BS EN 4132-2009 Aerospace series - Bolts normal hexagonal head coarse tolerance normal shank long thread in alloy steel cadmium plated - Classification 1100 MPa (at ambient tempera.pdf
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1、BS EN 4132:2009ICS 49.030.20NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bolts, normalhexagonal head, coarsetolerance normalshank, long thread, inalloy steel, cadmiumplated Classification:1 100 MPa (at ambienttemperature) / 235 CLicensed Copy
2、: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 01/12/2009 08:00, Uncontrolled Copy, (c) BSIThis British Standardwas published under theauthority of the StandardsPolicy and StrategyCommittee on 31 August2009 BSI 2009ISBN 978 0 580 68867 6Amendments/corrigenda issued since publicationDate CommentsBS EN 413
3、2:2009National forewordThis British Standard is the UK implementation of EN 4132:2009.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can be obtained onrequest to its s
4、ecretary.This publication does not purport to include all the necessary provisionsof a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 01/12/2009 08:00,
5、Uncontrolled Copy, (c) BSIBS EN 4132:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4132 July 2009 ICS 49.030.20 English Version Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambie
6、nt temperature) / 235 C Srie arospatiale - Vis tte hexagonale normale, tige normale tolrance large, filetage long, en acier alli, cadmies - Classification: 1 100 MPa ( temprature ambiante) / 235 C Luft- und Raumfahrt - Sechskantschrauben, langes Gewinde, aus legiertem Stahl, verkadmet - Klasse : 1 1
7、00 MPa (bei Raumtemperatur) / 235 C This European Standard was approved by CEN on 23 April 2009. 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-
8、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
9、 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, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, H
10、ungary, 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 FR NORMUNG Management Ce
11、ntre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4132:2009: ELicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 01/12/2009 08:00, Uncontrolled Copy, (c) BSIBS EN 4132:2009EN 4132:2009
12、 (E) 2 Contents Page Foreword 31 Scope 42 Normative references 43 Required characteristics .53.1 Configuration Dimensions Masses 53.2 Tolerances of form and position 53.3 Materials .53.4 Surface treatment 54 Designation 85 Marking .86 Technical specification .8Licensed Copy: Wang Bin, ISO/EXCHANGE C
13、HINA STANDARDS, 01/12/2009 08:00, Uncontrolled Copy, (c) BSIBS EN 4132:2009EN 4132:2009 (E) 3 Foreword This document (EN 4132:2009) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with t
14、he 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 identica
15、l text or by endorsement, at the latest by January 2010, and conflicting national standards shall be withdrawn at the latest by January 2010. 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 res
16、ponsible 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, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, Fra
17、nce, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 01/12/2009 08:00, Uncontrolled C
18、opy, (c) BSIBS EN 4132:2009EN 4132:2009 (E) 4 1 Scope This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. Classification: 1 100 MPa 1) / 235 C 2)2 Normative references The following referenced docume
19、nts 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 2133, Aerospace series Cadmium plating of steels with specified tensile stren
20、gth 1 450 MPa, copper, copper alloys and nickel alloys. EN 2137, Steel FE-PL75 1 100 MPa Rm 1 250 MPa Bars De 100 mm Aerospace series.3)EN 2424, Aerospace series Marking of aerospace products. EN 3514, Aerospace series Steel FE-PL711 Hardened and tempered 1 100 Rm 1 300 MPa Bar and wire for bolts De
21、 25 mm. 4) EN 9100, Aerospace series Quality management systems Requirements (based on ISO 9001:2000) and Quality systems Model for quality assurance in design, development, production, installation and servicing (based on ISO 9001:1994). EN 9133, Aerospace series Quality management systems Qualific
22、ation procedure for aerospace standard parts. TR 3775, Aerospace series Bolts and pins Materials. 5) ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. ISO 7689, Aerospace Bolts, with MJ threads
23、, made of alloy steel, strength class 1 100 MPa Procurement specification. ISO 7913, Aerospace Bolts and screws, metric Tolerances of form and position. 1) Minimum tensile strength of the material at ambient temperature. 2) Maximum temperature that the bolt can withstand without continuous change in
24、 its original characteristics, after return to ambient temperature. The maximum temperature is determined by the surface treatment. 3) Published as ASD Standard at the date of publication of this standard. 4) Published as ASD Prestandard at the date of publication of this standard. 5) Published as A
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