AECMA TR 7000-1-2002 Aerospace Series Non-Metallic Materials Rules for the Drafting and Presentation of Material Standards Part 1 General Rules Edition 1 Supersedes prEN 7000-1 Edi.pdf

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1、AECMA Technical Report TR 7000-1 Rapport Technique AECMA Edition 1 AECMA Fach bericht June 2002 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION Jn Gulledelle 94 - 8-1200 Brussels -Tel. + 32 2 775 81 10 - Fax. + 32 2 775 81 11 - www.aecma-stan.org Edition approved for

2、publication 28 June 2002 ICs: Descriptors: Extra copies can be supplied by B.N.A.E. Technopolis 54 - 199, rue Jean-Jacques Rousseau Non-metallic Material Domain 92138 ISSY - LES - MOULINEAUX CEDEX - FRANCE ENGLISH VERSION Aerospace series Non-metallic materials Rules for the drafting and presentatio

3、n of material standards Part 1 : General rules Supersedes prEN 7000-1 Edition PI September 1998 Srie arospatiale Luft- und Raumfahrt Matriaux non-mtalliques Nichtmetallische Werkstoffe Rgles pour la prparation et la prsentation des normes de materiaux Partie I : Rgles gnrales Regeln fr die Erstellun

4、g und die Gestaltung von Werkstoffnormen Teil 1: Allgemeine Regeln 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. I I I I Copyright 2002 O by AECMA-STA/

5、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 2 TR 7000-1 : 06-02 Foreword The main task of AECMA-STAN is to prepare EN standards. In exceptiona

6、l circumstances, 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 pub

7、lished as a European 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 Introduction . 1 Scope . 2 Normative references . 3 4 5 O Definitions, symbols and abbrevia

8、tions . Rules for drafting and presentation . Rules for completion of tables Annex A (normative) Form 1: Table 1 Annex B (normative) Form 2: Tables 2 to 4 . . . Annex C (normative) Optional characteristics 3 3 3 3 5 7 10 11 12 Copyright Association Europeene des Constructeurs de Materiel Aerospatial

9、 Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 TR 7000-1 06-02 O Introduction This standard is part of the series of TR non-metallic materials standards for aerospace applications. The general organisation of this se

10、ries is described in EN 4385. This document is a level 2 document as defined in EN 4385. 1 Scope This standard specifies the general rules for the drafting and presentation of non-metallic material standards, for aerospace applications. It is supported by additional rules specific to each family, de

11、fined in TR 7000-2 onwards. 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 next and the publications are listed hereafter. For dated references, subseq

12、uent 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. IS0 31-0 IS0 31-1 IS0 31-3 IS0 31-4 IS0 31-1 1 IS0 1000 EN 4385 TR 700

13、0-2 Quantities and units - Pari O: General principles Quantities and units - Part 1 : Space and time Quantities and units - Part 3: Mechanics Quantities and units - Part 4: Heat Quantities and units - Part 11: Mathematical signs and symbols for use in the physical sciences and technology SI units an

14、d recommendations for the use of their multiples and of certain other units Aerospace series - 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 standa

15、rds - Part 2: Rubbers 2) 3 Definitions, symbols and abbreviations 3.1 Defi nit ions For the purpose of this standard the following definitions apply: 3.1.1 material standard a standard specifying a series of requirements relating to a non-metallic material, which may be a semi- finished product, suc

16、h as: - one or more delivery conditions, - one reference set of processing conditions for acceptance test and qualification purposes which may differ from the use condition intended by the user, - series of technical requirements for these different conditions NOTE A material standard may also speci

17、fy one or more than one use condition, providing that the variants are not interconvertable. Such cases shall be clearly identified by the designation system given in the material standard. 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published as AECMA Technical

18、Report at the date of publication 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 4 TR 7000-1 : 06-02 3.1.2 family of non-metalli

19、c material a group of non-metallic materials characterised by basic descriptions generally in semi-finished product forms such as but not exclusively: - rubbers, - sealants, - transparent plastics, - glass, - adhesives, - anaerobic polymerizable compounds, - honeycombs, - paints, - reinforcement fib

20、re, - preimpregnates, - textiles 3.1.3 semi-finished products a generic term used to indicate that the material as delivered is in an intermediate form to that occuring in the final component This term may refer to the following: - adhesives where one delivered condition may be a two-part mix and th

21、e final use condition is the cured adhesive; - preimpregnates, which are subsequently shaped to produce a part with specified characteristics; - honeycomb which may be shaped and formed. 3.1.4 type of semi-finished products semi-finished product forms (sheets, rolls, tube, cloths, liquids, paste etc

22、.) associated with the relevant family of non-metallic materials 3.1.5 final condition of use the condition of the material in which no further processing (except machining or shaping) is required before use 3.2 Symbols and abbreviations For the purpose of this standard, the following symbols and ab

23、breviations shall apply: Abbreviations shall be taken from IS0 31. The following for sizes and units shall be taken from IS0 31-1, IS0 31-3, IS0 31-4, IS0 31-11 and IS0 1000. The following are typical symbols used: - %”for thickness; - ”b”for width; - lfor length; - Dfor outside diameter; - “”for in

24、side diameter; - “afor temperature; - “f”for time; - “RH”for relative humidity. NOTE The abbreviation “min.”, for minimum shall not be used. When it is necessary to state a minimum or maximum value this shall be done using the symbols , , alternatively the word shall be written in full. The exceptio

