EN 3687-2010 en Aerospace series - Bolts normal hexagon head relieved shank long thread in heat resisting steel FE-PA2601 (A286) silver plated - Classification 1 100 MPa 650 (Incor.pdf
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1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 3687:2010Aerospace series Bolts,normal hexagon head, relievedshank, long thread, in heatresisting steel FE-PA2601(A286), silver plated Classification: 1 100 MPa/650 CIncorp
2、orating corrigendum December 2011BS EN 3687:2010 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 3687:2010 incorporating corrigendum October 2011.The start and finish of text introduced or altered by corrigendum is indicated in the text by tags. Text altered by
3、CEN corrigendum October 2011 is indicated in the text by . Untagged corrections have been implemented in this document: all references to “heat resisting steel FE-PA92HT” have been changed to “heat resisting steel FE-PA2601”. Further untagged corrections appear in Table 2: duplicated values in row 0
4、44, column 050 (W min. and Mass) have been removed. Values in the 050 column (W min. and Mass) have been moved up by one row as a result.The UK participation in its preparation was entrusted to Tech-nical Committee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented
5、 on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. BSI 2011ISBN 978 0 580 76952 8ICS 49.030.20Compliance with a British Standard cannot confer immun
6、ity from legal obligations.This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 January 2011.Amendments/corrigenda issued since publicationDate Text affected31 December 2011 Implementation of CEN corrigendum October 2011EUROPEAN STANDARD NORME
7、EUROPENNE EUROPISCHE NORM EN 3687 December 2010 ICS 49.030.20 English Version Aerospace series - Bolts, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA2601 (A286), silver plated - Classification: 1 100 MPa/650 C Srie arospatiale - Vis tte hexagonale normale, ft dgag f
8、iletage long, en acier rsistant chaud FE-PA92HT (A286), argentes - Classification: 1 100 MPa/650 C Luft- und Raumfahrt - Sechskantschrauben, Dnnschaft, langes Gewinde, aus hochwarmfesten Stahl FE-PA92HT (A286) versilbert - Klasse: 1 100 MPa/650 C This European Standard was approved by CEN on 15 Augu
9、st 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 obta
10、ined on application to the CEN-CENELEC 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 CE
11、N-CENELEC 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,
12、 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 Centre: Avenue Marnix 17, B-1000 Brussels 2010 CEN All rights of
13、exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3687:2010: EIncorporating corrigendum October 20112 Contents Page Foreword 31 Scope 42 Normative references 43 Required characteristics .43.1 Configuration Dimensions Tolerances 43.2 Surface roughness
14、43.3 Material .43.4 Surface treatment 44 Designation . 115 Marking 116 Technical specification 11BS EN 3687:2010 EN 3687:2010 (E)3 Foreword This document (EN 3687:2010) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and v
15、otes 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,
16、 either by publication of an identical text or by endorsement, at the latest by June 2011, and conflicting national standards shall be withdrawn at the latest by June 2011. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/o
17、r 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 following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech
18、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. BS EN 3687:2010 EN 3687:2010 (E)4 1 Scope This
19、standard specifies the characteristics of silver-plated Bolts normal Hexagon Head with relieved shank and long thread, in heat resisting steel FE-PA2601 (A286), tensile strength class 1 100 MPa at room temperature. The maximum test temperature of the material is 650 C. 2 Normative references The fol
20、lowing 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 series Marking of aerospace products
21、EN 2786, Aerospace series Electrolytic silver plating of fasteners EN 3685, Aerospace series Bolts in heat resisting steel FE-PA2601 (A286) Classification: 1 100 MPa/650 C Technical specification EN 3761 , Aerospace series Heat resisting alloy FE-PA2601, softened and cold worked; bar for forged fast
22、eners D 50 mm, 1 100 MPa Rm 1 300 MPa ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads ISO 5855-1, Aerospace MJ threads Part 1: General requirements ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts 3 Required characteristics 3.1 Configuration
23、Dimensions Tolerances The configuration shall be in accordance with the figure. Dimensions and tolerances shall conform with the values shown in the figure and in Tables 1 and 2 after silver plating. 3.2 Surface roughness See figure. The specified values are applicable before silver plating. 3.3 Mat
24、erial Heat resisting steel FE-PA2601 to EN 3761. 3.4 Surface treatment Silver coat all over to EN 2786 Category A, coating thickness 3 m to 6 m on the thread flanks measured at the pitch diameter. BS EN 3687:2010 EN 3687:2010 (E)5 Dimensions in millimetres Key 1 thread 2 marking arolled bin accordan
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