1、BSI Standards PublicationBS EN 4710-07:2015Aerospace series Quickrelease fastening systems fornon-structural applicationsPart 07: Retaining grommetBS EN 4710-07:2015 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 4710-07:2015.The UK participation in its prepara
2、tion 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.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible fo
3、r its correctapplication. The British Standards Institution 2015.Published by BSI Standards Limited 2015ISBN 978 0 580 89136 6ICS 49.035Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and S
4、trategy Committee on 31 October 2015.Amendments/corrigenda issued since publicationDate Text affectedBS EN 4710-07:2015EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORMEN 4710-07 October 2015 ICS 49.035 English Version Aerospace series - Quick release fastening systems for non-structural application
5、s - Part 07: Retaining grommetSrie arospatiale - Fixations rapides filetes pour applications non-structurales - Partie 07 : Oeillet de retenue Luft- und Raumfahrt - Schnellverschlsse fr nicht-strukturelle Anwendungen - Teil 07: Haltering This European Standard was approved by CEN on 5 March 2015. CE
6、N 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 such national standards may be obtained on app
7、lication 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 M
8、anagement 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, La
9、tvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey andUnited Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Mar
10、nix 17, B-1000 Brussels 2015 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4710-07:2015 EBS EN 4710-07:2015EN 4710-07:2015 (E) 2 Contents Page European foreword . 3 1 Scope 4 2 Normative references 4 3 Requirements . 5 4 Designat
11、ion 6 5 Marking . 6 6 Technical specification 7 BS EN 4710-07:2015EN 4710-07:2015 (E) 3 European foreword This document (EN 4710-07:2015) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance
12、with the rules of this Association, this European 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
13、 of an identical text or by endorsement, at the latest by April 2016, and conflicting national standards shall be withdrawn at the latest by April 2016. 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
14、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, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, E
15、stonia, 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, Switzerland, Turkey and the United Kingdom. BS EN 4710-07:2015EN
16、 4710-07:2015 (E) 4 1 Scope This European Standard specifies the dimensions, mass and tolerances of the retaining grommet for use in fuselage interior equipment and non-structural or secondary structural area. This European Standard is to be used in conjunction with EN 4710-06 as described in EN 471
17、0-02. The applicable temperature range is -55 C to 85 C. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (incl
18、uding any amendments) applies. EN 2424, Aerospace series Marking of aerospace products EN 4710-01, Aerospace series Quick release fastening systems for non-structural applications Part 01: Technical specification EN 4710-02, Aerospace series Quick release fastening systems for non-structural applica
19、tions Part 02: Spring clamp stud combination EN 4710-06, Aerospace series Quick release fastening systems for non-structural applications Part 06: Stud - quick-release and locking EN 22768-1:1993, General tolerances Part 1: Tolerances for linear and angular dimensions without individual tolerance in
20、dications (ISO 2768-1:1989) EN 22768-2:1993, General tolerances Part 2: Geometrical tolerances for features without individual tolerance indications (ISO 2768-2:1989) BS EN 4710-07:2015EN 4710-07:2015 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration, dimensio
21、ns, tolerances and mass shall conform to Figure 1 and Table 1. Tolerances not specified, shall be in accordance with ISO 2768-mK (EN 22768-1:1993 and EN 22768-2:1993). Dimensions are unless otherwise specified per manufacturers option. Figure 1 Configuration grommet Rx Table 1 Dimensions and mass Di
22、mensions in millimetres Type code Length code a D d l Mass Approximate g RS 05 6,0 2,4 0,5 0,02 12 1,2 0,03 17 1,7 0,05 25 2,5 0,07 32 3,2 0,08 48 4,8 0,15 RM 17 9,5 4,0 1,7 0,12 25 2,5 0,20 40 4,0 0,28 50 5,0 0,38 60 6,0 0,48 RL 17 13,0 5,5 1,7 0,25 25 2,5 0,35 40 4,0 0,60 56 5,6 0,90 80 8,0 1,20 a
23、See “l” in 1/10 mm. BS EN 4710-07:2015EN 4710-07:2015 (E) 6 3.2 Material Material shall be in accordance with the Table 2. Table 2 Material and hardness Material code Material Hardness A Silicone 60 5 IHDC Shore A The silicone shall not have a live limit. 4 Designation EXAMPLE Description block RETA
24、INING GROMMET Identity block EN4710-07RM17A Number of the basic standard Standard family number Type code (see Table 1) Length code (see Table 1) Material code (see Table 2) 5 Marking EN 2424, style G. BS EN 4710-07:2015EN 4710-07:2015 (E) 7 6 Technical specification Required tests for acceptance an
25、d qualification shall be in accordance to Table 3. Table 3 Requirements, inspections and tests Characteristic Requirements Requirements as per EN 4710-01 Inspections and tests as per EN 4710-01 A aQ bMaterials In accordance with Table 2. 4.1 5.4.1 X X Dimensions and masses In accordance with Table 1
26、. 4.2 5.4.2 X X Surface defects Refer to EN 4710-01. 4.3.1 5.4.3.1 X X Burning behaviour Refer to EN 4710-01. 4.6.1 5.4.6.1 X Functionality Refer to EN 4710-01. 4.7.1 5.4.7.1 X Identification marking of the package Refer to EN 4710-01. 4.8.2 5.4.8.2 X X aAcceptance test. bQualification test. This pa
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