BS EN 4408-4-2005 Aerospace series - Technical drawings - Representation of parts made of composite materials - Items obtained by winding《航空航天系列 技术制图 复合材料制部件的表示法 缠绕式产品》.pdf

《BS EN 4408-4-2005 Aerospace series - Technical drawings - Representation of parts made of composite materials - Items obtained by winding《航空航天系列 技术制图 复合材料制部件的表示法 缠绕式产品》.pdf》由会员分享，可在线阅读，更多相关《BS EN 4408-4-2005 Aerospace series - Technical drawings - Representation of parts made of composite materials - Items obtained by winding《航空航天系列 技术制图 复合材料制部件的表示法 缠绕式产品》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、 g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58materials Part 4: Items obtained by windingThe European Standard EN 4408-4:2005 has the status of a

2、 British StandardICS 01.100.99; 49.020Technical drawings Representation of parts made of composite BRITISH STANDARD AEROSPACE SERIESBS EN 4408-4:2005BS EN 4408-4:2005This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 October 2005 BSI 31 Octob

3、er 2005ISBN 0 580 46481 4A list of organizations represented on this subcommittee can be obtained on request to its secretary.Cross-referencesThe British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section

4、entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue or of British Standards Online.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Complia

5、nce with a British Standard does not of itself confer immunity from legal obligations.Summary of pagesThis document comprises a front cover, an inside front cover, the EN title page, pages 2 to 9 and a back cover.The BSI copyright notice displayed in this document indicates when the document was las

6、t issued.Amendments issued since publicationAmd. No. Date Comments aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep UK interests informed; monitor related international and Europea

7、n developments and promulgate them in the UK.National forewordThis British Standard is the official English language version of EN 4408-4:2005. The UK participation in its preparation was entrusted by Technical Committee ACE/65, Non-metallic materials for aerospace purposes (excluding textiles), to

8、Subcommittee ACE/65/-/64, Structural reinforced plastics, which has the responsibility to:EUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 4408-004May 2005ICS 01.100.99; 49.020English versionAerospace series - Technical drawings - Representation of partsmade of composite materials - Part 4: Items o

9、btained by windingSrie arospatiale - Dessins techniques - Reprsentationdes articles en matriaux composites - Partie 4 : Articlesobtenus par enroulementLuft- und Raumfahrt - Technische Zeichnungen -Darstellung von Teilen aus Verbundwerkstoffen - Teil 4: ImWickelverfahren hergestellte TeileThis Europe

10、an Standard was approved by CEN on 15 July 2004.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerni

11、ng such nationalstandards may be obtained on application to the Central Secretariat or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any other language made by translationunder the responsibility of a CEN member into its own langua

12、ge and notified to the Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta,

13、 Netherlands, Norway, Poland, Portugal, Slovakia,Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 2005 CEN All rights of exploitation in any

14、 form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4408-004:2005: E2 Contents Page Foreword 3 Introduction4 1 Scope .5 2 Normative references .5 3 Terms and definitions.5 4 Presentation on drawings 6 4.1 General rules.6 4.2 Specific rules.6 4.2.1 Symbol.6 4.2.2 Winding of

15、filaments.6 4.2.3 Winding of plies 8 Bibliography.9 EN 4408-4:20053 Foreword This document (EN 4408-004:2005) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance with the rules of this Associatio

16、n, this Standard has received the approval of the National Associations and the Official Services of the member countries of AECMA, 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,

17、 at the latest by November 2005, and conflicting national standards shall be withdrawn at the latest by November 2005. 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 identifyin

18、g 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, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Ic

19、eland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4408-4:20054 Introduction The proposed representations only provide the definition of parts made up of cylinders, i.e. surface

20、s created by a straight (generator) line which moves while remaining parallel to a given direction, along a (directing) curve. These representations are insufficient to describe parts especially including truncated cones, cores or elliptic bottoms. This standard is intended: for items obtained by wi

21、nding helicoidal filaments of a basic yarn; for items obtained by winding plies (or layers). EN 4408-4:20055 1 Scope This standard specifies the rules for the representation of items in composite materials obtained by winding as well as the information to be indicated in technical drawings. It is ap

22、plicable to aerospace structures using items in composite materials obtained by winding. It shall be used together with EN 4408-001. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies.

