AECMA PREN 4500-1-1996 Aerospace Series Metallic Materials Rules for Drafting and Presentation for Material Standards Part 1 General Rules Edition P 1《航空航天系列.金属材料.金属半成品产品尺寸标准的起草和说.pdf

《AECMA PREN 4500-1-1996 Aerospace Series Metallic Materials Rules for Drafting and Presentation for Material Standards Part 1 General Rules Edition P 1《航空航天系列.金属材料.金属半成品产品尺寸标准的起草和说.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 4500-1-1996 Aerospace Series Metallic Materials Rules for Drafting and Presentation for Material Standards Part 1 General Rules Edition P 1《航空航天系列.金属材料.金属半成品产品尺寸标准的起草和说.pdf（18页珍藏版）》请在麦多课文档分享上搜索。

1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication prEN 4500-1 Edition P 1 June 1996 Comments should be sent within six months C5 Chairman after the date of publication to PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA Gulledelle 94 - 8-1200 BRUXELLES - Tel.

2、 (32) 2 775 81 10 - Fax. (321 2 775 81 11 ICs Descriptors : ENGLISH VERSION Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 1 : General rules Srie arospatiale Luft- und Raumfahrt Matriaux mtalliques Metallische Werkstoffe Regeln fr das Erstellen und

3、 die Gestaltung von Werkstoffnormen Teil 1 : Allgemeine Regeln Rgles pour la rdaction et la prsentation des normes de matriaux Partie 1 : Rgles gnrales This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). it is pu

4、blished on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that inter

5、changeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN

6、 (European Committee for Standardization) for formal vote. 1996-06-28 AECMA Gulledelle 94 B-1200 BRUXELLES Mr Odorico aecma 1996 COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesCopyright Association Europeene des Constructeurs de Materi

7、el Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 prEN 4500-1 : 1996 Contents list Page O Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , . . . .

8、. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Scope . 2 Normative references . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 Definitions . . . . . . . . . . . . . . . . .

9、 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Rules for drafting and presentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Annex A (normative) :

10、 Form 1 . Annex B (normative) : Form 2 . Annex C (normative) : Form 3 . Annex D (normative) : Allocation of numbers to optional lines . 3 3 3 4 4 15 16 17 18 COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesCopyright Association Europeen

11、e des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 4500-1 : 1996 O Introduction This standard is part of the series of EN metallic material standards for aerospace applicat

12、ions. The general organization of this series is described in EN 4258. i Scope This standard specifies the general rules for the drafting and presentation of metallic material standards for aerospace applications. It is supported by additional rules specific to : - Aluminium, aluminium alloys and ma

13、gnesium alloys EN 4500-2 - Heat resisting alloys EN 4500-3 - Titanium and titanium alloys EN 4500-4 - Steels EN 4500-5 - Filler metals for welding EN 4500-2 to -5 - Filler metals for brazing EN 4500-6 2 Normative references This European Standard incorporates by dated or undated reference provisions

14、 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 incorporated in it by ame

15、ndment 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 31-9 IS0 31-1 1 IS0 1000 EN 2002-1 EN 2032-1 EN 2032-2 EN 2043 EN 4258 EN 4259 EN 4500-2 EN 4500-3 EN 4500-4 EN 4500-5 EN 4500-6 General principles concerning

16、 quantities, units and symbols Quantities and units of space and time Quantities and units of mechanics Quantities and units of heat Quantities and units of atomic and nuclear physics Mathematical signs and symbols for use in the physical sciences and technology SI units and recommendations for the

17、use of their multiples and of certain other units Aerospace series - Test methods for metallic materials - Part 1 : Tensile testing at ambient temperature 1) Aerospace series - Metallic materials - Part 1 : Designation 1) Aerospace series - Metallic materials - Part 2 : Coding of material in deliver

18、y heat treatment conditions Aerospace series - EN metallic material wrought products - General requirements for product qualification 1) Metallic materials - General organization of standardization - Links between types of EN standards and their use 1) Aerospace series - Metallic materials - Definit

19、ion of general terms 2) Aerospace series - Metallic materials - Rules for the drafting and presentation of material standards - Part 2 : Specific rules for aluminium, aluminium alloys and magnesium alloys 1) Aerospace series - Metallic materials - Rules for the drafting and presentation of material

20、standards - Part 3 : Specific rules for heat resisting alloys 1) Aerospace series - Metallic materials - Rules for the drafting and presentation of material standards - Part 4 : Specific rules for titanium and titanium alloys 1) Aerospace series - Metallic materials - Rules for the drafting and pres

21、entation of material standards - Part 5 : Specific rules for steels 1) Aerospace series - Metallic materials - Rules for the drafting and presentation of material standards - Part 6 : Specific rules for filler metals for brazing 1) 1) Published as AECMA Prestandard at the date of publication of this

22、 standard 2) In preparation at the date of publication of this standard COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesCopyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANo

23、t for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN q500-1-ENGL 177b 1012311 00Llb7Li 575 M Page 4 prEN 4500-1 : 1996 3 Definitions For the purposes of this standard, the following definitions apply : - general definitions, see EN 4259. 3.1 Alloying elemen

24、ts Elements other than base metal, for which the mass content gives the typical characteristics of the alloy. 3.2 The limit dimension is the maximum size, expressed as the equivalent diameter (De), in which the mechanical properties can be obtained at the specified test piece positions, when heat-tr

