1、AECMA Technical Report Rapport Technique AECMA AECMA Fachbericht Edition approved for publication Extra copies can be supplied by B.N.A.E. Technopolis 54 - 199, rue Jean-Jacques Rousseau Non-metallic Material Domain 28June2002 92138 ISSY - LES - MOULINEAUX CEDEX - FRANCE TR 7000-1 O Edition I June 2
2、002 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION I AmnsTAa Gulledelle 94 - 6-1200 Brussels - Tel. + 32 2 775 81 10 - Fax. + 32 2 775 81 11 - www.aecrna-stan.org Supersedes prEN 7000-1 O Edition PI September 1998 Descriptors: ENGLISH VERSION Aerospace series Non-met
3、allic materials Rules for the drafting and presentation of material standards Part 1 O: Reinforcement fibres Srie arospatiale Luft- und Raumfahrt Matriaux non-mtalliques Nichtmetallische Werkstoffe Rgles pour la preparation et la presentation des normes de matriaux Partie 10 : Fibres de renfort Rege
4、ln fr die Erstellung und die Gestaltung von Werkstoffnormen Teil 1 O: Verstrkungsfasern This Technical Report was drawn up by the Non-metallic Material Domain of AECMA-STAN. The reason which led to the publication of the document as a Technical Report is explained in the foreword. Copyright Associat
5、ion Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 TR 7000-1 O: 06-02 Foreword The main task of AECMA-STAN is to prepare EN standards. In exceptional circumstances,
6、however, the publication of a Technical Report of one of the following types may be proposed : - type 1, the subject is still under technical development requiring wider exposure ; - type 2, a Technical Committee has collected data of a different kind from that which is normally published as a Europ
7、ean Standard. The Non-metallic Material Domain decided to publish this document in the form of a Technical Report of type 2 in order to facilitate the updating of this document. Contents Page O Introduction . 3 1 Scope . 3 2 Normative references . 3 Definitions, symbols and abbreviations 4 Rules for
8、 the drafting and presentation 3 Annex A (normative) Table AI - Characteristic numbers applicable to Table 1: General requirements 5 Annex B (normative) Table BI - Characteristic numbers applicable to Tables 2 to 4: Other requirements . 6 Annex C (informative) Example 7 Copyright Association Europee
9、ne des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 TR 7000-1 O: 06-02 O Introduction This standard is part of the series of TR non-metallic materials standards for aerospace ap
10、plications. The general organisation of this series is described in EN 4385. This document is a level 2 document as defined in EN 4385. It shall be used in conjunction with TR 7000-1, 1 Scope This standard specifies the rules for drafting and presentation of EN aerospace series non-metallic material
11、 standards for reinforcement fibres for aerospace applications. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed here
12、after. For dated references, subsequent amendments to or revisions of any of these publications apply to this European standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 4385 TR 7000-1 Aerospace series
13、- Non-metallic materials - General organisation of standardisation - Links between types of standards 1) Aerospace series - Non-metallic materials - Rules for the drafting and presentation of material standards - Part 1 : General rules 2) 3 Definitions, symbols and abbreviations See TR 7000-1 4 Rule
14、s for the drafting and presentation NOTE standardised EN products. Examples given below are only intended to illustrate the rules, and may not correspond to real 4.1 Title See TR 7000-1 and annex C of this standard. The following are examples of descriptions which shall be used; these exaples may be
15、 supplemented by other descriptions as required by the relevant WG. 1 Type of fibre - glass fibre - carbon fibre - aramid fibre - ceramic fibre 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published as AECMA Technical Report at the date of publication of this stan
16、dard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 TR 7000-1 O: 06-02 2 Linear density - no. of filaments - sizedlunsized - twist - nominal st
17、rength - nominal modulus - IS0 designation 4.2 Contents See TR 7000-1 and annex C of this standard. 4.3 Clause O: Onwards See TR 7000-1 and annex C of this standard. 4.4 General requirements See TR 7000-1 and annex C of this standard. 4.4.1 Table 1: General requirements The characteristic numbers ap
18、plicable to table 1 are given in annex A of this standard. All of the characteristics given in table 1 are mandatory and shall be completed in accordance with TR 7000-1 and annex C of this standard. 4.4.2 Tables 2 to 4 See TR 7000-1 and annex C of this standard. The characteristic numbers applicable
19、 to tables 2 to 4 are given in annex B of this standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 TR 7000-1 O: 06-02 1 .o01 1 .o02 Annex
20、A (norm at ive) Material description Formulation Table AI - Characteristic numbers applicable to Table I: General requirements 1 .O03 1 .O04 1 .O05 1 .O07 Characteristic number I Form and method of production Technical specification Grade Visual Characteristics 1 .o1 o 1 .o1 1 Storage Shelf life 1 .
