BS EN 6129-2016 Aerospace series Blind bolt protruding head high strength pulltype《航空航天系列 高强度牵引式凸头封闭螺栓》.pdf
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1、Aerospace series Blind bolt,protruding head, high strength,pulltypeBS EN 6129:2016Incorporating corrigendum .BSDI 2017BSI Standards PublicationBS EN 6129:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 6129:2016, incorporating corrigendum .BSDI 2017.The UK
2、participation in its preparation was entrusted to Technical Committee 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 con
3、tract. Users are responsible for its correct application. The British Standards Institution 2017. Published by BSI Standards Limited 2017ISBN 978 0 580 97497 7ICS 49.030.20; 49.030.60Compliance with a British Standard cannot confer immunity from legal obligations.This British Standard was published
4、under the authority of the Standards Policy and Strategy Committee on 30 September 2016.Amendments/corrigenda issued since publicationDate Text affected.BSDI 2017 Implementation of CEN corrigendum February 2017: figure in clause 4 correctedEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 6129 Se
5、ptember 2016 ICS 49.030.20; 49.030.60 English Version Aerospace series - Blind bolt, protruding head, high strength, pulltype Srie arospatiale - Boulon aveugle, tte protubrante, haute rsistance, installation en tirant Luft- und Raumfahrt - Blindniet, Universalkopf, hochfest (Zugtyp) This European St
6、andard was approved by CEN on 11 March 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 concerning
7、 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 its
8、 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, German
9、y, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. This document consolidates EN 6129:2016 and the corrigendum EN 6129:2016/AC:2017. EUROPEAN COM
10、MITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2016 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 6129:2016 EEN 6129:2016
11、(E) 2 Contents Page European foreword 3 1 Scope 4 2 Normative references 4 3 Requirements 4 3.1 Configuration, dimensions and tolerances 4 3.2 Grip range and weight 4 3.3 Material, finish, lubrication . 5 4 Designation 10 5 Marking . 10 6 Technical specification 11 BS EN 6129:2016g8g17g3g888g883g884
12、g891g483g884g882g883g888g3g525g8g526EN 6129:2016 (E) 3 European foreword This document (EN 6129:2016) has been prepared 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,
13、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. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at t
14、he latest by March 2017, and conflicting national standards shall be withdrawn at the latest by March 2017. 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 shall not be held responsible for identifying any or al
15、l such patent rights. This document includes the corrigendum EN 6129:2016/AC:2017 which corrects the figure in Clause 4. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium,
16、 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, Slovakia, Slovenia, Spain, Sweden, Switzerlan
17、d, Turkey and the United Kingdom. BS EN 6129:2016g8g17g3g888g883g884g891g483g884g882g883g888g3g525g8g526EN 6129:2016 (E) 4 1 Scope This standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with protruding head, for aerospace application. 2 Normative re
18、ferences The following documents, in whole or in part, 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
19、. EN 2424, Aerospace series Marking of aerospace products EN 4473, Aerospace series Aluminium pigmented coatings for fasteners Technical specification1)AS 5272, Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting Procurement Specification2)SAE AMS 5687, Nickel Alloy, Corrosion and Heat-Resistant
20、, Wire 74Ni 15,5Cr 8,0Fe Annealed2)SAE AMS 5737, Steel, corrosion and heat-resistant, bars, wire, forgings and tubing 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V, consumable electrode melted, 1650 F (899 C), solution and precipitation heat treated2) AMS-QQ-P-35, Passivation treatments for Corrosion-Resista
21、nt Steel2) MIL-PRF-46010F, Lubricant, Solid Film, Heat cured, Corrosion Inhibiting NATO Code-S-17383)SAE AS 87132, Lubricant, Cetyl Alcohol, 1- Hexadecanol, Application to fasteners3)DOD-L-85645, Lubricant, Dry Thin Film, Molecular Bonded3)NASM 8975, Fasteners, Blind, High Strength, Installation For
22、med, Corrosion Resistant Steel, Heat Resistant Steel and Titanium, General Specification for4)3 Requirements 3.1 Configuration, dimensions and tolerances The configuration, dimensions, tolerances, static and dynamic values shall conform to Figures 1 and 2 and Tables 1 and 2. 3.2 Grip range and weigh
23、t See Tables 3 and 4. 1)Published as AECMA Prestandard at the date of publication of this standard. 2)Published by: Society of Automotive Engineers (SAE), 400 Commonwealth drive, Warrendale, PA 15096-0001, USA. 3) Published by: Department of Defense (DoD), the Pentagon, Washington, D.C. 20301, USA.
24、4)Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C. 20005-3924, USA. BS EN 6129:2016g8g17g3g888g883g884g891g483g884g882g883g888g3g525g8g526EN 6129:2016 (E) 5 3.3 Material, finish, lubrication See Tables 5 and 6. Key 1 Marking, see clause 5
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