EN 3908-2017 en Aerospace series - Nipples lubricating axial type in corrosion resisting steel passivated《航空航天系列-钝化润滑轴向型耐腐蚀钢制乳头》.pdf
《EN 3908-2017 en Aerospace series - Nipples lubricating axial type in corrosion resisting steel passivated《航空航天系列-钝化润滑轴向型耐腐蚀钢制乳头》.pdf》由会员分享,可在线阅读,更多相关《EN 3908-2017 en Aerospace series - Nipples lubricating axial type in corrosion resisting steel passivated《航空航天系列-钝化润滑轴向型耐腐蚀钢制乳头》.pdf(16页珍藏版)》请在麦多课文档分享上搜索。
1、BS EN 3908:2017Aerospace series Nipples,lubricating, axial type, incorrosion resisting steel,passivatedBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 3908:2017 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 3908:2017. The
2、 UK participation in its preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems. A list of organizations represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a
3、 contract. Users are responsible for its correct application. The British Standards Institution 2017.Published by BSI Standards Limited 2017ISBN 978 0 580 92978 6 ICS 49.035 Compliance with a British Standard cannot confer immunity from legal obligations.This British Standard was published under the
4、 authority of the Standards Policy and Strategy Committee on 31 January 2017.Amendments/corrigenda issued since publicationDate T e x t a f f e c t e dBS EN 3908:2017EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3908 January 2017 ICS 49.035 English Version Aerospace series - Nipples, lubricat
5、ing, axial type, in corrosion resisting steel, passivated Srie arospatiale - Graisseurs accrochage axial, en acier rsistant la corrosion, passivs Luft- und Raumfahrt - Kegel-Schmiernippel, aus korrosionsbestndigem Stahl, passiviert This European Standard was approved by CEN on 11 March 2016. CEN mem
6、bers 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 concerning such national standards may be obtained on applicat
7、ion to the CEN-CENELEC Management Centre 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 language and notified to the CEN-CENELEC Manage
8、ment Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia,
9、 Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue
10、 Marnix 17, B-1000 Brussels 2017 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3908:2017 EBS EN 3908:2017EN 3908:2017 (E) 2 Contents Page European foreword . 3 1 Scope 4 2 Normative references 4 3 Required characteristics 5 4 Des
11、ignation 7 5 Marking . 8 6 Technical specification 8 7 Requirements and test methods 8 Annex A (normative) Installation requirements . 12 A.1 Space requirements 12 A.2 Installation thread requirement 12 BS EN 3908:2017EN 3908:2017 (E) 3 European foreword This document (EN 3908:2017) has been prepare
12、d by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this European Standard has received the approval of the National Associations and the Official Services of the member
13、countries of ASD, 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 July 2017, and conflicting national standards shall be withdrawn at the latest by July 2017. Att
14、ention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN-CENELEC Internal Regulations, the national standards organizations o
15、f the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Net
16、herlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 3908:2017EN 3908:2017 (E) 4 1 Scope This European Standard specifies the required characteristics and the tests for lubricating nipples of the axial type, in corr
17、osion resisting steel, passivated. Annex A (normative) states the clearance space requirements for the coupling and uncoupling of the lubricating gun and the maximum permissible diameter of the lubricating gun barrel, together with installation thread requirements. Lubricating nipples according to t
18、his European Standard are intended for use in aerospace assemblies, where regular lubrication of moving parts is required. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references,
19、 only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products EN 2516, Aerospace series Passivation of corrosion resisting steels and decontamination of nickel base al
20、loys EN 9100, Quality Management Systems Requirements for Aviation, Space and Defense Organizations ISO 68 (all parts), ISO general purpose screw threads Basic profile IS0 413, Aircraft Heads of lubricating nipples ISO 965-2, ISO general purpose metric screw threads Tolerances Part 2: Limits of size
21、s for general purpose external and internal screw threads Medium quality ISO 2859-1, Sampling procedures for inspection by attributes Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-lot inspection ISO 6507-1, Metallic materials Vickers hardness test Part 1: Test method
22、STANAG 1135:2008, Interchangeability of fuels, lubricants and associated products used by the armed forces of the North Atlantic Treaty Nations 1)1) Published by: North Atlantic Treaty Organization (NATO), Military Agency for Standardization (MAS), 1110 Brussels, Belgium. BS EN 3908:2017EN 3908:2017
23、 (E) 5 3 Required characteristics 3.1 Configuration Dimensions Masses The envelope dimensions for the nipple head are shown in Figure 1, detail “Z“ and are in accordance with ISO 413. The tip design of the nipple (face with the sealing ball) is left at the manufacturers option provided the profile r
24、emains within the envelope dimensions shown in figure 1 and the requirements of Clause 7 are met. The dimensions apply after surface treatment. A check valve (composed of a spring and ball) shall be located at the surface of the nipple to prevent the ingress of foreign matter into the nipple tip. Ot
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- EN39082017ENAEROSPACESERIESNIPPLESLUBRICATINGAXIALTYPEINCORROSIONRESISTINGSTEELPASSIVATED 航空航天 系列 钝化

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