EN 4133-2009 en Aerospace series - Bolts normal hexagonal head coarse tolerance normal shank long thread in titanium alloy aluminium IVD coated - Classification 1 100 MPa (at ambie.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 CThi
2、s 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 CommentsBS EN 4133:2009National forewordThis British Standard is the UK implementation of EN 4133:2009.The U
3、K 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 secretary.This publication does not purport to include all the necessary provisionsof a cont
4、ract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.BS EN 4133:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4133 April 2009 ICS 49.030.20 English Version Aerospace series - Bolts, normal hexagonal head, c
5、oarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated - Classification: 1 100 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 1
6、00 MPa ( temprature ambiante)/425 C Luft- und Raumfahrt - Sechskantschrauben, langes Gewinde, aus Titanlegierung, 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/CENEL
7、EC 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
8、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. C
9、EN members are the national standards bodies of Austria, Belgium, Bulgaria, 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, S
10、weden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION 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 Member
11、s. Ref. No. EN 4133:2009: EBS 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 BS EN 4133:2009EN 4133:2009 (E) 3 Foreword This document (EN 4133:2009) has been prepared b
12、y 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
13、 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, and conflicting national standards shall be withdrawn at the latest by October 2009. Attention
14、 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. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the
15、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, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia,
16、 Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4133:2009EN 4133:2009 (E) 4 1 Scope This 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
17、 C 2)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 2424, Aerospace se
18、ries Marking of aerospace products 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 mana
19、gement systems Qualification procedure for aerospace standard parts 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 7913, Aerospace Bolts and screws, metric Tolerances of form and position
20、ISO 9152, Aerospace Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa Procurement specification 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 te
21、mperature that the bolt can withstand without continuous change in its original characterictics, after return 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: Depa
22、rtment of Defense (DOD), the Pentagon, Washington, D.C. 20301, USA. BS 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 f
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