EN 6105-2016 en Aerospace series - Stud with shoulder《航空航天系列-带肩的螺柱》.pdf
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1、BS EN 6105:2016Aerospace series Stud withshoulderBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 6105:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 6105:2016.The UK participation in its preparation was entrusted to T
2、echnicalCommittee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplicatio
3、n. The British Standards Institution 2016.Published by BSI Standards Limited 2016ISBN 978 0 580 92622 8ICS 49.030.20Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on
4、 30 September 2016.Amendments/corrigenda issued since publicationDate Text affectedBS EN 6105:20162“ EN 6105 trsx vrurtr ss trsx 22 “ o CEN-CENELECManagement Centre: Avenue Marnix 17, B-1000 Brussels 9trsx xsrwtrsxBS EN 6105:2016EN 6105:2016 (E) 2 Contents Page European foreword 3 1 Scope 4 2 Normat
5、ive references 4 3 Requirements 5 3.1 Configuration, dimensions, tolerances and mass 5 3.2 Material and surface treatment 6 3.3 Mechanical characteristics . 7 3.3.1 General 7 3.3.2 Static values . 7 3.3.3 Installation torque 7 3.4 Operating temperature . 7 4 Designation 7 5 Marking . 7 6 Technical s
6、pecification 7 7 Example of installation 8 BS EN 6105:2016EN 6105:2016 (E) 3 European foreword This document (EN 6105:2016) 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
7、 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. This European Standard shall be given the status of a national standard, either by publication of an identical text o
8、r by endorsement, at the latest by March 2017, and conflicting national standards shall be withdrawn at the latest by March 2017.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
9、 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, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former
10、 Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 6105:2016EN 6105:2016 (E) 4 1 Scope T
11、his European Standard specifies the dimensions, tolerances, required characteristics and mass of a stud for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with retaining washer per EN6090A01 (conform to EN 6090) and receptacles per EN 6092
12、or EN 6093. 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, only the edition cited applies. For undated references, the latest edition of the referenced document (includi
13、ng any amendments) applies. EN 2424, Aerospace series Marking of aerospace products EN 2516, Aerospace series Passivation of corrosion resistant steels and decontamination of nickel base alloys EN 4318, Aerospace series Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipita
14、tion treated bar and section, De 100 mm, Rm 960 MPa1)EN 6090, Aerospace series Washer, retaining1)EN 6092, Aerospace series Receptacle, floating, double lug1)EN 6093, Aerospace series Receptacle, floating, single lug1)EN 6094, Aerospace series Washer, spring, countersunk1)EN 6095, Aerospace series R
15、otary fasteners Structural and non-structural applications Technical specification1)ISO 2768-1, General tolerances Part 1: Tolerances for linear and angular dimensions without individual tolerance indications SAE-AMS 2700, Passivation of corrosion resistant steels2)SAE-AMS 5629, Steel, corrosion-res
16、istant, bars, wire, forgings, rings and extrusions, 13Cr 8.0Ni 2.2Mo 1.1Al, vacuum induction plus consumable electrode melted, solution heat treated, precipitation hardenable2)SAE-AMS 5737, Steel, corrosion and heat-resistant, bars, wire, forgings and tubing 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V, con
17、sumable electrode melted, 1 650 F (899 C) solution and precipitation heat treated2)SAE-AS 8879, Screw threads, UNJ profile, inch controlled radius root with increased minor diameter2)MIL-DTL-83488, Coating, aluminum, high purity3)MIL-S-7742, Screw threads, standard, optimum selected series: general
18、specification for3)NASM 33781, Recess, Offset cruciform, dimensions of recess, gage and driver for4)1) Published as ASD Prestandard at the date of publication of this standard. 2) Published by: SAE International, 400 Commonwealth Drive, Warrendale, P.A., 15096-0001, USA 3) Published by: Department o
19、f Defense (DoD), the Pentagon, Washington, D.C., 20307, USA 4) Published by: Aerospace Industries Association of America, (AIA), 1250 Eye Street, N.W., Washington, D.C. 20005-3924, USA BS EN 6105:2016EN 6105:2016 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configurati
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