EN 4591-2005 en Aerospace series - Nuts barrel self-locking floating selfaligning in heat resisting nickel base alloy MoS2 lubricated - Classification 1 550 MPa (at ambient tempera.pdf
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1、BRITISH STANDARD AEROSPACE SERIESBS EN 4591:2005Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated Classification: 1 550 MPa (at ambient temperature) / 315 CThe European Standard EN 4591:2005 has the status of a British StandardICS 49.030.30g49g
2、50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 4591:2005This British Standard was published under the authority of the Standards Policy and Strat
3、egy Committee on 31 January 2006 BSI 31 January 2006ISBN 0 580 47212 4National forewordThis British Standard is the official English language version of EN 4591:2005. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, which
4、 has the responsibility to: A list of organizations represented on this committee can be obtained on request to its secretary.Cross-referencesThe British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section
5、entitled “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. Compli
6、ance with 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 UK interests informed; monitor related inte
7、rnational and European developments and promulgate them in the UK.Summary of pagesThis document comprises a front cover, an inside front cover, the EN title page, pages 2 to 7 and a back cover.The BSI copyright notice displayed in this document indicates when the document was last issued.Amendments
8、issued since publicationAmd. No. Date CommentsEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4591 December 2005 ICS 49.030.30 English Version Aerospace series - Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated - Classification: 1 550 MPa
9、 (at ambient temperature) / 315 C Srie arospatiale - crous porte cylindrique, freinage interne, flottants, orientables, en alliage rsistant chaud base de nickel, lubrifis MoS2 - Classification : 1 550 MPa ( temprature ambiante) / 315 C Luft- und Raumfahrt - Selbsteinstellende, freibewegliche, selbst
10、sichernde Tonnenmuttern, aus hochwarmfester Nickelbasislegierung, MoS2-geschmiert - Klasse: 1 550 Mpa (bei Raumtemperatur) / 315 C This European Standard was approved by CEN on 26 October 2005. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions f
11、or 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 European Standard exists in three officia
12、l 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 national standards bodies of Austria, Bel
13、gium, 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 Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION C
14、OMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2005 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4591:2005: E2 Contents Page Foreword 3 1 Scope .4 2 Normative
15、references .4 3 Required characteristics 5 4 Designation .7 5 Marking 7 6 Technical specification.7 EN 4591:20053 Foreword This European Standard (EN 4591:2005) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried
16、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 shall be given the status of a national standard, either by
17、publication of an identical text or by endorsement, at the latest by June 2006, and conflicting national standards shall be withdrawn at the latest by June 2006. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC s
18、hall not be held responsible for identifying any or all such patent rights. According 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, Fi
19、nland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4591:20054 1 Scope This standard specifies the characteristics of self-locking, flo
20、ating, self-aligning barrel nuts, in heat resisting nickel alloy, MoS2lubricated. Classification: 1 550 MPa 1) / 315 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
21、 references, the latest edition of the referenced document (including any amendments) applies. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. ISO 5858, Aerospace Nuts, self-locking, with maximum operating temperature less than or equal to 425 C Procurement specificatio
22、n. ISO 8788, Aerospace Nuts, metric Tolerances of form and position. ISO 12278, Aerospace Nuts, barrel, self-locking, floating, self-aligning, with MJ thread, Classifications: 900 MPa (at ambient temperature) / 235 C, 1 100 MPa (at ambient temperature) / 235 C, 1 250 MPa (at ambient temperature) / 2
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- EN45912005ENAEROSPACESERIESNUTSBARRELSELFLOCKINGFLOATINGSELFALIGNINGINHEATRESISTINGNICKELBASEALLOYMOS2LUBRICATEDCLASSIFICATION1550MPAATAMBIENTTEMPERAPDF

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