BS EN 3011-1998 Bolts hexagon head relieved shank long thread in heat resisting nickel base alloy NI-P101HT (Waspaloy) silver plated - Classification 1210 MPa (at ambient temperatu.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 3011:1998 Bolts, hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated Classification: 1210MPa (at ambient temperature)/730C The European Standard EN 3011:1998 has the status of a British Standard IC
2、S 49.030.20BSEN3011:1998 This British Standard, having been prepared under the direction of the Engineering Sector Board, was published under the authority of the Standards Board and comes into effect on 15 July 1998 BSI 04-1999 ISBN 0 580 30161 3 National foreword This British Standard is the Engli
3、sh language version of EN 3011:1998. The UK participation in its preparation was entrusted by Technical Committee ACE/12, Aerospace fasteners and fastening systems, to Subcommittee ACE/12/1, Aerospace fasteners and fastening systems (International), which has the responsibility to: aid enquirers to
4、understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UKinterests informed; monitor related international and European developments and promulgate them in the UK. A list of organizations represented
5、 on this subcommittee can be obtained on request to its secretary. Cross-references The British Standards which implement international or European publications referred to in this document may be found in the BSI Standards Catalogue under the section entitled “International Standards Correspondence
6、 Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itse
7、lf confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pages i and ii, theEN title page, pages2 to 7 and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicat
8、ed in the amendment table on the inside front cover. Amendments issued since publication Amd. No. Date CommentsBSEN3011:1998 BSI 04-1999 i Contents Page National foreword Inside front cover Foreword 2 Text of EN 3011 3ii blankEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3011 May 1998 ICS 49.
9、030.20 Descriptors: Aircraft industry, screw, hexagonal head screw, nickel alloy, heat resistant material, characteristic, surface treatment, screw thread, code, dimension, designation, marking English version Aerospace series Bolts, hexagon head, relieved shank, long thread, in heat resisting nicke
10、l base alloy NI-P101HT (Waspaloy), silver plated Classification: 1210MPa (at ambient temperature)/730C Srie arospatiale Vis tte hexagonale, ft dgag, filetage long, en alliage rsistant chaud base de nickel NI-P101HT (Waspaloy), argentes Classification: 1210 MPa ( temprature ambiante)/730C Luft- und R
11、aumfahrt Sechskantschrauben, Dnnschaft, langes Gewinde, aus hochwarmfester Nickelbasislegierung NI-P101HT (Waspaloy), versilbert Klasse: 1210MPa (bei Raumtemperatur)/730C This European Standard was approved by CEN on 23 February 1998. CEN members are bound to comply with the CEN/CENELEC Internal Reg
12、ulations 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 Central Secretariat or to any CEN member. This
13、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 Central Secretariat has the same status as the official versions. CEN members are the
14、national standards bodies of Austria, Belgium, CzechRepublic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europi
15、sches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1998 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3011:1998 EEN3011:1998 BSI 04-1999 2 Foreword This European Standard has been prepared by the Eu
16、ropean Association of Aerospace Manufacturers (AECMA). After inquiries 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 AECMA, prior to its presentation to
17、 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 November1998, and conflicting national standards shall be withdrawn at the latest by November1998. According to the CEN/CENELEC Internal Regul
18、ations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, CzechRepublic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the Un
19、itedKingdom. Contents Page Foreword 2 1 Scope 3 2 Normative references 3 3 Required characteristics 3 4 Designation 7 5 Marking 7 6 Technical specification 7 Figure 1 4 Table 1 4 Table 2 5EN3011:1998 BSI 04-1999 3 1 Scope This standard specifies the characteristics of hexagon headed bolts with relie
20、ved shank and long thread, in NI-P101HT, silver plated, for aerospace applications. Classification: 1210MPa 1) /730 C 2) 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriat
21、e places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication
22、 referred to applies. ISO 3353, Aerospace Rolled threads for bolts Lead and runout requirements. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. EN 2424, Aerospace series Marking of aerospace products. EN 2582, Aerospace series Bolts in heat resisting nickel base alloy
23、NI-P101HT (Waspaloy) Classification: 1210 MPa/730 C Technical specification 3) . EN 2786, Aerospace series Electrolytic silver plating of fasteners 3) . EN 2959, Aerospace series Heat resisting nickel base alloy (NI-P101HT) Solution treated and cold worked Bar for hot upset forging for fasteners 3 D
24、 30mm 3) . EN 3220, Aerospace series Heat resisting nickel base alloy (NI-P101HT) Cold worked and softened Bar and wire for continuous forging or extrusion for fasteners 3 D 30mm 3) . 3 Required characteristics 3.1 Configuration Dimensions Tolerances Masses SeeFigure 1 andTable 1 andTable 2. Dimensi
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