1、BSI Standards PublicationBS EN 4710-06:2015Aerospace series Quickr e l e a s e f a s t e n i n g s y s t e m s f o rnon-structural applicationsPart 06: Stud quick-release and lockingBS EN 4710-06:2015 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 4710-06:2015.
2、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.This publication does not purport to include all the necessaryprovisions of a
3、 contract. Users are responsible for its correctapplication. The British Standards Institution 2015.Published by BSI Standards Limited 2015ISBN 978 0 580 89135 9ICS 49.035Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the aut
4、hority of theStandards Policy and Strategy Committee on 31 October 2015.Amendments/corrigenda issued since publicationDate T e x t a f f e c t e dBS EN 4710-06:2015EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4710-06 October 2015 ICS 49.035 English Version Aerospace series - Quick release fa
5、stening systems for non-structural applications - Part 06: Stud - quick-release and locking Srie arospatiale - Fixations rapides filetes pour applications non-structurales - Partie 06 : Pion dmontage et verrouillage rapide Luft- und Raumfahrt - Schnellverschlsse fr nicht-strukturelle Anwendungen - T
6、eil 06: Bolzen - Schnell auslsend und schlieend This European Standard was approved by CEN on 5 March 2015. 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 alterat
7、ion. Up-to-date lists and bibliographical references concerning 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 b
8、y translation under the responsibility of a CEN member into its 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,
9、 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 United Kingdom. EUROPEAN COMMITTEE FOR STANDARD
10、IZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 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 4710-06:2015 EBS EN 4710-06:2015EN 4710-06:
11、2015 (E) 2 Contents Page European foreword . 3 1 Scope 4 2 Normative references 4 3 Requirements . 5 4 Designation 8 5 Marking . 9 6 Technical specification 9 BS EN 4710-06:2015EN 4710-06:2015 (E) 3 European foreword This document (EN 4710-06:2015) has been prepared by the Aerospace and Defence Indu
12、stries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance 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 pres
13、entation 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 the latest by April 2016, and conflicting national standards shall be withdrawn at the latest by April 2016. Attention is drawn to the possibilit
14、y 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 all such patent rights. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bou
15、nd to implement this 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, Portuga
16、l, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 4710-06:2015EN 4710-06:2015 (E) 4 1 Scope This European Standard specifies the dimensions, mass, tolerances and static values of stud - quick-release and locking for use in fuselage interior equipment an
17、d non-structural or secondary structural area. This European Standard is to be used in conjunction with EN 4710-03, EN 4710-04, EN 4710-05 and EN 4710-07 as described in EN 4710-02. The applicable temperature range is -55 C to 85 C. 2 Normative references The following referenced documents are indis
18、pensable for the application of this document. 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 products EN 2516, Aerospace series Passivation
19、 of corrosion resisting steels and decontamination of nickel base alloys EN 4710-01, Aerospace series Quick release fastening systems for non-structural applications Part 01: Technical specificationEN 4710-02, Aerospace series Quick release fastening systems for non-structural applications Part 02:
20、Spring clamp stud combination EN 4710-03, Aerospace series Quick release fastening systems for non-structural applications Part 03: Spring clamp EN 4710-04, Aerospace series Quick release fastening systems for non-structural applications Part 04: Spring clamp One way tolerance compensation EN 4710-0
21、5, Aerospace series Quick release fastening systems for non-structural applications Part 05: Spring clamp Two ways tolerance compensation EN 4710-07, Aerospace series Quick release fastening systems for non-structural applications Part 07: Retaining grommet EN 10088-3, Stainless steels Part 3: Techn
