BS EN 3912-2007 Aerospace series - Bolts pan head six lobe recess relieved shank long thread in heat resisting steel FE-PA2601 (FE-PA92HT A286) silver plated - Classification 1100 .pdf
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1、BRITISH STANDARDBS EN 3912:2007Aerospace series Bolts, pan head, six lobe recess, relieved shank, long thread, in heat resisting steel FE-PA2601 (FE-PA92HT, A286), silver plated Classification: 1 100 MPa (at ambient temperature) / 650 CThe European Standard EN 3912:2007 has the status of a British S
2、tandardICS 49.030.20g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58Licensed Copy: Wang Bin, na, Wed Aug 15 07:53:04 GMT+00:00 2007, Uncontrolled Co
3、py, (c) BSIBS EN 3912:2007This British Standard was published under the authority of the Standards Policy and Strategy Committee on 30 April 2007 BSI 2007ISBN 978 0 580 50642 0National forewordThis British Standard was published by BSI. It is the UK implementation of EN 3912:2007.The UK participatio
4、n in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented 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
5、 are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.Amendments issued since publicationAmd. No. Date CommentsLicensed Copy: Wang Bin, na, Wed Aug 15 07:53:04 GMT+00:00 2007, Uncontrolled Copy, (c) BSIEUROPEAN STANDARD NORME EU
6、ROPENNE EUROPISCHE NORM EN 3912 April 2007 ICS 49.030.20 English Version Aerospace series - Bolts, pan head, six lobe recess, relieved shank, long thread, in heat resisting steel FE-PA2601 (FE-PA92HT, A286), silver plated - Classification: 1 100 MPa (at ambient temperature) / 650 C Srie arospatiale
7、- Vis tte cylindrique, empreinte six lobes, ft dgag, filetage long, en acier rsistant chaud FE-PA2601 (FE-PA92HT, A286), argentes - Classification : 1 100 MPa ( temprature ambiante) / 650 C Luft- und Raumfahrt - Flachkopfschrauben, Sechs-Bogenzahn, Innenantrieb, langes Gewinde, aus hochwarmfestem St
8、ahl FE-PA2601 (FE-PA92HT, A286), versilbert - Klasse: 1 100 MPa (bei Raumtemperatur) / 650 C This European Standard was approved by CEN on 28 August 2006. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the st
9、atus 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).
10、 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, Cyprus, Czech Repub
11、lic, 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 COMIT EUROPEN DE
12、NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2007 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3912:2007: ELicensed Copy: Wang Bin, na, Wed Aug 15 07:53:04 GMT+00:00 2007, U
13、ncontrolled Copy, (c) BSI2 Contents Page Foreword3 1 Scope 4 2 Normative references 4 3 Required characteristics.4 4 Designation 8 5 Marking .8 6 Technical specification .8 EN 3912:2007Licensed Copy: Wang Bin, na, Wed Aug 15 07:53:04 GMT+00:00 2007, Uncontrolled Copy, (c) BSI3 Foreword This document
14、 (EN 3912:2007) 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
15、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 2007, and conflicting national standards shall be withdrawn at th
16、e latest by October 2007. 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. According to the CEN/CENELEC Internal Regulations, the natio
17、nal 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, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, P
18、oland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 3912:2007Licensed Copy: Wang Bin, na, Wed Aug 15 07:53:04 GMT+00:00 2007, Uncontrolled Copy, (c) BSI4 1 Scope This standard specifies the characteristics of pan head bolts with six lobe recess, reliev
19、ed shank and long thread, in FE-PA2601 (FE-PA92HT), silver plated, for aerospace applications. Classification: 1 100 MPa 1)/ 650 C 2)NOTE Taking account of the recess geometry, the strength class to be used for the seating torque calculation shall not be greater than 900 MPa. 2 Normative references
20、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. ISO 3353-1, Aerospace Lead and runout threads Par
21、t 1: Rolled external threads. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. EN 2399, Heat resisting steel FE-PA92-HT Rm 900 MPa Bars for forged bolts D 25 mm Aerospace series. 3)EN 2424, Aerospace series Marking of aerospace products. EN 2786, Aerospace series Electro
22、lytic silver plating of fasteners. 4)EN 3685, Aerospace series Bolts in heat resisting steel, FE-PA92HT (A286) Classification: 1 100 MPa/650 C Technical specification. 4)EN 3761, Aerospace series Heat resisting alloy FE-PA2601 Softened and cold worked Bar for forged fasteners D 50 mm 1 100 MPa Rm 1
23、300 MPa. 4)EN 3905, Aerospace series Six lobe recesses for bolts Technical specification. 4)EN 3911, Aerospace series Six lobe recess Geometrical definition. 4)3 Required characteristics 3.1 Configuration - Dimensions - Tolerances See Figure 1 and Tables 1 and 2. Dimensions and tolerances are in mil
24、limetres. They apply after silver plating. 1) Minimum tensile strength of the material at ambient temperature. 2) Maximum test temperature of the parts. 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 standa
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