BS EN 3301-2007 Aerospace series - Bolts T-head close tolerance medium thread length in heat resisting steel FE-PM1708 (FV535) uncoated - Classification 1000 MPa 550 C《航空航天系列 未涂敷FE.pdf
《BS EN 3301-2007 Aerospace series - Bolts T-head close tolerance medium thread length in heat resisting steel FE-PM1708 (FV535) uncoated - Classification 1000 MPa 550 C《航空航天系列 未涂敷FE.pdf》由会员分享,可在线阅读,更多相关《BS EN 3301-2007 Aerospace series - Bolts T-head close tolerance medium thread length in heat resisting steel FE-PM1708 (FV535) uncoated - Classification 1000 MPa 550 C《航空航天系列 未涂敷FE.pdf(12页珍藏版)》请在麦多课文档分享上搜索。
1、Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 17/04/2008 07:59, Uncontrolled Copy, (c) BSIg49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58t
2、hread length in heat resisting steel FE-PM1708 (FV535), uncoated Classification: 1 000 MPa/550 CICS 49.030.20Aerospace series Bolts, T-head, close tolerance medium BRITISH STANDARDBS EN 3301:2007BS EN 3301:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 17/04/2008 07:59, Uncontrolled Copy
3、, (c) BSIThis British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 January 2008 BSI 2008ISBN 978 0 580 60320 4Amendments/corrigenda issued since publicationDate CommentsCompliance with a British Standard cannot confer immunity from legal obligations
4、.National forewordThis British Standard is the UK implementation of EN 3301:2007.The UK participation 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 secr
5、etary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3301 December 2007 ICS 49.030.20 English Version Aerospace series - Bolts, T-head, close tolerance med
6、ium thread length in heat resisting steel FE-PM1708 (FV535), uncoated - Classification: 1 000 MPa/550 C Srie arospatiale - Vis de prcision tte anti-rotation T filetage moyen en acier rsistant chaud FE-PM1708 (FV535), non revtu - Classification : 1 000 MPa/550 C Luft- und Raumfahrt - T-Kopf-Paschaube
7、n mittlere Gewindelnge, aus hochwarmfestem Stahl FE-PM1708 (FV535), blank - Klasse: 1 000 MPa/550 C This European Standard was approved by CEN on 5 November 2007. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standar
8、d 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 CEN member. This European Standard exists in three official versions (English, French,
9、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. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Cze
10、ch 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 United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUR
11、OPEN DE 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 3301:2007: ELicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 17/
12、04/2008 07:59, Uncontrolled 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 3301:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 17/04/2008 07:59, Uncontrolled Copy, (c) BSI
13、3 Foreword This document (EN 3301:2007) 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 Associ
14、ations 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 June 2008, and conflicting national standards sha
15、ll be withdrawn at the latest by June 2008. 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 Regu
16、lations, 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, Latvia, Lithuania, Luxembourg, Malta, Neth
17、erlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 3301:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 17/04/2008 07:59, Uncontrolled Copy, (c) BSI4 1 Scope This standard specifies the dimensions of uncoated T-head bolts,
18、 close tolerance, with MJ-thread, medium thread length, in heat resisting steel FE-PM1708 for aerospace applications. Maximum test temperature of the parts is 550 C. These bolts are to be used in aerospace fastening systems mainly stressed in shearing force. 2 Normative references The following refe
19、renced 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 Part 1: Rolled extern
20、al 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. EN 2424, Aerospace series Marking of aerospace products. EN 2493 1), Heat resisting steel FE-PM38 1 000 MPa Rm 1 140 MPa Bars Aerospace series. 2)E
21、N 3302, Aerospace series Bolts in heat resisting steel FE-PM1708 (FV535) Classification: 1 000 MPa / 550 C Technical specification. 3)EN 4244, Aerospace series Heat resisting alloy FE-PM1708 Vacuum arc remelted Hardened and tempered Bar a or D 200 mm 1 000 MPa Rm 1 140 MPa. 3)EN 4245, Aerospace seri
22、es Heat resisting alloy FE-PM1708 Vacuum arc remelted As forged Forging stock De 300 mm. 3)3 Required characteristics 3.1 Configuration - Dimensions - Tolerances Configuration shall be in accordance with the Figure 1. Dimensions, tolerances and masses shall conform to the Figure 1 and the Tables 1 a
23、nd 2. Details of form, not stated are at the manufacturers option. 3.2 Material Heat resisting steel FE-PM38 according to EN 2493. 3.3 Surface treatment None. 1) Inactive for new design, see EN 4244 and EN 4245. 2) Published as ASD Standard at the date of publication of this standard. 3) Published a
24、s ASD Prestandard at the date of publication of this standard. EN 3301:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 17/04/2008 07:59, Uncontrolled Copy, (c) BSI5 3.4 Thread surface See Figure 1. Key 1 Rolled 2 Thread pitch- 3 Thread major diameter: max.: actual shank diameter minus 0,0
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