BS EN 4710-02-2015 Aerospace series Quick release fastening systems for non-structural applications Spring clamp stud combination《航空航天系列 非结构性应用的快速释放紧固系统 弹簧夹螺柱组合》.pdf

《BS EN 4710-02-2015 Aerospace series Quick release fastening systems for non-structural applications Spring clamp stud combination《航空航天系列 非结构性应用的快速释放紧固系统 弹簧夹螺柱组合》.pdf》由会员分享，可在线阅读，更多相关《BS EN 4710-02-2015 Aerospace series Quick release fastening systems for non-structural applications Spring clamp stud combination《航空航天系列 非结构性应用的快速释放紧固系统 弹簧夹螺柱组合》.pdf（10页珍藏版）》请在麦多课文档分享上搜索。

1、BSI Standards PublicationBS EN 4710-02:2015Aerospace series Quick r e l e a s e f a s t e n i n g s y s t e m s f o r non-structural applicationsPart 02: Spring clamp stud combinationBS EN 4710-02:2015 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 4710-02:2015

2、.The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions

3、of a contract. Users are responsible for its correct application. The British Standards Institution 2015. Published by BSI Standards Limited 2015ISBN 978 0 580 89131 1 ICS 49.035 Compliance with a British Standard cannot confer immunity from legal obligations.This British Standard was published unde

4、r the authority of the Standards Policy and Strategy Committee on 31 October 2015.Amendments issued since publicationDate T e x t a f f e c t e dBS EN 4710-02:2015EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4710-02 October 2015 ICS 49.035 English Version Aerospace series - Quick release fas

5、tening systems for non-structural applications - Part 02: Spring clamp stud combination Srie arospatiale - Fixations rapides filetes pour applications non-structurales - Partie 02 : Combinaison de colliers lyre et pions Luft- und Raumfahrt - Schnellverschlsse fr nicht-strukturelle Anwendungen - Teil

6、 02: Federclip-Bolzen-Kombination 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 alteration. Up-to-dat

7、e 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 by translation

8、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, Finland, Form

9、er 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 STANDARDIZATION COMIT

10、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 4710-02:2015 EBS EN 4710-02:2015EN 4710-02:2015 (E) 2 Con

11、tents Page European foreword . 3 1 Scope 4 2 Normative references 4 3 Representations 4 4 Example of installation . 6 BS EN 4710-02:2015EN 4710-02:2015 (E) 3 European foreword This document (EN 4710-02:2015) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardiz

12、ation (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 presentation to CEN. This European Standard s

13、hall 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 possibility that some of the elements of this docum

14、ent 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 bound to implement this European Standard: A

15、ustria, 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, Portugal, Romania, Slovakia, Slovenia, Spain, Sw

16、eden, Switzerland, Turkey and the United Kingdom. BS EN 4710-02:2015EN 4710-02:2015 (E) 4 1 Scope This European Standard describes the compilation of the component system the spring clamp pin family for use in the fuselage interior equipment and in the not structural or secondary structural area for

17、 aerospace applications. 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 docu

18、ment (including any amendments) applies. EN 4710-01, Aerospace series Quick release fastening systems for non-structural applications Part 01: Technical specification EN 4710-03, Aerospace series Quick release fastening systems for non-structural applications Part 03: Spring clamp EN 4710-04, Aerosp

19、ace series Quick release fastening systems for non-structural applications Part 04: Spring clamp One way tolerance compensationEN 4710-05, Aerospace series Quick release fastening systems for non-structural applications Part 05: Spring clamp Two ways tolerance compensationEN 4710-06, Aerospace serie

20、s Quick release fastening systems for non-structural applications Part 06: Stud - quick-release and lockingEN 4710-07, Aerospace series Quick release fastening systems for non-structural applications Part 07: Retaining grommetEN 10088-3, Stainless steels Part 3: Technical delivery conditions for sem

21、i-finished products, bars, rods, wire, sections and bright products of corrosion resisting steels for general purposes EN 10132-4, Cold rolled narrow steel strip for heat-treatment Technical delivery conditions Part 4: Spring steels and other applicationsEN 10151, Stainless steel strip for springs T

22、echnical delivery conditions EN 12165, Copper and copper alloys Wrought and unwrought forging stock 3 Representations Table 1 shows the different components of the quick release fastening systems for non-structural and lining applications including the different family numbers of the standard EN 471

23、0-03 to EN 4710-07. EN 4710-01 is reserved for the technical specification of the system. BS EN 4710-02:2015EN 4710-02:2015 (E) 5 Table 1 Types EN 4710- Figure Description Type Type code aPlate codes Material code 03 Spring Clamp CS CM CL 3 4 5 A = Alloy steel per EN 10132-4 S = Stainless steel per

24、EN 10151 Fixed shift none 04 Spring Clamp Tolerance compensation Direction CTS CTM 3 4 A = Alloy steel per EN 10132-4 S = Stainless steel per EN 10151 shift (left-right) 05 Spring Clamp Tolerance compensation Direction CSM 5 A = Alloy steel per EN 10132-4 S = Stainless steel per EN 10151 shift (left

25、-right- up-down) 06 Stud quick release and locking PS PM PL C = Stainless steel per EN 10088-3 B = Copper alloy per EN 12165 turning 07 Grommet RS RM RL A = Silicone aOnly type code with the same end letter can be combined. Possible combinations are given through the type code small (xS), medium (xM

26、) and large (xL). A sample of the CM/CSM/CTM, PM and RM combination can be found in Clause 4. BS EN 4710-02:2015EN 4710-02:2015 (E) 6 4 Example of installation Figure 1 shows an example of installation of EN 4710-06 (1), EN 4710-07 (2) and EN 4710-03 to EN 4710-05 (3). Example of possible end letter

27、 combinations: CM (3), CTM (3) and CSM (3) can be combined with PM (1) and RM (2) 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 1 Example of installation This page deliberately left blankBSI is the national body responsible

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