22、ical delivery conditions for semi-finished products, bars, rods, wire, sections and bright products of corrosion resisting steels for general purposes EN 12165, Copper and copper alloys Wrought and unwrought forging stock EN 22768-1:1993, General tolerances Part 1: Tolerances for linear and angular
23、dimensions without individual tolerance indications (ISO 2768-1:1989) EN 22768-2:1993, General tolerances Part 2: Geometrical tolerances for features without individual tolerance indications (ISO 2768-2:1989) EN ISO 1456, Metallic and other inorganic coatings Electrodeposited coatings of nickel, nic
24、kel plus chromium, copper plus nickel and of copper plus nickel plus chromium (ISO 1456) BS EN 4710-06:2015EN 4710-06:2015 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration, dimensions, tolerances and mass shall conform to Figure 1 and Table 1. Tolerances not
25、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 pin Px BS EN 4710-06:2015EN 4710-06:2015 (E) 6 Figure 2 shows an example of installation of EN 4710-06 (1), EN 4710-07
26、(2) and EN 4710-03 to EN 4710-05 (3). H shows the maximum thickness of parts assembled with the used pin. Key 1 Stud as per EN 4710-06 (1) 2 Grommet as per EN 4710-07 (2) 3 Spring Clamp as per EN 4710-03 to EN 4710-05 (3) Figure 2 Grip range H BS EN 4710-06:2015EN 4710-06:2015 (E) 7 Table 1 Dimensio
27、ns and mass Dimensions in millimetres Type code Length code b D1 D2 D3 h1h2l1 l2 l3 H r1 r2 r3 Mass Approx. + 0,1 0 0 0,1 0,1 0,1 max. min. g PS 020 1,0 8,0 2,6 3,9 2,2 1,0 11,2 7,9 9,3 2,9 1,0 0,5 0,1 1,4 025 11,6 9,7 3,3 1,4 030 12,2 10,3 3,9 1,4 035 12,6 10,7 4,3 1,4 040 13,0 11,1 4,7 1,5 045 13,
28、4 11,5 5,1 1,5 050 13,9 12,0 5,6 1,5 060 15,0 13,1 6,7 1,6 070 16,0 14,1 7,7 1,6 080 17,2 15,3 8,9 1,7 090 18,2 16,3 9,9 1,7 100 19,2 17,3 10,9 1,8 120 21,2 19,3 12,9 1,9 PM 020 1,5 11,0 4,5 6,3 2,4 1,0 15,6 11,9 13,4 3,3 1,6 1,0 3,9 030 16,6 14,4 4,3 4,0 040 17,6 15,4 5,3 4,2 050 18,6 16,4 6,3 4,4
29、060 19,8 17,6 7,5 4,6 070 20,6 18,4 8,3 4,7 080 21,8 19,6 9,5 4,8 090 22,6 20,4 10,3 4,9 100 23,6 21,4 11,3 5,0 110 24,6 22,4 12,3 5,2 120 25,8 23,6 13,5 5,4 130 26,8 24,6 14,5 5,6 140 27,6 25,4 15,3 5,9 160 29,6 27,4 17,3 6,0 180 31,6 29,4 19,3 6,2 200 33,8 31,6 21,5 6,5 220 35,6 33,4 23,3 6,8 PL 0
30、40 2,0 16,0 6,5 9,4 3,3 1,5 22,2 15,7 18,4 6,1 2,5 1,5 10,9 050 23,2 19,4 7,1 11,2 060 24,2 20,4 8,1 11,5 080 26,2 22,4 10,1 12,1 100 28,1 24,3 12,0 12,7 120 30,1 26,3 14,0 13,3 140 32,4 28,6 16,3 13,9 160 34,1 30,3 18,0 14,5 180 36,0 32,2 19,9 15,1 200 38,1 34,3 22,0 15,7 BS EN 4710-06:2015EN 4710-
31、06:2015 (E) 8 3.2 Mechanical characteristics Ultimate loads, see Table 2. Table 2 Loads Type code Ultimate tensile loads Ultimate shear loads Push-in loads Torque-out Material code N N N max. N cm PS 500 300 30 5 - 15 C B PM 900 600 30 5 - 15 C B PL 2 000 1 500 80 30 - 50 C B 3.3 Material and surfac
32、e treatment Materials and finished shall be in accordance with the Table 3. Table 3 Materials and surface treatment Material code Material Surface treatment C Stainless steel 1.4301 per EN 10088-3 Passivated per EN 2516 B CuZn39Pb3 or CuZn39Pb2 per EN 12165 Electrodeposited coatings per EN ISO 1456
33、4 Designation EXAMPLE Description block STUD - QUICK RELEASE AND LOCKING Identity block EN4710-06PM080C Number of the basic standard Standard family number Type code (see Table 1) Length code (see Table 1) Material code (see Table 3) BS EN 4710-06:2015EN 4710-06:2015 (E) 9 5 Marking EN 2424, style F
34、. 6 Technical specification Required tests for acceptance and qualification shall be in accordance to Table 4. Table 4 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 3. 4.
35、1 5.4.1 X X Dimensions and masses In accordance with Table 1. 4.2 5.4.2 X X Surface defects Refer to EN 4710-01. 4.3.1 5.4.3.1 X X Surface treatment In accordance with Table 3. 4.3.2 5.4.3.2 X X Ultimate tensile loads In accordance with Table 2. 4.4.1 5.4.4.1 X Ultimate shear loads In accordance wit
36、h Table 2. 4.4.2 5.4.4.2 X Push-in load In accordance with Table 2. 4.4.3 5.4.4.3 X Torque-out In accordance with Table 2. 4.4.4 5.4.4.4 X Corrosion resistance Refer to EN 4710-01. 4.5 5.4.5 X Functionality Refer to EN 4710-01. 4.7.1 5.4.7.1 X Endurance Material code C per Table 3: 500 cycles. Mater
37、ial code B per Table 3: 1 500 cycles. 4.7.2 5.4.7.2 X Identification marking of the product Refer to EN 4710-01. 4.8.1 5.4.8.1 X 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 page deliberately left blankThis page deliberate
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