.5 EN 2436-003:20063 Foreword This European Standard (EN 2436-003:2006) has been prepared by the AeroSpace and Defense Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in a
16、ccordance with the rules of this Association, this Standard has re-ceived the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publicati
17、on of an identical text or by endorsement, at the latest by December 2006, and conflicting national standards shall be withdrawn at the latest by December 2006. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC sh
18、all not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Den-mark, Estonia, Fi
19、nland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxem-bourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzer-land and the United Kingdom. EN 2436-003:20064 0 Introduction This standard is part of a series of EN no
20、n-metallic materials standards for aerospace applications. The general organisation of this series is described in EN 4385. This standard is a level 3 document as defined in EN 4385. Definition of subcase numbering in Tables 2 to 5 is given in TR 7000-9. 1 Scope This standard specifies the requireme
21、nts 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 accord
22、ance 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. 2 Normative refere
23、nces The following referenced documents are indispensable for the application of this document. For dated refer-ences, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2334, Aerospace series Chromic-sulphuric
24、 acid pickle of aluminium and aluminium alloys EN 2379, Aerospace series Fluids for assessment of non-metallic materials1)EN 3837, Aerospace series Paints and varnishes Nature and method for surface preparation of test pieces in aluminium alloys1)EN 2434-003, Aerospace series Paints and varnishes Tw
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