25、eated in accordance with the material standard. Limit dimension and equivalent diameter De 4 Rules for drafting and presentation NOTE : Examples given in part 2 to 6 are only intended to illustrate the rules for drafting and presentation and may not correspond to real standardized EN products. Techn

26、ological development may require the use of terms additional to those listed. 4.1 Page 1 : Title of the material standard The title shall give sufficient information to unambiguously identify the semi-finished product, in the use condition (see 4.4.1 O). Consequently : 1. the same title shall not be

27、 used for different material standards ; 2. overlapping of mechanical property limits for otherwise identical material standards shall not normally be permitted. Each part of the title shall consist of one or several different lines : - aerospace series ; - the family of metallic material, followed

28、by the designation of the metallic material in accordance with EN 2032-1 ; - method of melting, if appropriate ; - use condition and heat treatment ; - the forms written in singular, or plural, in conformity with the language used and, if appropriate, the method of production and/or final intended u

29、se ; - limiting dimensions ; - relevant mechanical property or physical property limits, if appropriate. 4.2 Page 2 Blank, in principle. Foreword, if necessary. 4.3 Page 3 Clause O : Introduction This clause shall read : COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed

30、 by Information Handling ServicesCopyright 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 prEN 4500-1 : 1996 - “This standard is part of the series of EN

31、 metallic material standards for aerospace applications. The general organization of this series is described in EN 4258“. - “This standard has been prepared in accordance with EN 4500-2“ or “EN 4500-3“ or “EN 4500-4“ or “EN 4500-5“ or “EN 4500-6“. Clause 1 : Scope This clause shall read : “This sta

32、ndard specifies the requirements relating to :“ Repeat all information in the title, presented in the same format, followed by “for aerospace applications. I. If necessary, further information may be added to clarify the scope. Clause 2 : Normative references This clause shall read : “This European

33、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 hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply

34、 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.“, followed by the list of documents, with their titles, to which reference is made in the text. 4.4 Form 1 is a fixed format. Page 4 : c

35、orresponds to form 1 given in annex A If there is insufficient space on a line: - use notes ; - repeat the line(s). Complete the relevant lines with the pertinent requirements, according to 4.4.1 to 4.4.23. Requirements (test method, frequency of testing, sample type, test piece definition, heat tre

36、atment condition of test piece, testing condition) that are already specified in the technical specification or the test method standard called up by the technical specification referenced on line 5, shall not be repeated, in this case writte “See EN XXXX“. If it is necessary to modify the requireme

37、nts of the technical specification or test method, use notes in the table. A hyphen shall be marked on those lines that are not required. Values other than those mentioned on lines 2, 12, 19, 21, 23 and 25 shall be preceded by a sign depending on whether they are minimum or maximum values (, I, 2).

38、Where more than one - test method, - test condition, - test value, is stated, all are mandatory except when indicated by a note, which one is to be used. Symbols for sizes and units : See IS0 31-0, IS0 31-1, IS0 31-3,ISO 31-4, IS0 31-9, IS0 31-1 1 and IS0 1000. Specific examples are given for each f

39、amily of metallic material in EN 4500-2 to EN 4500-6. COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesCopyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo rep

40、roduction or networking permitted without license from IHS-,-,-Page 6 prEN 4500-1 : 1996 4.4.1 This line shall give the family of the metallic material and the conventional designation, in accordance Page 4, line 1 : Material designation with EN 2032-1. 4.4.2 The chemical symbols of the elements sha

41、ll be written in the first line of boxes, in accordance with established conventions (see IS0 31 -9). Page 4, line 2 : Chemical composition The second line of boxes shall indicate the minimum content of that element. The third line of boxes shall indicate the maximum content of that element. The mas

42、s content of alloying elements shall be explicitly defined by the specified values in the second and third line of the boxes. The mass content of other identified elements (e.g. trace elements, impurities, base metal for filler metals, etc) shall only be specified by a minimum and/or a maximum value

43、, as applicable. When other elements are not identified, indicate them as “others“, subdivided into “each“ and “total“. For each element shown, the absence of a value shall be indicated by means of a hyphen. Ratio and/or total content of two or more elements may be specified on line 2. All values V

44、shall be expressed in mass percentage. When very low values are expressed in mass parts per million, a note shall be used to define the abbreviation “p.p.m.“. The following rules shall be observed for the value V : - V min. or V max, I0,Ol % - V min. 0,Ol % express V minrn and V max. in “p.p.m.“ ; e

45、xpress in %. The number of decimal places written shall be consistent with the accuracy required. The base metal shall be indicated in the last column of the second line of boxes by means of a minimum and/or maximum value or by the expression “base“. The standard order for presentation of the elemen

46、ts for each family of metallic materials is specified in EN 4500-2 to EN 4500-6. 4.4.3 Line 3 shall be completed with the appropriate information when one or several specific methods of melting are required. Page 4, line 3 : Method of melting Modification to line 3 (by addition of further melting me

47、thods or changes to melting methods) cannot include a change of the EN reference number if the requirements defined in lines 12 to 98 do not change. When several methods of melting can be used under the same EN reference (.e. the requirements in the lines 12 to 98 do not change), line 3 shall contai

48、n a note which will state in line 98 ; “the melting route for qualification and subsequent delivery of products shall be identical“. 4.4.4 The form or similar forms of the products covered by the standard shall be stated using the same terms as specified in the title. Page 4, line 4.1 : Form COPYRIG

49、HT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesCopyright 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 prEN 4500-1 : 1996 French 4.4.5 The method or methods of production shall be indicated, if necessary. In the case of castings or forgings, indicate requir