1、STD-AECMA PREN 2833-L-ENGL 1777 10123L1 0014042 241 W I I aecma 1997 AECMA STANDARD NORME AECMA AECMA NORM l prEN 2833-1 Edition P 2 November 1997 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 11
2、 ICs: Supersedes edition P 1 September 1994 Descriptors: ENGLISH VERSION Aerospace series Glass fibre thermosetting preimpregnates Technical specification Part 1 : General requirements Srie arospatiale Luft- und Raumfahrt Primprgns de verre textile/rsine thermodurcissable Partie 1 : Exigences gnrale
3、s Warmhrtbare Glasfaser - Prepregs Teil 1 : Allgemeine Anforderungen Spcification technique Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the
4、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 interchangeability is affected, phys
5、ically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (N?S) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standa
6、rdization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX Comments should be sent within six months after the date of pubiication to I Edition approved for publication 1997-1 1-28 AECMA Gulledelle
7、94 B-1200 BRUXELLES C7 Chairman Mr Wright 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-,-,-STD-AECMA PREN 2833-II-ENGL 1797 LOL23L1 OOII4OLI3 188 m Page
8、 2 prEN 2833-1 : 1997 Contents . . . . , , . . . . . . . . . . . . . . . . . . . . . . . . 1 Scope ._._._ . , . . . , , . , . . , , , . . . . , , . . . . . . . . . . . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Normative references 3
9、 Definitions . . 3.1 Batch . . 3.2 Preimpregnate . 3.3 3.4 Work Life .f .I. I . . Storage Life (NOTE : sometimes known as shelf life) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.5 3.6 3.7 3.8 3.9 3.10 3.1 1 3.12 3.13 3.14 3.1 5 3.16 3.17 3.1 8 Inclusion Woven fa
10、bric . Unidirectional sheet and tape Orientation of Fibres . Material standard . Individual product sp Qualification Side qualification . Screening tests Qualification testing Compatibility Acceptance testing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . I . . . . . . . . . . ,
11、 Mandated body Release testing/Supplier quality control testing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Requirements 4.1 General requirements 4.2 Workmanship . . 4.3 Supply of Defective Material . . . 4.4 Physical, chemical and mechanical . . . , . . . . ,
12、 , . . , . . , . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , . . . . . , , . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Qualification . . . . 5.2 Quality assur
13、ance . 5.3 Product qualification 5.4 Health and safety 6 Batch control . . . . . 6.2 Release tests 6.3 Warranty . . . 6.4 Sampling . . ., . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . .
14、. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 Preparation for delive . . . . . . . . . . 7.2 Packaging . 7.4 Delivery date 7.6 Order endorsement . . . . . 7.3 Storage before shipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 3 5 5 5
15、 5 5 6 6 6 6 6 6 6 6 6 7 7 7 7 7 7 7 10 12 13 17 17 17 17 21 21 21 21 23 23 24 24 25 26 26 26 26 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-,-,-STD-AE
16、CMA PREN 2833-1-ENGL 1797 W LUL23L1 0014044 014 = Page 3 prEN 2833-1 : 1997 1 Scope This European Standard specifies glass fibre thermosetting preimpregnates for aerospace applications. The specification is applicable to material containing unidirectional or woven fabric supplied as flat sheet or wo
17、und onto reels. The specification also includes unidirectional reinforcements which consist of glass fibre warp yarns held together by not more than 5% mass/mass of fibres other than glass. Three dimensional woven forms or chopped strand non-woven mats are not covered. This standard does not cover s
18、ingle glass rovings impregnated with thermosetting resin. A series of EN material standards defines the individual requirements for each particular type or grade of glass fibre thermosetting preimpregnate. 2 Normative references This European Standard incorporates by dated or undated reference, prov
19、isions from other publication. 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 publication apply to this standard only when incorporated in it by amendmen
20、t or revision. For undated references the latest edition of the publication referred to applies. IS0 1183 EN 2000 EN 2243-3 EN 2243-4 EN 2329 EN 2330 EN 2331 EN 2332 EN 2374 EN 2377 EN 2379 EN 2489 Plastics - Methods for determining the density and relative density of non-cellular plastics Aerospace
21、 series - Quality assurance - EN aerospace products - Approval of the quality system of manufacturers Aerospace series - Structural adhesives - Test methods : Part 3: Peeling test metal to honeycomb core Aerospace series - Structural adhesives - Test methods : Part 4: Metal-honeycomb core flatwise t
22、ensile test Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of mass per unit area Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of the content of volatile matter Aerospace series - Textile glass fibre preimpregnate
23、s - Test method for the determination of the resin and fibre content and mass of fibre per unit area Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of the resin flow Aerospace series - Glass fibre reinforced mouldings and sandwich structures - production of
24、 test panels Aerospace series - Glass fibre reinforced plastics - Test method - Determination of apparent interlaminar shear strength Aerospace series - Fluids for assessment of non-metallic materials 1) Aerospace series - Fibre reinforced plastics - Determination of the action of test fluids 2) 1 1
25、 In preparation at the date of publication of this standard 2 1 Published as AECMA Prestandard at the date of this publication Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted witho
26、ut license from IHS-,-,-STD-AECMA PREN 2833-1-ENGL 1777 = 1Ol123Ll 0014045 T50 D Page 4 prEN 2833-1 : 1997 EN 2564 EN 2597 EN 2743 EN 2746 EN 2747 EN 2823 EN 2824 EN 2825 EN 2826 EN 2850 EN 3042 EN 3615 EN 3703 EN 3783 EN 3844 EN 4238 EN 6031 EN 6032 Aerospace series - Carbon fibre laminates - Test
27、method for the determination of the fibre and resin fractions and porosity content 1) Aerospace series - Carbon thermosetting resin unidirectional laminates - Tensile test perpendicular to the Ffbre direction 1) Aerospace series - Reinforced plastics - Standard procedures for conditioning prior to t
