AECMA PREN 2833-5-2001 Areospace series Glass Fibre Thermosetting Preimpregnates Technical Specification Part 5 Glass Fabric Phenolic Resin Preimpregnate Edition P 1《航天系列玻璃纤维热固性保混剂.pdf

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1、AECMA STANDARD prEN 2833-5 Edition P 1 NORME AECMA AECMA NORM October 2001 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION (AECMA-STAN) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 1 1 ICs: Descriptors: Edition approved for publicat

2、ion 2001 -1 0-31 ENGLISH VERSION Comments should be sent within six months aiter the date of publication to Gulledelle 94 AECMA-STAN 8-1200 BRUXELLES Aerospace series Glass fibre thermosetting preimpregnates Technical specification Part 5: Glass fabric/phenolic resin preimpregnate Srie arospatiale P

3、rimprgns de verre textile/rsine thermodurcissable Spcification technique Partie 5: Verre textile/rsine phnolique primprgns Luft- und Raumfahrt Warmhrtbare Glasfaser - Prepregs Technische Lieferbedingungen Teil 5: Gewebe - Prepregs aus Glasfaser und Phenolharz This “Aerospace Series“ Prestandard has

4、been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published on green paper for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comment

5、s. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of AECMA-STAN it will b

6、e submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX 1 I Material Domain Mr Pays I I 0 aecma 200 Copyright Associat

7、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 prEN 2833-5: 2001 Blank page Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by

8、 IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 2833-5: 2001 1 Scope This standard specifies the requirements for glass fabric/phenolic resin preimpregnates. It shall be used together with EN 2833-1. 2 Normative references T

9、his 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, subsequent amendments to or revisions of any of these publ

10、ications 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 1183-2 Plastics - Methods for determining the density of non-cellular plastics - Part 2: Density gradient column metho

11、d 0 IS0 1889 Reinforcement yarns - Determination of linear density IS0 3572 Textiles - Weaves - Definitions of general terms and basic weaves I EN 2155-12 EN 2377 EN 2379 EN 2489 EN 2743 EN 2823 EN 2824 e EN2825 EN 2826 EN 2833-1 EN 3615 EN 3703 EN 3783 EN 3844-1 EN 3844-2 Aerospace series - Test me

12、thods for transparent materials for aircraft glazing - Part 12: Determination of linear thermal expansion Aerospace series - Glass fibre reinforced plastics - Test method - Determination of apparent interlaminar shear strength Aerospace series - Fluids for assessment of non-metallic materials 1) Aer

13、ospace series - Fibre reinforced plastics - Determination of the action of test fluids Aerospace series - Reinforced plastics - Standard procedures for conditioning prior to testing 1) Aerospace series - Fibre reinforced plastics - Determination of the effect of exposure to humid atmosphere on physi

14、cal and mechanical characteristics 1) Aerospace series - Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of smoke density and gas components in the smoke of materials - Test equipment, apparatus and media 1) Aerospace series - Burning beha

15、viour of non metallic materials under the influence of radiating heat and flames - Determination of smoke density 1) Aerospace series - Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of gas components in the smoke 1) Aerospace series - Gl

16、ass fibre thermosetting preimpregnates - Technical specification - Part i: General requirements 1) Aerospace series - Fibre reinforced plastics - Determination of the conditions of exposure to humid atmosphere and of moisture absorption 1) Aerospace series - Heat release rate for materials and produ

17、cts under the influence of radiating heat and flames - Test method 1) Aerospace series - Fibre composite materials - Normalisation of fibre dominated mechanical properties 1) Aerospace series - Flammability of non metallic materials - Part 1 : Small burner test, vertical - Determination of the verti

18、cal flame propagation 1) Aerospace series - Flammability of non metallic materials - Part 2: Small burner test, horizontal - Determination of the horizontal flame propagation 1) Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for

19、ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 2833-5: 2001 Type Grade Fibre Form Resin Reinforcement EN 3844-3 Aerospace series - Flammability of non metallic materials - Part 3: Small burner test, 45” - Determination of the resistance of material to flame an

20、d glow propagation and to flame penetration 1) Aerospace series - Fibre reinforced plastics - Test method - Determination of the glass transition temperatures 1) Aerospace series - Fibre reinforced plastics - Test method - Determination of bearing strength 1) Aerospace series - Non-metallic material

21、s - Rules for the drafting and presentation of material standards - Part I: General rules 1) Standard Test Methods for Complex Permittivity (Dielectric Constant) of Soiid Electrical Insulating Materials at Microwave Frequencies and Temperatures to 1 650 OC 2) EN 6032 EN 6037 EN 7000-1 ASTM D-2520 Ph

22、enolic Flame resistant “E glass Fabric in accordance with IS0 3572 3 Definitions, abbreviations Not applicable. 4 Material description See table 1. Table 1 - Description of preimpregnate material r 1 1 I Parameter 1 TY Pe 1 5 Testing 5.1 Screening Screening shall be carried out in accordance with EN

23、 2833-1 and tables 2, 3 and 5 of this standard. 5.2 Qualification Qualification shall be carried out in accordance with EN 2833-1 and tables 2, 3, 4 and 5 of this specification. 5.3 Batch release Batch release shall be carried out in accordance with EN 2833-1 and tables 2 and 3 of this specification

24、. 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published by: American Society for Testing and Materials (ASTM), 1916 Race Street, Philadelphia, PA 19103, USA. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license w

25、ith AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 2833-5: 2001 1 T I e m E d 1 .J al v) m al al r o m P o S m S O m o tt, m 3 r S S al o v) I u) al - L ici .- ici .- - I5 f! .- ,- ?i P P m o v) h L: I N al 2 - .- ci n ii I I I t /o 1 mnoum Copyri

26、ght 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 prEN 2833-5: 2001 . al E E i? 2 n m al VJ m al - L c o m P D S m C O m o ._ m a m 6 S S al L o v) I v)

27、 al o - .- f c .- .- : c m S m al Y E .- L“ u) u. I ln Q) P - ii E g E L m - r - b b m Cu z W F - b b m cv z W C O Q o (D .- c .- R - 8 I al o S (CI u) u) ci .- f - Q C ci E S C W I 2 .- a d c O O z 9 O b r O O O r -z 9 m Cu al n im o O Y o O r O m - o O r o Cu 7 cf3 Cu b Cu w 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-,-,-

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