BS EN 2934-1996 Bolts T-head relieved shank long thread in heat resisting nickel base alloy NI-P100HT (Inconel 718) silver plated - Classification 1275 MPa (at ambient temperature).pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 2934:1996 Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel718), silverplated Classification: 1275MPa (at ambient temperature)/650 C The European Standard EN2934:1996 has the status of a BritishStandard ICS 49.0
2、40.20BSEN2934:1996 This BritishStandard, having been prepared under the directionof the Engineering SectorBoard, was published underthe authority of the Standards Board andcomesintoeffect on 15June1996 BSI12-1999 The following BSI references relate to the work on this standard: Committee reference A
3、CE/12 Draft for comment88/76308 DC ISBN 0 580 25928 5 Committees responsible for this BritishStandard The preparation of this BritishStandard was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, upon which the following bodies were represented: Association of Elect
4、ronic, Telecommunications and Business Equipment Industries British Industrial Fasteners Federation Ministry of Defence Society of British Aerospace Companies Amendments issued since publication Amd. No. Date CommentsBSEN2934:1996 BSI 12-1999 i Contents Page Committees responsible Inside front cover
5、 National foreword ii Foreword 2 1 Scope 3 2 Normative references 3 3 Required characteristics 3 4 Designation 8 5 Marking 8 6 Technical specification 8 Figure 1 4 Table 1 5 Table 2 6 List of references Inside back coverBSEN2934:1996 ii BSI 12-1999 National foreword This BritishStandard has been pre
6、pared by Technical Committee ACE/12 and is the English language version of EN2934:1996 Aerospace series Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel718), silver plated Classification:1275MPa (at ambient temperature)/650 C, published by the Europe
7、an Committee for Standardization (CEN). EN2934:1996 was produced as a result of international discussions in which the United Kingdom took an active part. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their c
8、orrect application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Cross-references Publication referred to Corresponding BritishStandard EN2424:1995 BS EN2424:1995 Marking of aerospace products ISO3353:1992 BS2A231:1993 Rolled threads for bolts. Lead a
9、nd runout requirements ISO5855-2:1988 BS6293 Aerospace. MJ threads Part2:1994 Limit dimensions for bolts and nuts Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, theEN title page, pages2 to8, an inside back cover and a back cover. This standard has been u
10、pdated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN2934 March1996 ICS 49.040.20 Descriptors: Aircraft industry, screw, nickel alloy, heat resistant material,
11、 silver coating, classification, surface treatment, dimension, designation English version Aerospace series Bolts, T-head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel718), silver plated Classification:1275MPa (atambient temperature)/650 C Srie arospatiale Vis
12、tete en T, ft dgag, filetage long, en alliage rsistant a chaud base de nickel NI-P100HT (Inconel718) argentes Classification:1275MPa ( temprature ambiante)/650 C Luft- und Raumfahrt T-Kopfschrauben, Dnnschaft, langes Gewinde, aus hochwarmfester Nickelbasislegierung NI-P100HT (Inconel178), versilbert
13、 Klasse:1275MPa (bei Raumtemperatur)/650 C This European Standard was approved by CEN on1995-08-31. 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-
14、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 European Standard exists in three official versions (English, French, German). A version in any other language made by translation unde
15、r 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 national standards bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherla
16、nds, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1996 Copyright reserved to CEN members Ref. No. EN2934:1996EEN2934:19
17、96 BSI 12-1999 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in accordance with the rules of this Association, this standard has successively received the approval of the National Associations
18、 and the Official Services of the member countries of AECMA, 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 September1996, and conflicting national standards sha
19、ll be withdrawn at the latest by September1996. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxe
20、mbourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom.EN2934:1996 BSI 12-1999 3 1 Scope This standard specifies the characteristics of T-headed bolts with relieved shank, long thread, in NI-P100HT, silver plated, for aerospace applications. Classification:1275MPa 1) /65
21、0 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 appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or
22、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 referred to applies. ISO3353, Aerospace Rolled threads for bolts Lead and runout requirements. ISO5855-2, Aerospa
23、ce MJ threads Part2: Limit dimensions for bolts and nuts. EN2424, Aerospace series Marking of aerospace products. EN2583, Aerospace series Bolts in heat resisting nickel base alloy NI-P100HT (Inco718) Classification:1275MPa/650 C Technical specification 3) . EN2786, Aerospace series Electrolytic sil
24、ver plating of fasteners 3) . EN2952, Aerospace series Heat resisting alloy NI-PH2601 Solution treated and cold worked Bar for forged fasteners Dk 50mm 1270MPak R m k 1550MPa 3) . EN3219, Aerospace series Heat resisting nickel base alloy (NI-P100HT) Cold worked and softened Bar and wire for continuo
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