EN 6092-2016 en Aerospace series - Receptacle floating double lug《航空航天系列-插座 浮动 双耳》.pdf
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1、BS EN 6092:2016Aerospace series Receptacle,floating, double lugBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 6092:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 6092:2016.The UK participation in its preparation was
2、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.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its cor
3、rectapplication. The British Standards Institution 2016. Published by BSI StandardsLimited 2016ISBN 978 0 580 92619 8ICS 49.030.99Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strateg
4、y Committee on 30 September 2016.Amendments issued since publicationDate Text affectedBS EN 6092:20162“ EN 6092 trsx vrur ss trsx 22 “ o CEN-CENELECManagement Centre: Avenue Marnix 17, B-1000 Brussels 9trsx xrttrsxBS EN 6092:2016EN 6092:2016 (E) 2 Contents Page European foreword 3 1 Scope 4 2 Normat
5、ive references 4 3 Requirements 5 4 Designation 9 5 Marking . 9 6 Technical specification 9 7 Example of installation 9 BS EN 6092:2016EN 6092:2016 (E) 3 European foreword This document (EN 6092:2016) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (
6、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. This European Standard shall be given th
7、e status of a national standard, either by publication of an identical text or by endorsement, at the latest by February 2017, and conflicting national standards shall be withdrawn at the latest by February 2017. Attention is drawn to the possibility that some of the elements of this document may be
8、 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 European Standard: Austria, Be
9、lgium, 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, Swit
10、zerland, Turkey and the United Kingdom. BS EN 6092:2016EN 6092:2016 (E) 4 1 Scope This European Standard specifies the dimensions, tolerances, required characteristics and mass of a receptacle for use in fuselage interior equipment and structural applications. This standard shall be used in conjunct
11、ion with studs per EN 6088 or EN 6105. 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 r
12、eferenced document (including any amendments) applies. DIN 17850, Titanium, chemical composition EN 2424, Aerospace series Marking of aerospace products EN 2516, Aerospace series Passivation of corrosion resistant steels and decontamination of nickel base alloys EN 2808, Aerospace series Anodizing o
13、f titanium and titanium alloys EN 6088, Aerospace series Stud1)EN 6089, Aerospace series Washer, retaining, for usage with stud EN 60881)EN 6090, Aerospace series Washer, retaining1)EN 6091, Aerospace series Circlip1)EN 6094, Aerospace series Washer, spring, countersunk1)EN 6095, Aerospace series Ro
14、tary fasteners Structural and non-structural applications Technical specification1)EN 6105, Aerospace series Stud with shoulder1)EN 10088-3, Stainless steels Part 3: Technical delivery conditions for semi-finished products, bars, rods, wire, sections and bright products of corrosion resisting steels
15、 for general purposes EN 10270-1, Steel wire for mechanical springs Part 1: Patented cold drawn unalloyed spring steel wire EN 10270-3, Steel wire for mechanical springs Part 3: Stainless spring steel wire ISO 2768-1, General tolerances Part 1: Tolerances for linear and angular dimensions without in
16、dividual tolerance indications ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process SAE AMS 2700, Passivation of corrosion resistant steels2)1)Published as ASD-STAN Prestandard at the date of publication of this standard (www.asd-stan.org). 2)Published by: Socie
17、ty of Automotive Engineers (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA BS EN 6092:2016EN 6092:2016 (E) 5 SAE AMS 5528, Steel, corrosion resistant, sheet, strip and plate, 17Cr-7.1Ni-1.1Al, solution heat treated, precipitation hardenable2)SAE AS 8879, Screw threads UNJ profile, inch
18、 controlled radius root with increased minor diameter2)MIL-DTL-83488, Coating, aluminium, high purity3)MIL-PRF-46010, Lubricant, solid film, heat cured, corrosion inhibiting3)3 Requirements 3.1 Configuration, dimensions and tolerances The configuration, dimensions and tolerances shall conform with F
19、igure 1. Dimensions and tolerances are expressed in millimetres. Tolerances not specified shall be in accordance with ISO 2768-1 (Tolerance class: ISO 2768-m). All dimensions and tolerances apply after surface treatment. All burrs to be removed/sharp edges to be broken. 3)Published by: Department of
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