BS EN 6029-2017 Aerospace series Rod-ends adjustable single fork with UNJ threaded shank min engagement 1 5 x thread diameter in corrosion resisting steel Dimensions and loads Inch.pdf
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1、BS EN 6029:2017Aerospace series Rod-ends,adjustable, single fork withUNJ threaded shank min.engagement: 1,5 x threaddiameter in corrosion resistingsteel Dimensions and loads Inch seriesBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 6029:2017 BRITISH STANDARDNa
2、tional forewordThis British Standard is the UK implementation of EN 6029:2017.The 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 beobtained on request to its secretary
3、.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2017. Published by BSI Standards Limited 2017ISBN 978 0 580 94473 4ICS 49.035Compliance with a British Standard cannot confer i
4、mmunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 31 January 2017.Amendments/Corrigenda issued since publicationDate Text affectedBS EN 6029:2017EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 6029 January 2017
5、 ICS 49.035 English Version Aerospace series - Rod-ends, adjustable, single fork with UNJ threaded shank min. engagement: 1,5 x thread diameter in corrosion resisting steel - Dimensions and loads - Inch series Srie arospatiale - Embouts rglables a chape simple a tige filete UNJ, implantation min. :
6、1,5 x diamtre de filetage en acier rsistant la corrosion - Dimensions et charges - Srie en inches Luft- und Raumfahrt - Einstellbare Gabelkpfe, einfach, UNJ-Gewindeschaft, min. Einschraubtiefe 1,5 x Gewindedurchmesser, aus korrosionsbestndigem Stahl - Mae und Belastungen - Inch-Reihe This European S
7、tandard was approved by CEN on 20 August 2016. 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 concerni
8、ng such national standards may be obtained on application 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 i
9、ts own language and notified to the CEN-CENELEC Management 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, Germ
10、any, Greece, Hungary, Iceland, Ireland, Italy, Latvia, 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 KO
11、MITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue 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 6029:2017 E BS EN 6029:2017EN 6029:2017 (E) 2 Contents Page European foreword . 3 1 Scope 4 2 No
12、rmative references 4 3 Required characteristics 4 4 Designation 9 5 Marking . 9 6 Technical specification 9 Annex A (informative) Standard evolution form . 10 BS EN 6029:2017EN 6029:2017 (E) 3 European foreword This document (EN 6029:2017) has been prepared by the Aerospace and Defence Industries As
13、sociation of Europe - Standardization (ASD-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 ASD, prior to its presentation to CEN. T
14、his 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. Attention is drawn to the possibility that some of the e
15、lements 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 of the following countries are bound to implement this
16、 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, Netherlands, Norway, Poland, Portugal, Romania, Serbia,
17、Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 6029:2017EN 6029:2017 (E) 4 1 Scope This European Standard specifies the characteristics of adjustable rod ends in corrosion resisting steel, inch series, consisting of: a single fork ; a UNJ threaded shank with ; m
18、in. engagement 1,5 times thread diameter and longitudinal groove for locking purposes. These rod ends are intended for use with control rods or rods for aerospace structures. They shall be used in the temperature range 54 C and 150 C. 2 Normative references The following documents, in whole or in pa
19、rt, are normatively referenced in this document and are indispensable for its application. For dated references, 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 pr
20、oducts EN 2601, Aerospace series Fork ends, adjustable Technical specification EN 3161, Aerospace series Steel FE-PM3801 (X5CrNiCu17-4) Air melted, solution treated and precipitation treated, bar a or D 200 mm, Rm 930 MPa ISO 3161:1999, Aerospace UNJ threads General requirements and limit dimensions
21、 ISO 3353-1:2002, Aerospace Lead and runout threads Part 1: Rolled external threads ISO 8074, Aerospace Surface treatment of austenitic stainless steel parts NAS 559, Rod End Lock 1)3 Required characteristics 3.1 Configuration Dimensions Tolerances Masses See Figure 1 and Table 1. Dimensions and tol
22、erances are expressed in millimetres (inches) and apply after passivation. 3.2 Surface roughness See Figure 1. Values in micrometres (microinches) apply before passivation. 3.3 Materials Steel EN 3161: 34 HRC to 42 HCR. 3.4 Surface treatment Passivated according to ISO 8074. Break sharp edges and co
23、rners and remove all burrs and slivers. 1) Published by: Aerospace Industries Association of America, Inc., 1250 Eye street, NW Washington, DC 20005, USA. BS EN 6029:2017EN 6029:2017 (E) 5 Key R3 (0.004)0,10max. 1 Marking a Thread run-out according to ISO 3353-1 b Pitch - c Groove as per NAS 559 Fig
24、ure 1 Configuration BS EN 6029:2017EN 6029:2017 (E) 6 Concentricity of 0,25 (0.01) between D4axis and A where “A“ is the axis of the thread pitch diameter. Table 1 Dimensions, tolerances and mass (1 of 3) Size code Shank Type of thread UNJF-3A according to ISO 3161D4L6L8L9L10L11R1R20 0,3 + 1,0 0, +
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