BS-EN-4322-2004.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 4322:2004 Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated Strength class: 1 100 MPa (at ambient temperature) The European Standard EN 4322:2004 has the status of a British Standard
2、 ICS 49.030.20 ? Licensed Copy: sheffieldun sheffieldun, na, Sat Nov 04 08:41:03 GMT+00:00 2006, Uncontrolled Copy, (c) BSI BS EN 4322:2004 This British Standard, was published under the authority of the Standards Policy and Strategy Committee on 15 December 2004 BSI 15 December 2004 ISBN 0 580 4509
3、4 5 National foreword This British Standard is the official English language version of EN 4322:2004. It supersedes BS EN 4322:2003 which is withdrawn. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, which has the respon
4、sibility 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 entitled “Int
5、ernational 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 with a
6、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 internationa
7、l 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. Amendments issu
8、ed since publication Amd. No. DateComments Licensed Copy: sheffieldun sheffieldun, na, Sat Nov 04 08:41:03 GMT+00:00 2006, Uncontrolled Copy, (c) BSI EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4322 November 2004 ICS 49.030.20 Supersedes EN 4322:2003 English version Aerospace series - Bolts
9、, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature) Srie arospatiale - Vis tte bihexagonale avec trous de fil frein, ft dgag, filetage long, en alliage de titane TI- P64001, an
10、odises, revtues MoS2 - Classe de rsistance : 1 100 MPa ( temprature ambiante) Luft- und Raumfahrt - Zwlfkantschrauben mit Lcher fr Sicherungsdraft, Dnnschaft, langes Gewinde, aus Titanlegierung TI-P64001, anodisiert, MoS2 beschichtet - Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur) This European
11、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. Up-to-date lists and bibliographical references conc
12、erning 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 under the responsibility of a CEN member into its own
13、 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, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembou
14、rg, 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 Stassart, 36 B-1050 Brussels 2004 CEN All rights of expl
15、oitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4322:2004: E Licensed Copy: sheffieldun sheffieldun, na, Sat Nov 04 08:41:03 GMT+00:00 2006, Uncontrolled Copy, (c) BSI EN 4322:2004 (E) 2 Contents Page Foreword3 1 Scope4 2 Normative references4 3 Require
16、d characteristics.4 4 Designation 9 5 Marking.9 6 Technical specification.9 Licensed Copy: sheffieldun sheffieldun, na, Sat Nov 04 08:41:03 GMT+00:00 2006, Uncontrolled Copy, (c) BSI EN 4322:2004 (E) 3 Foreword This document (EN 4322:2004) has been prepared by the European Association of Aerospace M
17、anufacturers - 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 presentation to CEN. This
18、 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 4322:2003. According to the CEN/C
19、ENELEC 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, Luxembourg, M
20、alta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. Licensed Copy: sheffieldun sheffieldun, na, Sat Nov 04 08:41:03 GMT+00:00 2006, Uncontrolled Copy, (c) BSI EN 4322:2004 (E) 4 1 Scope This standard specifies the characteristics of dou
21、ble hexagon headed bolts with lockwire holes, relieved shank and long thread, in TI-P64001, anodized, MoS2 coated, for aerospace applications. Strength class: 1 100 MPa 1) 2 Normative references The following referenced documents are indispensable for the application of this document. For dated refe
22、rences, 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
23、 ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts EN 2424, Aerospace series Marking of aerospace products EN 2491, Aerospace series Molybdenum disulphide dry lubricants Coating methods EN 3813, Aerospace series Titanium alloy TI-P64001 Annealed Bar and wire for forged fas
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