BS EN 4133-2009 Aerospace series - Bolts normal hexagonal head coarse tolerance normal shank long thread in titanium alloy aluminium IVD coated - Classification 1100 MPa (at ambien.pdf
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1、BS EN 4133:2009ICS 49.030.20,NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bolts, normalhexagonal head, coarsetolerance normalshank, long thread,in titanium alloy,aluminium IVD coated Classification: 1100 MPa (at ambienttemperature) / 425 CLic
2、ensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 27/08/2009 02:42, Uncontrolled Copy, (c) BSIThis British Standardwas published under theauthority of the StandardsPolicy and StrategyCommittee on 31 May 2009 BSI 2009ISBN 978 0 580 65952 2Amendments/corrigenda issued since publicationDate CommentsB
3、S EN 4133:2009National forewordThis British Standard is the UK implementation of EN 4133:2009.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
4、to its secretary.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, 27/08/2009
5、 02:42, Uncontrolled Copy, (c) BSIBS EN 4133:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4133 April 2009 ICS 49.030.20 English Version Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated - Classification: 1
6、 100 MPa (at ambient temperature) / 425 C Srie arospatiale - Vis tte hexagonale normale, tige normale tolrance large, filetage long, en alliage de titane, revtues aluminium IVD - Classification: 1 100 MPa ( temprature ambiante)/425 C Luft- und Raumfahrt - Sechskantschrauben, langes Gewinde, aus Tita
7、nlegierung, Aluminium IVD beschichtet - Klasse: 1 100 MPa (bei Raumtemperatur) / 425 C This European Standard was approved by CEN on 12 March 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
8、 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 vers
9、ion 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, Cyprus, Czech Republic, De
10、nmark, 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 COMIT EUROPEN DE NORMALI
11、SATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: 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 4133:2009: ELicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 27/08/2009 02:42, Un
12、controlled Copy, (c) BSIBS EN 4133:2009EN 4133:2009 (E) 2 Contents Page Foreword 3 1 Scope 4 2 Normative references 4 3 Required characteristics .5 4 Designation 8 5 Marking .8 6 Technical specification .8 Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 27/08/2009 02:42, Uncontrolled Copy, (c
13、) BSIBS EN 4133:2009EN 4133:2009 (E) 3 Foreword This document (EN 4133:2009) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has receive
14、d 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 October 2009
15、, and conflicting national standards shall be withdrawn at the latest by October 2009. 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.
16、 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, France, Germany, Greece, Hungary, Iceland, Ireland, Italy,
17、 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, 27/08/2009 02:42, Uncontrolled Copy, (c) BSIBS EN 4133:2009EN 4133:2009 (E) 4 1 Scope T
18、his standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated. Classification: 1 100 MPa 1) / 425 C 2)2 Normative references The following referenced documents are indispensable for the application of t
19、his document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products EN 9100, Aerospace series Quality management systems Requirements (bas
20、ed 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 Qualification procedure for aerospace standard parts ISO 3353-1, Aerospace Lead and runout
21、 threads Part 1: Rolled external threads ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts ISO 7913, Aerospace Bolts and screws, metric Tolerances of form and position ISO 9152, Aerospace Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa Procurement spec
22、ification TR 3775, Aerospace series Bolts and pins Materials 3) MIL-DTL-83488D, Coating, aluminium, high purity 4)1) Minimum tensile strength of the material at ambient temperature. 2) Maximum temperature that the bolt can withstand without continuous change in its original characterictics, after re
23、turn to ambient temperature. The maximum temperature is determined by the surface treatment 3) Published as ASD Technical Report at the date of publication of this standard. 4) Published by: Department of Defense (DOD), the Pentagon, Washington, D.C. 20301, USA. Licensed Copy: Wang Bin, ISO/EXCHANGE
24、 CHINA STANDARDS, 27/08/2009 02:42, Uncontrolled Copy, (c) BSIBS EN 4133:2009EN 4133:2009 (E) 5 3 Required characteristics 3.1 Configuration Dimensions Masses See Figure 1 and Table 1. Dimensions and tolerances are expressed in millimetres and apply after surface treatment. 3.2 Tolerances of form an
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