BS EN 4321-2004 Aerospace series - Bolts double hexagon head with lockwire holes relieved shank long thread in heat resisting nickel base alloy NI-PH2601 (Inconel 718) silver plate.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 4321:2004 Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated Classification: 1 550 Mpa (at ambient temperature)/650 C The European Standard EN 4321:2004 has th
2、e status of a British Standard ICS 49.030.20 Licensed Copy: Wang Bin, na, Fri Mar 18 02:25:02 GMT 2005, Uncontrolled Copy, (c) BSIBS EN 4321:2004 This British Standard was published under the authority of the Standards Policy and Strategy Committee on 14 December 2004 BSI 14 December 2004 ISBN 0 580
3、 45095 3 National foreword This British Standard is the official English language version of EN 4321:2004. It supersedes BS EN 4321:2003, which is withdrawn. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, which has the
4、responsibility to: A list of organizations represented on this committee 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 Catalogue under the section entitle
5、d “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue or of British Standards Online. This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. Compliance w
6、ith a British Standard does not of itself confer immunity from legal obligations. aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related intern
7、ational and European developments and promulgate them in the UK. Summary of pages This document comprises a front cover, an inside front cover, the EN title page, pages 2 to 9 and a back cover. The BSI copyright notice displayed in this document indicates when the document was last issued. Amendment
8、s issued since publication Amd. No. Date Comments Licensed Copy: Wang Bin, na, Fri Mar 18 02:25:02 GMT 2005, Uncontrolled Copy, (c) BSI EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4321 November 2004 ICS 49.030.20 Supersedes EN 4321:2003 English version Aerospace series - Bolts, double hexag
9、on head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 550 MPa (at ambient temperature) / 650 C Srie arospatiale - Vis tte bihexagonale avec trous de fil frein, ft dgag, filetage long, en alliage rsista
10、nt chaud base de nickel NI-PH2601 (Inconel 718), argentes - Classification : 1 550 MPa ( temprature ambiante) / 650 C Luft- und Raumfahrt - Zwlfkantschrauben mit Lcher fr Sicherungsdraft, Dnnschaft, langes Gewinde, aus hochwarmfester Nickelbasislegierung NI-PH2601 (Inconel 718), versilbert - Klasse:
11、 1 550 MPa (bei Raumtemperatur) / 650 C This European Standard was approved by CEN on 11 September 2003. 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
12、. 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 European Standard exists in three official versions (English, French, German). A version in any other language made by translation
13、 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 national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary
14、, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de St
15、assart, 36 B-1050 Brussels 2004 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4321:2004: E Licensed Copy: Wang Bin, na, Fri Mar 18 02:25:02 GMT 2005, Uncontrolled Copy, (c) BSI EN 4321:2004 (E) 2 Contents Page Foreword3 1 Scope 4
16、 2 Normative references 4 3 Required characteristics.4 4 Designation 9 5 Marking .9 6 Technical specification .9 Licensed Copy: Wang Bin, na, Fri Mar 18 02:25:02 GMT 2005, Uncontrolled Copy, (c) BSIEN 4321:2004 (E) 3 Foreword This document (EN 4321:2004) has been prepared by the European Association
17、 of Aerospace Manufacturers - Standardization (AECMA-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 AECMA, prior to its presentati
18、on 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 May 2005, and conflicting national standards shall be withdrawn at the latest by May 2005. This document supersedes EN 4321:2003. Accordi
19、ng to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania
20、, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. Licensed Copy: Wang Bin, na, Fri Mar 18 02:25:02 GMT 2005, Uncontrolled Copy, (c) BSI EN 4321:2004 (E) 4 1 Scope This standard specifies the characteristics of double he
21、xagon headed bolts with lockwire holes, relieved shank and long thread, in NI-PH2601, silver plated, for aerospace applications. Classification: 1 550 MPa 1)/ 650 C 2)2 Normative references The following referenced documents are indispensable for the application of this document. For dated reference
22、s, 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 external threads ISO 4095, Aerospace Bihexagonal drives Wrenching configuration Metric series ISO
23、5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts EN 2424, Aerospace series Marking of aerospace products EN 2786, Aerospace series Electrolytic silver plating of fasteners 3)EN 2952, Aerospace series Heat resisting alloy NI-PH2601 Solution treated and cold worked Bar for forg
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- BSEN43212004AEROSPACESERIESBOLTSDOUBLEHEXAGONHEADWITHLOCKWIREHOLESRELIEVEDSHANKLONGTHREADINHEATRESISTINGNICKELBASEALLOYNIPH2601INCONEL718SILVERPLATEPDF

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