EN 3301-2007 en Aerospace series - Bolts T-head close tolerance medium thread length in heat resisting steel FE-PM1708 (FV535) uncoated - Classification 1 000 MPa 550 《航空航天系列 非涂覆FE.pdf
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1、BRITISH STANDARDBS EN 3301:2007Aerospace series Bolts, T-head, close tolerance medium thread length in heat resisting steel FE-PM1708 (FV535), uncoated Classification: 1 000 MPa/550 CICS 49.030.20g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g
2、38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 3301:2007This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 January 2008 BSI 2008ISBN 978 0 580 60320 4National forewordThis British Standar
3、d 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 secretary.This publication does not purpor
4、t to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.Amendments/corrigenda issued since publicationDate CommentsEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN
5、3301 December 2007 ICS 49.030.20 English Version Aerospace series - Bolts, T-head, close tolerance medium 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
6、FE-PM1708 (FV535), non revtu - Classification : 1 000 MPa/550 C Luft- und Raumfahrt - T-Kopf-Paschauben 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 wit
7、h 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 obtained on application to the CEN Management Ce
8、ntre 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 CEN Management Centre has the same status as the offic
9、ial versions. CEN 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, Slo
10、venia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN 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 CE
11、N national Members. Ref. No. EN 3301:2007: E2 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 3301:20073 Foreword This document (EN 3301:2007) has been prepared by the Aerospace and Defence Industrie
12、s 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 ASD, prior to its presentation to CE
13、N. 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 shall be withdrawn at the latest by June 2008. Attention is drawn to the possibility that some of t
14、he 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 following countries are bound to implement
15、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, Slovenia, Spain, Sweden, Switzerland and t
16、he United Kingdom. EN 3301:20074 1 Scope This standard specifies the dimensions of uncoated T-head bolts, 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
17、 aerospace fastening systems mainly stressed in shearing force. 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 documen
18、t (including any amendments) applies. 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. EN 2424, Aerospace series Marking of aeros
19、pace products. EN 2493 1), Heat resisting steel FE-PM38 1 000 MPa Rm 1 140 MPa Bars Aerospace series. 2)EN 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 Vacu
20、um arc remelted Hardened and tempered Bar a or D 200 mm 1 000 MPa Rm 1 140 MPa. 3)EN 4245, Aerospace series 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 accorda
21、nce with the Figure 1. Dimensions, tolerances and masses shall conform to the Figure 1 and the Tables 1 and 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 4
22、244 and EN 4245. 2) Published as ASD Standard at the date of publication of this standard. 3) Published as ASD Prestandard at the date of publication of this standard. EN 3301:20075 3.4 Thread surface See Figure 1. Key 1 Rolled 2 Thread pitch- 3 Thread major diameter: max.: actual shank diameter min
23、us 0,025 mm min.: defined by 6h tolerance 4 R typical0,40,95 Identity marking 6 Lead thread ISO 3353-1 7 Thread runout ISO 3353-1 8 43 to 47 aTotal straightness with reference to nominal length N. bWhen the length of the shank is less than one time the nominal value of the shank diameter, D, the run
24、out is measured at a distance equal to half the actual shank length. cFor boIts having a shank length less than one time the nominal value of the shank diameter, D, the pitch diameter axis shall be used as datum. Figure 1 Configuration Table 1 Dimensions Dimensions in millimetres C D E K Q R S X Y C
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- EN33012007ENAEROSPACESERIESBOLTSTHEADCLOSETOLERANCEMEDIUMTHREADLENGTHINHEATRESISTINGSTEELFEPM1708FV535UNCOATEDCLASSIFICATION1000MPA550

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