EN 3294-2008 en Aerospace series - Bolts T-head close tolerance in heat resisting nickel base alloy NI-P101HT (Waspaloy) uncoated for increased height nuts -Classification 1 210 MP.pdf
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1、BRITISH STANDARDBS EN 3294:2008Aerospace series Bolts, T-head, close tolerance, in heat resisting nickel base alloy NI-P101HT (Waspaloy), uncoated for increased height nuts Classification: 1 210 MPa/730 CICS 49.030.20g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54
2、g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 3294:2008This British Standard was published under the authority of the Standards Policy and Strategy Committee on 30 April 2008 BSI 2008ISBN 978 0 580 60517 8National forewordT
3、his British Standard is the UK implementation of EN 3294:2008.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 publicat
4、ion does not purport 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
5、EUROPISCHE NORM EN 3294 April 2008 ICS 49.030.20 English Version Aerospace series - Bolts, T-head, close tolerance, in heat resisting nickel base alloy NI-P101HT (Waspaloy), uncoated for increased height nuts -Classification: 1 210 MPa/730 C Srie arospatiale - Vis de prcision tte anti-rotation T en
6、alliage rsistant chaud base de nickel NI-P101HT (Waspaloy), non revtu pour crou renforc - Classification: 1 210 MPa/730 C Luft- und Raumfahrt - T-Kopf-Passschrauben, aus hochwarmfester Nickelbasislegierung NI-P101HT (Waspaloy), blank fr hohe Muttern - Klasse: 1 210 MPa/730 C This European Standard w
7、as approved by CEN on 3 November 2007. 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
8、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). A version in any other language made by translation under the responsibility of a CEN member into its own language
9、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 Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxemb
10、ourg, 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: rue de Stassart, 36 B-1050 Brussels 2008 CEN All rig
11、hts of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3294:2008: E2 Contents Page 1 Scope 4 2 Normative references 4 3 Required characteristics.4 3.1 Configuration, dimensions, tolerances, masses4 3.2 Material .4 3.3 Surface treatment 4 3.4 Thread
12、surface .4 4 Designation 8 5 Marking .8 6 Technical specification .8 Figures Figure 1 Configuration 5 Tables Table 1 Dimensions. 5 Table 2 Lengths and masses . 6 BS EN 3294:20083 Foreword This document (EN 3294:2008) has been prepared by the Aerospace and Defence Industries Association of Europe - S
13、tandardization (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 CEN. This European Standard s
14、hall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by October 2008, and conflicting national standards shall be withdrawn at the latest by October 2008. Attention is drawn to the possibility that some of the elements of this d
15、ocument 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 this European Standar
16、d: 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 the United Kingdom. BS
17、 EN 3294:20084 1 Scope This standard specifies the dimensions of uncoated T-head bolts, close tolerance, with MJ-thread, thread length for increased height nuts, in heat resistant nickel base alloy NI-P101HT for aerospace applications. Maximum test temperature of the parts is 730 C. These bolts are
18、to be used in 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 refer
19、enced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products1)EN 2582, Aerospace series Bolts in heat resisting nickel base alloy NI-P101HT (Waspaloy) Classification: 1 210 MPa/730 C Technical specification1)EN 2959, Aerospace series Heat resisting alloy
20、 NI-PH1302 (NiCr20Co13Mo4Ti3Al) Solution treated and cold worked Bar for forged fasteners 3 mm D 30 mm1)EN 3220, Aerospace series Heat resisting nickel base alloy (Ni-P101 HT) Cold worked and softened Bar and wire for continuous forging or extrusion for fasteners 3 D 30 mm1)ISO 3353-1, Aerospace Lea
21、d 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, dimensions, tolerances, masses Configuration shall be in accor
22、dance with the figure. Dimensions, tolerances and masses shall conform to Figure 1 and Tables 1 and 2. Details of form, not stated are at the manufacturers option. 3.2 Material Heat resisting nickel base alloy NI-P101HT according to EN 2959 or EN 3220. 3.3 Surface treatment None. 3.4 Thread surface
23、See Figure 1. 1) Published as AECMA Prestandard at the date of publication of this standard. BS EN 3294:20085 Dimensions in millimetres Break sharp edges 0,1 mm to 0,4 mm aWhen the length of the shank is less than one time the nominal value of the shank diameter, D, the run-out is measured at a dist
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