EN 4352-2004 en Aerospace series - Bolts double hexagon head with lockwire holes relieved shank long thread in heat resisting nickel base alloy NI-PH2601 (Inconel 718) MoS2 coated .pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 4352:2004 Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS 2coated Classification: 1 550 MPa (at ambient temperature) / 425 C The European Standard EN 4352:2004 has th
2、e status of a British Standard ICS 49.030.20 BS EN 4352:2004 This British Standard was published under the authority of the Standards Policy and Strategy Committee on 16 December 2004 BSI 16 December 2004 ISBN 0 580 45100 3 National foreword This British Standard is the official English language ver
3、sion of EN 4352:2004. It supersedes BS EN 4352:2003 which is withdrawn. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, which has the responsibility to: A list of organizations represented on this committee can be obtain
4、ed 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 “International Standards Correspondence Index”, or by using the “Search” facility of
5、 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 British Standard does not of itself confer immunity from legal obligations. aid
6、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 international and European developments and promulgate them in the UK. Summary of pages This
7、 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 issued since publication Amd. No. Date Comments EUROPEAN STANDARD NORME EUROPENNE EU
8、ROPISCHE NORM EN 4352 November 2004 ICS 49.030.20 Supersedes EN 4352:2003 English version Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1 550 MPa (at ambient t
9、emperature) / 425 C Srie arospatiale - Vis tte bihexagonale avec trous de fil frein, ft dgag, filetage long, en alliage rsistant chaud base de nickel NI-PH2601 (Inconel 718), revtues MoS2 - Classification : 1 550 MPa ( temprature ambiante) / 425 C Luft- und Raumfahrt - Zwlfkantschrauben mit Lcher fr
10、 Sicherungsdraft, Dnnschaft, langes Gewinde, aus hochwarmfester Nickelbasislegierung NI-PH2601 (Inconel 718), MoS2 beschichtet - Klasse: 1 550 MPa (bei Raumtemperatur) / 425 C This European Standard was approved by CEN on 11 September 2003. CEN members are bound to comply with the CEN/CENELEC Intern
11、al 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 national standards may be obtained on application to the Central Secretariat or to any CEN member.
12、 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 and notified to the Central Secretariat has the same status as the official versions. CEN members ar
13、e the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Ki
14、ngdom. 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 exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4352:2004: E EN
15、 4352:2004 (E) 2 Contents Page Foreword3 1 Scope 4 2 Normative references 4 3 Required characteristics.4 4 Designation 9 5 Marking .9 6 Technical specification .9 EN 4352:2004 (E) 3 Foreword This document (EN 4352:2004) has been prepared by the European Association of Aerospace Manufacturers - Stand
16、ardization (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 European Standard s
17、hall 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 4352:2003. According to the CEN/CENELEC Internal Regu
18、lations, 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, Malta, Netherlands, N
19、orway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4352:2004 (E) 4 1 Scope This standard specifies the characteristics of double hexagon headed bolts with lockwire holes, relieved shank and long thread, in NI-PH2601, MoS 2coated, for aerospace applicat
20、ions. Classification: 1 550 MPa 1)/ 425 C 2)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 referenced document (including any ame
21、ndments) applies. ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads ISO 4095, Aerospace Bihexagonal drives Wrenching configuration Metric series ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts EN 2424, Aerospace series Marking of aerospace pro
22、ducts EN 2491, Aerospace series Molybdenum disulphide dry lubricants Coating methods EN 2952, Aerospace series Heat resisting alloy NI-PH2601 Solution treated and cold worked Bar for forged fasteners D 50 mm 1 270 MPa R m 1 550 MPa 3)EN 3666, Aerospace series Heat resisting alloy NI-PH2601 Solution
23、treated and cold worked Bar for forged fasteners D 50 mm 1 550 MPa R m 1 830 MPa 3)EN 3833, Aerospace series Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated Classification: 1 550 MPa (at ambient temperature) / 650 C Technical specification 3 Required charac
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- EN43522004ENAEROSPACESERIESBOLTSDOUBLEHEXAGONHEADWITHLOCKWIREHOLESRELIEVEDSHANKLONGTHREADINHEATRESISTINGNICKELBASEALLOYNIPH2601INCONEL718MOS2COATEDPDF

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