SIST EN 2133:2011
(Main)Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
This standard specifies 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.
Luft und Raumfahrt - Kadmieren von Stählen mit einer Zugfestigkeit ≤ 1 450 MPa, von Kupfer, von Kupferlegierungen und von Nickellegierungen
Diese Norm legt das elektrolytische Kadmieren von Teilen aus Stahl mit einer Zugfestigkeit
Rm (max.) ≤ 1 450 MPa, aus Kupfer, Kupferlegierungen und Nickellegierungen fest, deren Betriebstemperatur
235 °C nicht überschreitet.
Série aérospatiale - Cadmiage électrolytique des aciers de résistance ≤ 1 450 MPa, du cuivre, des alliages de cuivre et des alliages de nickel
La présente norme spécifie le cadmiage électrolytique des pièces en acier de résistance en traction
Rm (max.) £ 1 450 MPa, en cuivre, alliages de cuivre et alliages de nickel, dont la température en service ne
dépasse pas 235 °C.
Aeronavtika - Kadmiranje jekla z določeno natezno trdnostjo ≤ 1450 MPa z bakrom, bakrovimi in nikljevimi zlitinami
Ta standard določa elektrolitsko kadmiranje delov iz jekla natezne trdnosti Rm (max.) < = 1 450 MPa, bakra, bakrovih zlitin in nikljevih zlitin, katerih temperatura pri delovanju ni večja od 235 °C.
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Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.49.040Prevleke in z njimi povezani postopki, ki se uporabljajo v letalski in vesoljski industrijiCoatings and related processes used in aerospace industryICS:Ta slovenski standard je istoveten z:EN 2133:2010SIST EN 2133:2011en01-maj-2011SIST EN 2133:2011SLOVENSKI
STANDARDSIST EN 2133:20011DGRPHãþD
SIST EN 2133:2011
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 2133
October 2010 ICS 49.040 Supersedes EN 2133:1997English Version
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
Série aérospatiale - Cadmiage électrolytique des aciers de résistance ≤ 1 450 MPa, du cuivre, des alliages de cuivre et des alliages de nickel
Luft- und Raumfahrt - Kadmieren von Stählen mit einer Zugfestigkeit ≤ 1 450 MPa, von Kupfer, 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 alteration. 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 translation 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, 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 STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR 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: ESIST EN 2133:2011
EN 2133:2010 (E) 2 Contents Page Foreword .31Scope .42Normative references .43Purpose of process .44Limitations of process use .55Terms and definitions .56Coating thickness .57Symbols .58Information for the processor .59Condition of parts prior to the treatment .610Process schedule .611Post-treatment .712Removal of the plating .713Required characteristics .714Test methods .815Quality assurance .916Designation . 10 SIST EN 2133:2011
EN 2133:2010 (E) 3 Foreword This document (EN 2133:2010) 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 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 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 April 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 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, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. SIST EN 2133:2011
EN 2133:2010 (E) 4 1 Scope This European standard specifies 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. 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 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 1463:2003) 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 coatings 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 — Measurement 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-lot ins
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