BS EN 4710-05-2015 Aerospace series Quick release fastening systems for non-structural applications Spring clamp Two ways tolerance compensation《航空航天系列 非结构性应用的快速释放紧固系统 弹簧夹 双向公差补偿》.pdf
《BS EN 4710-05-2015 Aerospace series Quick release fastening systems for non-structural applications Spring clamp Two ways tolerance compensation《航空航天系列 非结构性应用的快速释放紧固系统 弹簧夹 双向公差补偿》.pdf》由会员分享,可在线阅读,更多相关《BS EN 4710-05-2015 Aerospace series Quick release fastening systems for non-structural applications Spring clamp Two ways tolerance compensation《航空航天系列 非结构性应用的快速释放紧固系统 弹簧夹 双向公差补偿》.pdf(12页珍藏版)》请在麦多课文档分享上搜索。
1、BSI Standards PublicationBS EN 4710-05:2015Aerospace 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 05: Spring clamp Two waystolerance compensationBS EN 4710-05:2015 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN
2、4710-05:2015.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 necessarypr
3、ovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2015. Published by BSI Standards Limited 2015ISBN 978 0 580 89134 2ICS 49.035Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published
4、 under the authority 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 4710-05:2015EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4710-05 October 2015 ICS 49.035 English Version Aerospace series - Qu
5、ick release fastening systems for non-structural applications - Part 05: Spring clamp - Two ways tolerance compensation Srie arospatiale - Fixations rapides filetes pour applications non-structurales - Partie 05 : Collier lyre -Deux degrs de libert Luft- und Raumfahrt - Schnellverschlsse fr nicht-st
6、rukturelle Anwendungen - Teil 05: Federclip - Zweifacher Toleranzausgleich 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 s
7、tandard without any alteration. 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 i
8、n any other language made by 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
9、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, Switzerland, Turkey andUnited Kingdom. EUROP
10、EAN COMMITTEE FOR STANDARDIZATION 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 4710-05:2015 EBS
11、EN 4710-05:2015EN 4710-05:2015 (E) 2 Contents Page European foreword . 3 1 Scope 4 2 Normative references 4 3 Requirements . 4 4 Designation 6 5 Marking . 6 6 Technical specification 7 BS EN 4710-05:2015EN 4710-05:2015 (E) 3 European foreword This document (EN 4710-05:2015) has been prepared by the
12、Aerospace and Defence Industries 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
13、 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 the latest by April 2016, and conflicting national standards shall be withdrawn at the latest by April 2016. Attention
14、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 all such patent rights. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the f
15、ollowing countries are bound 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, Netherland
16、s, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 4710-05:2015EN 4710-05:2015 (E) 4 1 Scope This European Standard specifies the dimensions, mass, tolerances and static values of catch spring for use in fuselage interior equipm
17、ent and non-structural or secondary structural area. This European Standard is to be used in conjunction with EN 4710-06 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 indispensable for the a
18、pplication 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 of corrosion resi
19、sting 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: Spring clamp stud
20、combination EN 4710-06, Aerospace series Quick release fastening systems for non-structural applications Part 06: Stud - quick-release and locking EN 4710-07, Aerospace series Quick release fastening systems for non-structural applications Part 07: Retaining grommet EN 10132-4, Cold rolled narrow st
21、eel strip for heat treatment Technical delivery conditions Part 4: Spring steels and other applications EN 10151, Stainless steel strip for springs Technical delivery conditions EN 22768-1:1993, General tolerances Part 1: Tolerances for linear and angular dimensions without individual tolerance indi
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