AECMA PREN 2331-1983 Test Methods for the Determination of the Resin Content of Woven Textile Glass Fibre Fabric Preimpregnate Aerospace Series Edition 1《航空航天系列.玻璃纤维中树脂物质的比例试验方法.第1.pdf
《AECMA PREN 2331-1983 Test Methods for the Determination of the Resin Content of Woven Textile Glass Fibre Fabric Preimpregnate Aerospace Series Edition 1《航空航天系列.玻璃纤维中树脂物质的比例试验方法.第1.pdf》由会员分享,可在线阅读,更多相关《AECMA PREN 2331-1983 Test Methods for the Determination of the Resin Content of Woven Textile Glass Fibre Fabric Preimpregnate Aerospace Series Edition 1《航空航天系列.玻璃纤维中树脂物质的比例试验方法.第1.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、CU I i a 8 a F a w Approved by COMITE DE NORMALISATION Of A.ECJ4.A. 1982-09-15 -J w a 9 w - The equivalent versions in French and German languages can be supplied by B.N.A.E., 8, rue Moreau-Vauthier 92100 BOULOGNE-BILLANCOURT - FRANCE. w w CI w 2 2 w u E AECMA-PREN233143 1012311 0002929 4 I _ _ A.E.
2、C.M.A. STANDARD NORME A.E.C.M.A. A.E.C.M.A. NORM prE N2331 Edition 1 February 1983 ENGLISH VERSION TEST METHODS FOR THE DETERMINATION OF THE RESIN CONTENT OF WOVEN TEXTILE GLASS FIBRE FABRIC PREIMPREGNATE AEROSPACE SERIES METHODES DESSAI POUR LA DETERMINATION LUFT- UND RAUMFAHRT DE LA TENEUR EN RESI
3、NE PRFVERFAHREN ZUR BESTIMMUNG DES TISSUS DE VERRE TEXTILE PREIMPREGNES SERIE AEROSPATIALE DES HARZANTEILS VON VORIMPRGNI ERTENI G LASFI LAMENTGEWEBE This industrial standard for the aerospace sector has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matr
4、iel Arospatial). It is published on yellow paper in three equivalent versions (English, French, German. It will be submitted to CEN (European Committee for Standardization) as a draft European Standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under l
5、icense with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. I? AECMA PREN2331 d3.,9 LOL23LL 0002730 O W - prEN2331 Page 2 CONTENTS 1 2 3 4 5 6 7 8 9 10 11 SCOPE FIELD OF APPLICATION REFERENCES DEFINITIONS PRINCIPLE OF THE METHOD APPARATUS STANDARD ATMOSPHERE
6、 FOR CONDITIONING AND TESTING SAMPLING PROCEDURE CALCULATION AND EXPRESSION OF RESULTS TEST REPORT 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-,-,-*
7、e O 1. - AECMA PREN2331 83 LOL23LL 0002731 2 = prEN2331 Page 3 A.E.C.M.A. STANDARD prEN2331 TEST METHODS FOR THE DETERMINATION OF THE RESIN CONTENT OF WOVEN TEXTILE GLASS FIBRE FABRIC PREIMPREGNATE SCOPE This standard specifies, for woven textile glass fibre fabric preimpregnate for aerospace use, m
8、ethods for determining the resin content and the insolubility factor of the resin by calcination and solvent extraction. FIELD OF APPLICATION 2.1 Calcination method This method had to be used if the material to be tested contains only glass and a resin which is completely combustible. The resin cont
9、ent is equal to the loss on igni ti on. 2.2 Solvent extraction method This method applies to products which contain fillers that lose mass at a temperature equal to or below 600OC. The resin content is equal to the loss on solvent ex tract i on. NOTE : By application of the methods defined in 2.1 an
10、d 2.2 the insolubility factor can be calculated. REFERENCES EN2330, Test method for the determination of the percentage of volatile matter in woven textile glass fibre fabric preimpregnate EN62 , Glass reinforced plastics - Standard atmospheres for conditioning and testing. DEFINITIONS A woven texti
11、le glass fibre fabric preimpregnate with a thermosetting resin is a material that can be purchased in the form of a synthetic resin impregnated woven textile glass fibre fabric and used for the manufacture of moulded components (The term preimpregnate is often abbreviated to prepreg). Copyright Asso
12、ciation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN2331 83 = LO12311 0002732 4 W prEN2331 Page 4 5 PRINCIPLE OF THE METHOD 5.1 Calcination method Ignition of
13、weighed test specimens at a temperature of 625OC to constant mass. 5.2 Solvent extraction method Extraction of resin from weighed specimens with solvent to constant mass. 6 APPARATUS 6.1 Calcination method 6.1.1 Laboratory burner of the Meker type or similar. 6.1.2 Container made of an appropriate m
14、aterial and of suitable dimensions (a porcelain or platinium crucible or porcelain boat may be used). 6.1.3 Electric muffle furnace, capable of maintaining a temperature of 625 4 20OC. 6.1.4 Desiccator containing a suitable drying agent (for example : silica gel, calcium chloride, phosphorus pentoxi
15、de). 6.1.5 Balance with an accuracy of 0,l mg. 6.2 Solvent extraction method 6.2.1 Single thickness extraction thimble, nominal diameter 20 to 22 mm, nominal length 60 to 80 mm. 6.2.2 Electric oven capable of maintaining a temperature of 105 ,+ 5OC. 6.2.3 A suitable extraction apparatus of the Soxhl
16、et type, comprising a condenser, siphon tube and flask and provided with an electric heating mantle. 6.2.4 Vacuum desiccator. 6.2.5 Balance with an accuracy of 0,l mg. 6.2.6 Methyl ethyl ketone (MEK), analytical grade, or other sui- table solvent, as agreed between purchaser and supplier. 7- - I 8 I
17、 1 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-,-,-AECMA PREN2331 83 10123Ll 0002733 b 1 prEN2331 Page 5 7 STANDARD ATMOSPHERE FOR CONDITIONING AND TES
18、TING 7.1 Conditioning 7.1.1 Material stored at ambient temperature- Unless otherwise specified, the necessary amount of material (see clause 8) shall be sampled and conditioned in the standard testing atmosphere (see clause 7.2.1) for a minimum of 2 h. 7.1.2 Material stored below ambient temperature
19、 The material, suitably packed in an airtight and solvent resistant bag to prevent moisture pick-up, shall be allowed to reach ambient temperature over a period of time according to the mass of the package. This time shall not be less than 8 h and the actual time shall be recorded in the report. Whe
20、n the material has reached the ambient temperature, the necessary amount (see clause 8) shall be sampled and conditioned in the standard testing atmosphere, for a minimum of 2 h, unless otherwise specified. 7.2 Testing 7.2.1 Standard atmosphere for testing The standard atmosphere shall be in accorda
21、nce with standard EN62 that is to say that the tests shall be carried out at 23 -+ 2OC and (50 + 5) % relative humidity. Time interval between conditioning and testing - 7.2.2 After conditioning, the test shall be carried out within 6 h, unless otherwise specified, the specimen being kept in the sta
22、ndard atmosphere until the test is carried out. 8 SAMPLING 8.1 Test specimen The specimen shall have a length of 100 i 1 mm and a width of 100 ,+ 1 mm. Other dimensions of the test specimen may be used subject to agreement between the purchaser and the supplier, but having a surface area of 100 cm2
23、with an accu- racy of 1: 2%. 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-,-,-AECIA PREN2331 83 m 1012311 0002734 8 U prEN2331 Page 6 5.2 Number and dis
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