25、n to this in when “min.” and ”max.” are defined for other uses within abbreviations, e.g. Rmax. or - The family of the non-metallic material; - Form or forms, written in singular or plural, in conformity with the language used and, if appropriate, the method of production andlor final use; - Dimensi

26、ons if appropriate; - Relevant mechanical or physical limits if appropriate. 4.2 Clause O: Introduction When required, this clause shall read: O Introduction This standard is part of the series of EN non-metallic materials standards for aerospace applications. The general organisation of this series

27、 is described in EN 4385. This standard is a level 3 document as defined in EN 4385. It has been prepared in accordance with (hserf relevant TR 7000 Part number). 4.3 Clause I: Scope This clause shall read: Scope This standard specifies the requirements relating to . (repeat all the information in t

28、he title in a grammatical sequence that satisfies the language used . for aerospace applications. (Followed by any additional information, as necessaty, to clarify the field of application). 4.4 Clause 2: References This clause shall read: 2 This European Standard incorporates by dated or undated re

29、ference provisions from other publications. These normative references are cited at the appropriate places in the text 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 incorpo

30、rated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. Nor ma tive refe re n ces Footnotes shall indicate: - for AECMA documents the relevant status (if not EN), - for other documents the body responsible for the publication (except IS

31、OAEC). 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 6 TR 7000-1 : 06-02 4.5 4.5.1 Clause 3.1: Definitions This clause shall read : Clause 3: De

32、finitions, symbols and abbreviations 3.1 Definitions For the purpose of this standard, the following definitions apply: 3.1.1 Sub-case numbering In the column requirement at the left side a sub-case number is given, The definition of these sub- case numbers is as follows: Sub-case number Definitions

33、 - Technical specification I Test method 2 Frequency of testing 3 Sample type 4 Test piece definition 5 Conditioning of test piece 6 Testing condition 7 Acceptance criteria NOTE 1 standard, e.g. in the reference to the technical standard (characteristic number 1.004). The absence of a sub-case indic

34、ates that the necessary information is given in table 1 of this 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

35、 are highlighted in the form of bold frame and bold characters to show they are mandatory for routine release of the material. 3.1.2 Other definitions Continue sub-clause numbering as necessary. 4.5.2 This clause shall read : Clause 3.2 : Symbols and abbreviations 3.2 Symbols and abbreviations For t

36、he purpose of this standard, the following symbols and abbreviation apply: Followed by a list of symbols and abbreviations. 4.6 Clause 4: Requirements The material standard requirements are given in a series of tables. The format of these tables, and rules for their completion, are given in clauses

37、3.1.1, 5.1 and 5.2 of this standard. Within each material standard, the following clause shall be used: 4 Requirements The required characteristics are given in: Table 1 : General requirements Table 2: Requirements in the delivery condition Table 3: Requirements as processed to characteristic number

38、 1 .O13 Table 4: Environmental testing requirements as processed to characteristic number 1 .O1 3. 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

39、 7 TR 7000-1 : 06-02 - I 2 3 4 5 6 7 5 Rules for completion of tables Technical specification Test method Frequency of testing Sample type Test piece definition Conditioning of test piece Testing condition Acceptance criteria 5.1 Format of tables 5.1.1 Table I: see Annex A This form is mandatory irr

40、espective of the family of non-metallic material. The actual format is dependent on the family of non-metallic material. This form describes the general characteristics of the product, and is applicable to all non-metallic material standards. 5.1.2 This form shall be used for each of the following t

41、hree tables for which it is required to specify requirements. When required optional characteristic selected from annex C shall be completed as follows: Tables 2 to 4: see Annex B Table 2, requirements in the delivery condition (column 0 optional (see figure 1): add line or case number). Table 3, re

42、quirements as processed to characteristic number 1.013 (column 0 optional: add line or case number). Table 4, environmental testing requirements as processed to characteristic number 1 .O13 (column 0 optional: add line or case number). The characteristic numbers, (see annex C) shall be written in co

43、lumn (see figure I), and shall be pre-fixed with the table number. When more than one characteristic number applies for a particular requirement, both characteristic numbers shall be shown in column 0. The characteristic titles shall be written in column 0 (see figure I), including any information t

44、o clarify the requirements. Column (see figure I) shall be completed with a sub-case number corresponding to the information to be given in column 0 (see figure 1) and selected from the following: 0 Case number or line number (optional) I Characteristic number 0 Characteristic Sub-case number 7 - Fi

45、gure I 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 7000-1 : 06-02 - A sub-case shall be omitted, if the necessary information is given in

46、 the technical specification referenced in 1.004. - If all the necessary information is contained in the technical specification, the sub-case is opened by stating “see EN xxxx“. In this case a hyphen is inserted in the third column. No other sub-case number will be given. - If the technical specifi

47、cation or the test method: - does not give any information, - only gives partial information, - or gives a choice, or if the requirements differ from those given in the technical specification or test method, then sub- cases 1 !o 7 shall be completed as required with the necessary information. - Col

48、umn 0 is completed, in accordance with the specific instructions given in the relevant dash numbered part of this standard. Values which will be agreed during qualification shall be expressed as a range in the material standard, e: No “X values to be specified in material standards. It is only neces

49、sary to complete those sub-cases for which information is required to be specified. 5.2 5.2.1 General The column 0 (see figure 1) is optional. If used, the case number shall be consecutive. Alternatively, it can be replaced by a consecutive line numbering as indicated in the dash number part. If there is insufficient width in a column then information shall be repeated below and marked “continued“. General instructions for