EN 3730-2009 en Aerospace series - Clamps saddle fixed and sliding version in aluminium alloy with rubber cushioning - Dimension masses《航空航天系列 鞍座形 带橡胶弹性垫料的铝合金的固定式滑动型夹件 尺寸 质量》.pdf
《EN 3730-2009 en Aerospace series - Clamps saddle fixed and sliding version in aluminium alloy with rubber cushioning - Dimension masses《航空航天系列 鞍座形 带橡胶弹性垫料的铝合金的固定式滑动型夹件 尺寸 质量》.pdf》由会员分享,可在线阅读,更多相关《EN 3730-2009 en Aerospace series - Clamps saddle fixed and sliding version in aluminium alloy with rubber cushioning - Dimension masses《航空航天系列 鞍座形 带橡胶弹性垫料的铝合金的固定式滑动型夹件 尺寸 质量》.pdf(16页珍藏版)》请在麦多课文档分享上搜索。
1、BSEN3730:2009ICS49.080NOCOPYINGWITHOUTBSIPERMISSIONEXCEPTASPERMITTEDBY COPYRIGHTLAWBRITISHSTANDARDAerospaceseriesClamps,saddlefixedandslidingversioninaluminiumalloywithrubbercushioningDimension,massesThis British Standardwas publishedunderthe authority of theStandards PolicyandStrategy Committee on
2、30November2009.BSI 2009ISBN9780580677106Amendments/corrigendaissuedsincepublicationDate CommentsBSEN3730:2009NationalforewordThis BritishStandardisthe UK implementation of EN 3730:2009.Itsupersedes BS EN 3730:2001 which is withdrawn.The UK participation in its preparation was entrustedtoTechnicalCom
3、mittee ACE/6, Aerospace avionic electrical and fibreoptictechnology.Alist of organizationsrepresented on thiscommittee canbeobtained onrequest to its secretary.This publication does not purport to include all the necessary provisionsof acontract. Users areresponsible for itscorrect application.Compl
4、iancewithaBritishStandardcannotconferimmunityfromlegalobligations.BS EN 3730:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORMEN 3730 September 2009 ICS 49.080 Supersedes EN 3730:2001English Version Aerospace series - Clamps, saddle fixed and sliding version in aluminium alloy with rubber cushio
5、ning - Dimension, masses Srie arospatiale - Colliers du type Omga avec serrage ou coulissants en alliage daluminium avec profil en lastomre - Dimensions, massesLuft- und Raumfahrt - Schellen in Sattelform ausaluminiumlefierung mit Profilgummi fr feste und gleitende Rohrhalterung - Mae, Massen This E
6、uropean Standard was approved by CEN on 1 July 2009.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-date lists and bibliographical references con
7、cerning such nationalstandards may be obtained on application to the CEN 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 ow
8、n language and notified to the CEN Management Centre has the same status as the official versions.CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuani
9、a, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All
10、rights of exploitation in any form and by any means reserved worldwide for CEN national Members.Ref. No. EN 3730:2009: EBS EN 3730:2009EN 3730:2009 (E)2 Contents PageForeword 31Scope 42Normative references43Required characteristics.44Designation 95Marking 116Technical specification 12BS EN 3730:2009
11、EN 3730:2009 (E)3 Foreword This document (EN 3730:2009) has been prepared bythe Aerospace and Defenc e Industries Association ofEurope - Standardization (ASD-STAN). After enquiriesand votes carried out in accordancewiththe rules of this Association, this Standard has received the approval of the Nat
12、ional 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 of an identical textorbyendorsement, at the latest by March 2010, and conflicting nationalstanda
13、rds shall be withdrawn atthe latest by March 2010.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 be held responsible for identifying any orall such patent rights. This document supersedes EN 3730:2001
14、.According to the CEN/CENELEC Internal Regulations, the national standards organizations of the followingcountriesare bound to implement this European Standard: Austria,Belgium, Bulgaria, Cyprus, CzechRepublic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary , Iceland, Ireland, Italy, La
15、tvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain,Sweden, Switzerland and the UnitedKingdom. BS EN 3730:2009EN 3730:2009 (E)4 1 ScopeThis standard specifies the required characteristics of saddle clamps in aluminium alloywith various cushio
16、nmaterials.These clamps, fixed version (typ e 1) or sliding version (type 2) , are used for supporting pipe assemblies.They are used up to 80 C max.Usage at a higher temperature is at the option of the user. For temperature range and environmental considerations see the various cushion material stan
17、dards.2 NormativereferencesThe following referenced documents are indispensable for the application of this document. For datedreferences, only the edition cited applies. For undated references, the latest edition of the referenceddocument (including any amendments) applies.EN 2261, Aerospace series
18、 Silicone rubber (VMQ) Hardness 70 IRHD.EN 2424, Aerospace series Marking of aerospace products. EN 2437, Aerospace series Chromate conversion coatings (yellow) for aluminium and aluminium alloys.EN 2566, Aerospace series Fluorocarbon rubber (FPM) Hardness 70 IRHD. 1)EN 2693, Aerospaceseries Alumini
19、um alloy AL-P5086- H111 Sheet and strip 0,3 mm a 6 mm.EN 3078, Aerospace series P, Q and saddle clamps with rubber cushion Technical specification. 1)EN 3825, Aerospace series Fluorosilicone rubber (FVMQ) Hardness 60 IRHD. 1)EN 3826, Aerospace series Fluorosilicone rubber (FVMQ) Hardness 70 IRHD. 1)
20、EN 4115, Aerospace series Cushion, rubber for clamps Dimensions, masses . 3 Required characteristics3.1 Materials According to Table 1.Clamp: Aluminium alloy according to EN 2693.Cushion: According to EN 4115.1) Published as ASD Prestandard at the date of publication of this standard.BS EN 3730:2009
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