21、O93 1 .O94 I 1 .o09 I Application and use Quality assurance certificate Designation 1.999 I 1 .O1 3 I Processing condition Notes I 1 .O95 I Packaging 1 .O96 Identification and marking I 1 .O98 I Health and safety Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by I
22、HS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 TR 7000-1 O: 06-02 Composition Density - size content - fibre density - linear density Annex B (normative) x X X Table BI - Characteristic numbers applicable to Tables 2 to 4: Other r
23、equirements Dry heat - oxydation resistance Notes Characteristic number X 012 104 301 305 313 503 999 Characteristic I Dimensional - filament diameter - twist Tensile properties - strength - modulus - elongation X X X Flexural shear - apparent ILSS Ix used in table(s) 314 X X X X X X X X lx Copyrigh
24、t Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 7 TR 7000-10: 06-02 Annex C (informative) Example Example C.l EN xxxx ENGLISH VERSION Aerospace series Non
25、-metallic materials Carbon filament yarn 4 O00 MPa nominal tensile strength 240 GPa nominal modulus Srie arospatiale Matriaux non-mtalliques Fil en fibre de carbone Rsistance nominale la traction de 4 O00 MPa Module nominal de 240 GPa Luft- und Raumfahrt Nichtmetallische Werkstoffe Kohlenstoffasern
26、4 O00 MPa Nenfestigkeit 240 GPa Nennmodul Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 8 TR 7000-10: 06-02 Example C.l (continued) Page 2 EN xx
27、xx Blank page Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 9 TR 7000-1 O: 06-02 Example C.l (continued) Page 3 EN xxxx O Introduction This stan
28、dard is part of the series of non-metallic material standards for aerospace applications. The general organisation of this series is described in EN 4385. This standard is a level 3 document as defined in EN 4385. It has been prepared in accordance with TR 7000-10. 1 Scope This standard specifies th
29、e requirements relating to a carbon filament yarn of 4 O00 MPa nominal tensile strength and 240 GPa nominal modulus for aerospace applications. 2 Normative references This European Standard incorporates by dated or undated reference, provisions from other publications. These normative references are
30、 cited at the appropriate places in the next and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest ed
31、ition of the publication referred to applies. IS0 13002 Carbon fibres - Designation system for filament yarns EN 2962 Aerospace series - Carbon fibre filament yarn (Polyacrylonitrile precursor) - Technical specification EN 4385 Aerospace series - Non-metallic materials - General organisation of stan
32、dardisation - Links between types of standard ) TR 7000-10 Aerospace series - Non-metallic materials - Rules for the drafting and presentation of material standards - Part 1 O: Reinforcement fibres ) 3 Definitions, symbols and abbreviations 3.1 Definitions 3.1.1 Sub-case numbering In the column requ
33、irement at the left hand side a sub-case number is given. The definition of these sub- case numbers is as follows: 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published as AECMA Technical Report at the date of publication of this standard Copyright Association Eu
34、ropeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 10 TR 7000-10: 06-02 Example C.1 (continued) Page 4 EN xxxx Sub-case number - 1 2 3 4 5 6 7 Definitions Technical specific
35、ation Test method Frequency of testing Sample type Test piece definition Conditioning of test piece Testing condition Acceptance criteria NOTE 1 The absence of a sub-case number indicates that the necessary information is given in table 1 of this standard, e.g. in the reference to the technical spec
36、ification (characteristic number 1.004). All the necessary information which does not appear is to be found in the referenced technical specification or the relevant test method. NOTE 2 In this material standard, batch acceptance test titles and sub-cases 7 acceptance criteria are highlighted in the
37、 form of a bold frame and bold characters to show that they are mandatory for routine acceptance of the material. 3.1.2 Other definitions See EN 2962. 3.2 Symbols and abbreviations See EN 2962. 4 Requirements The required characteristics are given in: Table 1 : General requirements Table 2: Requirem
38、ents in the delivery condition Table 3: Requirements as processed to characteristics number 1 .O13 Table 4: Environmental testing requirements as processed to characteristic number 1 .O13 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AEC
39、MANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 11 TR 7000-1 O: 06-02 1 .O04 1 .O05 Example C.1 (continued) Technical specification Grade Page 5 EN xxxx 200 400 Table 1 -General requirements 1200 Characteristics Characteristic number 1 1 .o09 1 .o1 o I 1 .o0
40、1 1 Material description Application and use Storage 1.002 I Formulation 1.01 I 1 .O1 3 1 .O03 Shelf life Processing condition Form and method of I production 1.999 Notes 1 .O07 I Visuai 1 .O93 Quality assurance certificate 1.094 1 Designation 1 .O96 Identification and marking 1 .O98 I Health and sa
41、fety Requirements Carbon fibre filament yarn Sized - polymeric size based on epoxy resin Carbon fibre - PAN precursor See EN 2962. Filament winding, fabric and preimpregnates See EN 2962. 2 24 m at ambient temperature Supplied in final condition of use See EN 2962. a See EN 2962. See EN 2962. _ See
42、safety data sheet. a This material corresponds to IS0 designation (adc correct designation here) as defined in IS0 13002 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without lic
43、ense from IHS-,-,-Page 12 TR 7000-10: 06-02 200 Example C.1 (continued) 400 1200 Page 6 EN xxxx 200 Table 2 - Requirements in the delivery condition 400 1200 Characteristic number + 2 to - 1 Characteristic O to 1,5 Oto1 Requirements 200 400 1 200 2.104 Size content grade I % Ihobbin i: 0,4 2.01 2 Tw
44、ist grade bobbin f 1 I O to 0,5 I O to 0,3 r 2.01 2 Filament diameter grade 2.301 200 I 4001 1200 Density grade glcm3 grade 1,78 f 0,06 2.301 182 - 214 368 - 425 750 - 850 t 192 - 208 382 - 413 775 - 825 Linear density bobbin grade 2.305 200 I 400 I 1200 Tensile properties MPa I Ebbin - 3 200 to 4 7
45、00 3 620 to 4 500 210 to 270 I GPa modulus lot 220 to 260 % elongation bobbin lot 2 1,2 2 1,45 2.31 3 Apparent ILSS grade 200 I 400 -1 1200 MPa 1 :bbir 2 70 2 80 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reprodu
46、ction or networking permitted without license from IHS-,-,-Page 13 TR 7000-1 O: 06-02 Example C.l (concluded) Page 7 EN xxxx Table 3 - Requirements as processed to characteristic number 1.013 No requirement Table 4 - Environmental testing requirements as processed to characteristic number 1.013 No requirement Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