23、 For undated references, the latest edition of the referenced document (including any amendments) applies. EN 4408-001, Aerospace series Technical drawings Representation of parts made of composite materials Part 1: General rules. EN 4408-002, Aerospace series Technical drawings Representation of pa

24、rts made of composite materials Part 2: Laminated parts. 3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 4408-001 and the following apply. 3.1 angle of the spiral angle formed by the basic yarn, or the laid ply, and the 0 direction of the direction ke

25、y (this 0 direction corresponds to the direction of the cylinders axis in the case of rotational parts) 3.2 lap set of fibres and/or filaments and/or yarns and/or fibrillated laminates arranged in an orderly manner or not, sufficiently cohesive to ensure easy handling and a slight thickness with res

26、pect to other dimensions. 3.3 layer in the winding of filaments, the layer is specifically defined as being made up of the smallest whole number of winding motives such that the surface described is entirely covered 3.4 spiral pitch axial advance of the yarn or ply lay device corresponding to a whol

27、e turn of the part 3.5 tape preimpreg fibrous composite supplied in different widths the fibres of which are arranged in an unidirectional manner lengthways 3.6 to-and-fro by winding filaments, elementary figure made up of two spirals of opposite pitches EN 4408-4:20056 A to-and fro corresponds to t

28、wo consecutive “passes“ and in the opposite direction by the yarn laying device. 3.7 lay width distance between two adjacent yarns or laps or plies, measured perpendicularly at their axes 3.8 winding symbol means that the ply in question is obtained by winding 3.9 winding motive figure described by

29、the smallest whole number of to-and-fro movements such that a symmetry appears with respect to the axis in the winding of the filaments 4 Presentation on drawings 4.1 General rules The general rules for the representation of items in composite materials obtained by winding shall be in conformity wit

30、h EN 4408-001. The representation rules described in EN 4408-002 remain applicable for items obtained by winding (stratification table, direction key, symbolisation of direction in the stratification table, etc.). 4.2 Specific rules 4.2.1 Symbol Winding is symbolised in the stratification table by t

31、he symbol . This symbol appears in the stratification table and shall be accompanied by a note defining the basic material used for winding (yarn, rough roving, tape, fabric). 4.2.2 Winding of filaments See Figure 1 and Figure 2. In the case of items obtained by the helicodal filamentary winding of

32、a basic thread, the drawing does not represent the section of the thread. EN 4408-4:20057 Key 1 Layer end side 136 and 141 (see Figure 2) Figure 1 Dimensions in millimetres 1-3 141 90 0,375 2 ROUGH ROVINGS 1-3 136 90 0,375 2 ROUGH ROVINGS 1 131 90 0,375 2 ROUGH ROVINGS 2 126 45 0,31 2 121 0 0,31 1 1

33、16 V V 261,3261,3V1V1130,63 ROUGH ROVINGS 3 WINDING END1/3NUMBER OF TO-and-FROs = 29 2 111 0 0,31 2 106 0 0,31 1 101 90 0,375 2 ROUGH ROVINGS A1 A2 A3 A4 FABRIC LAP YARN AREA THICKNESS NOTE ELEMENTIDENTIFICATION DIRECTIONTHICKNESS 4,042,80V 0,975 Key = winding V = variable in the area 1 = carbon fib

34、re 2 = bi-directional fabric V1= see file N XXXXXXX 3 = for layers 136 and 141, make a dead stop once at the stop mark. Figure 2 WARP 0 EN 4408-4:20058 4.2.3 Winding of plies See Figure 3 and Figure 4. In the case of items obtained by winding plies: the drawing differentiates the laid elementary wid

35、ths; the representation rules are similar to those for draped items, provided that certain plies which appear to be distinct on a cross section according to a generator, come in fact from single wound plies. Two cases are to be differentiated: Circumferential or spiral winding; the number of winding

36、 turns shall figure: either in a note, or be entirely represented on the drawing, Helical winding: the stratification table indicates as usual the angle of the plys reference direction in relation to the 0 direction of the direction key of the part, and winding is defined on the drawing with respect

37、 to its spiral angle, or its spiral pitch, or its lay pitch. It may be useful to mark on the drawing the point at which the spiral starts. NOTE Plies are generally cut out parallel to their reference direction and the spiral angle corresponds to the angle figuring in the stratification table. Dimens

38、ions in millimetres Figure 3 Dimensions in millimetres 1111 790,3 2106 790,3 1101 790,3 A1 FABRIC LAP AREA THICKNESS WINDING NOTE LAYER IDENTIFICATION DIRECTIONTHICKNESS 1 Figure 4 EN 4408-4:20059 Bibliography 1 EN 4408-003, Aerospace series Technical drawings Representation of parts made of composi

39、te materials Part 3: Parts including core materials. 2 EN 4408-005, Aerospace series Technical drawings Representation of parts made of composite materials Part 5: Seams. 3 EN 4408-006, Aerospace series Technical drawings Representation of parts made of composite materials Part 6: Preforms. EN 4408-

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