28、esting Aerospace series - Glass fibre reinforced plastics - Determination of flexural properties - three point bend method 1) Aerospace series - Glass fibre reinforced plastics. Determination of tensile properties 1) Aerospace series - Fibre reinforced plastics - Test method for the determination of
29、 the effect of exposure to humid atmosphere on physical and mechanical characteristics 1) Aerospace series - Burning behaviour - determination of smoke density and gas components in the smoke of materials under the influence of radiating heat and flames - Test equipment, apparatus and media 1) Aeros
30、pace series - Burning behaviour - determination of smoke density and gas components in the smoke of materials under the influence of radiating heat and flames - Determination of smoke density 1) Aerospace series - Burning behaviour - determination of smoke density and gas components in the smoke of
31、materials under the influence of radiating heat and flames - Determination of gas components in smoke 1) Aerospace series - Carbon thermosetting resin unidirectional laminates - Compression test parallel to fibre direction 1) Aerospace series - Quality assurance - EN aerospace products - Qualificati
32、on procedure Aerospace series - Fibre reinforced plastics - Procedure for the determination of the conditions of exposure to humid atmosphere and the determination of moisture absorbtion Aerospace series - Heat release rate for materials and products under the influence of radiating heat and flames
33、- test method Aerospace series - Fibre composite materials - Normalisation of fibre dominated mechanical properties 1) Aerospace series - Flammability of non-metallic materials - Parts 1, 2 and 3 Aerospace series - Fibre reinforced plastics - Determination of the effect of dry heat on physical and m
34、echanical characteristics 1) Aerospace series - Fibre reinforced plastics - Determination of in-plane shear properties ( * 45O tensile test) 2) Aerospace series - Fibre reinforced plastics - Test method - Determination of the glass transition temperature 2) 1 ) In preparation at the date of publicat
35、ion of this standard 2) Published as AECMA Prestandard at the date of this publication 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-,-,-EN 6033 EN6039 E
36、N 6040 EN 6041 EN 6042 EN 6043 ASTM-C-393 ASTM-D-2520 Aerospace series - Carbon fibre reinforced plastics - Test method - Determination of interlaminar fracture toughness energy Mode 1 - Glc 1) Aerospace series - Fibre reinforced plastics - Determination of the exothermic reaction during curing of p
37、reimpregnate materials 2) Aerospace series - Non-metallic materials - Analysis of thermoset systems by High Performance Liquid Chromatography (HPLC) 2) Aerospace series - Non-metallic materials - Analysis of non-metallic materials (uncured) by Differential Scanning Calorimetry (DSC) 2) Aerospace ser
38、ies - Analysis of organic compounds by Infra-red Spectroscopy 2) Aerospace series - Fibre reinforced plastics - Determination of gel time and viscosity of matrix resins 2) Test method for the flexural properties of flat sandwich constructions 3) Test methods for complex permitivity (dielectric const
39、ant) of solid electrical insulating materials at microwave frequencies and temperatures to 1650C 3) 3 Definitions For the purposes of this standard, the following definitions apply. 3.1 Batch A number of rolls or sheets that are impregnated in one single continuous operation that conforms to an acce
40、pted manufacturing method. 3.2 Preimpregnate Woven fabric or unidirectional fibre sheet or tape impregnated with a matrix resin, and suitably processed (B-staged) for storage, handling purposes and curing by heat and pressure without further additives. 3.3 Storage Life (NOTE : sometimes known as she
41、lf life) Period of time from the impregnation date during which the preimpregnate, when stored under the specified storage and workshop conditions: - keeps all its physical, chemical and mechanical properties conforming to the standard requirements. - is covered by the manufacturers guarantee. 3.4 W
42、ork Life Cumulative period under workshop conditions during which the preimpregnate remains processable and will meet the requirements of the material standard and/or the IPS. I) In preparation at the date of publication of this standard 2) Published as AECMA Prestandard at the date of this publicat
43、ion 3) Published by: American Society for Testing and Materials (ASTM), 11 91 6 Race Street, Philadelphia, PA 19103 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license
44、from IHS-,-,-3.5 Inclusion Any foreign body of size greater than 0,5 mm in any direction. 3.6 Woven fabric Glass fibre yarns woven into a fabric of any two dimensional weave pattern. 3.7 Unidirectional sheet and tape A planar array of parallel glass fibre yarns. When required, stabilising fibres of
45、another material (e.g. aramid fibre) may be stitched at intervals into the array at 90“ to the yarn orientation. 3.8 Orientation of Fibres Traditionally, the direction of the Oo fibres is parallel to the warp of the fabric. 3.9 Material standard The material standard lists data describing the perfor
46、mance of the material group. It gives the requirements, limits and test methods for the qualification of a product group. NOTE: This performance level is directly related to the design allowable of that group. 3.10 Individual product specification (IPS) The individual product specification gives the
47、 expected performance about a specific product of one manufacturer and its performance. NOTE: Each product has a separate specification. The individual performance and the acceptance values of the product for release testing are listed, including the requirements for physicochemical testing. 3.1 1 Q
48、ualification See EN 2000 NOTE: This demonstrates that the manufacturers and the preimpregnate supplied meet the requirements as laid down in this specification and the relevant material standard. The demonstration is given by the approval of the manufacturers quality system and the results of the qu
49、alification testing. 3.12 Side qualification Side qualification is a reduced qualification program as a result of minor changes in the original qualified material. 3.13 Screening tests Screening tests are tests performed by the manufacturer on samples of material made according to the requirements of this specification and the relevant material standard to evaluate the suitability of the material for qua
