BS EN 2133-2010 Aerospace series Cadmium plating of steels with specified tensile strength 1450 MPa copper copper alloys and nickel alloys《航空航天系列 规定抗拉强度小于或等于1450 MPa 材质为铜 铜合金及镍合金的钢.pdf
《BS EN 2133-2010 Aerospace series Cadmium plating of steels with specified tensile strength 1450 MPa copper copper alloys and nickel alloys《航空航天系列 规定抗拉强度小于或等于1450 MPa 材质为铜 铜合金及镍合金的钢.pdf》由会员分享,可在线阅读,更多相关《BS EN 2133-2010 Aerospace series Cadmium plating of steels with specified tensile strength 1450 MPa copper copper alloys and nickel alloys《航空航天系列 规定抗拉强度小于或等于1450 MPa 材质为铜 铜合金及镍合金的钢.pdf(14页珍藏版)》请在麦多课文档分享上搜索。
1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 2133:2010Aerospace series Cadmium plating of steels with specified tensile strength null 1 450 MPa, copper, copper alloys and nickel alloysLicensed Copy: Wang Bin, ISO/EXCH
2、ANGE CHINA STANDARDS, 26/05/2011 08:49, Uncontrolled Copy, (c) BSIBS EN 2133:2010 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 2133:2010. Itsupersedes BS EN 2133:1998, which is withdrawn.The UK participation in its preparation was entrusted to TechnicalCommit
3、tee ACE/65/-/4, Surface Finish and Protective Treatments forAerospace Purposes.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correc
4、tapplication. BSI 2011 ISBN 978 0 580 71361 3 ICS 49.040 Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 28 February 2011. Amendments issued since publicationDate
5、Text affectedLicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 26/05/2011 08:49, Uncontrolled Copy, (c) BSIBS EN 2133:2010EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2133 October 2010 ICS 49.040 Supersedes EN 2133:1997English Version Aerospace series - Cadmium plating of steels with sp
6、ecified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys Srie arospatiale - Cadmiage lectrolytique des aciers de rsistance 1 450 MPa, du cuivre, des alliages de cuivre et des alliages de nickel Luft- und Raumfahrt - Kadmieren von Sthlen mit einer Zugfestigkeit 1 450 MPa, von Kupfe
7、r, von Kupferlegierungen und von Nickellegierungen This European Standard was approved by CEN on 30 July 2010. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alte
8、ration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in any other language made by tra
9、nslation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Fra
10、nce, 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 STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE F
11、R NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2010 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2133:2010: ELicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 26/05/2011 08:49, Uncontrolled Copy, (c) BSIBS E
12、N 2133:2010EN 2133:2010 (E) 2 Contents Page Foreword 31 Scope 42 Normative references 43 Purpose of process .44 Limitations of process use .55 Terms and definitions .56 Coating thickness 57 Symbols 58 Information for the processor 59 Condition of parts prior to the treatment 610 Process schedule 611
13、 Post-treatment 712 Removal of the plating 713 Required characteristics .714 Test methods 815 Quality assurance 916 Designation . 10Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 26/05/2011 08:49, Uncontrolled Copy, (c) BSIBS EN 2133:2010EN 2133:2010 (E) 3 Foreword This document (EN 2133:201
14、0) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of t
15、he member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by April 2011, and conflicting national standards shall be withdrawn at the latest by Apr
16、il 2011. 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 shall not be held responsible for identifying any or all such patent rights. This document supersedes EN 2133:1997. According to the CEN/CENELEC Internal
17、Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg
18、, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 26/05/2011 08:49, Uncontrolled Copy, (c) BSIBS EN 2133:2010EN 2133:2010 (E) 4 1 Scope This European standard specifie
19、s the electrolytic cadmium plating of parts in steel of tensile strength Rm(max.) 1 450 MPa, copper, copper alloys and nickel alloys, whose temperature in service does not exceed 235 C. 2 Normative references The following referenced documents are indispensable for the application of this document.
20、For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2828, Aerospace series Adhesion test for metallic coatings by burnishing EN 2831, Aerospace series Hydrogen embrittlement of steels Test
21、by slow bending EN 2832, Aerospace series Hydrogen embrittlement of steels Notched specimen test EN 9100, Quality management systems Requirements for Aviation, Space and Defense Organizations EN ISO 1463, Metallic and oxide coatings Measurement of coating thickness Microscopical method (ISO 1463:200
22、3) EN ISO 2082, Metallic and other inorganic coatings Electroplated coatings of cadmium with supplementary treatments on iron or steel (ISO 2082:2008) EN ISO 2177, Metallic coatings Measurement of coating thickness Coulometric method by anodic dissolution (ISO 2177:2003) EN ISO 2178, Non-magnetic co
23、atings on magnetic substrates Measurement of coating thickness Magnetic method (ISO 2178:1982) EN ISO 2819, Metallic coatings on metallic substrates Electrodeposited and chemically deposited coatings Review of methods available for testing adhesion (ISO 2819:1980) EN ISO 3497, Metallic coatings Meas
24、urement of coating thickness X-ray spectrometric methods (ISO 3497:2000) EN ISO 9227, Corrosion tests in artificial atmospheres Salt spray tests (ISO 9227:2006) ISO 2859-1, Sampling procedures for inspection by attributes Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-
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