AECMA PREN 2559-1988 Aerospace Series Carbon Fibre Preimpregnates Test Method for the Determination of the Resin and Fibre Content and the Mass of Fibre Per Unit Area Issue P 1《航空航.pdf
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1、, A. E. C. M. A. STAN DAR D NORME A. E.C. M.A. A.E.C.M.A. NORM prEN 2559 Issue P 1 October 1988 EDITE PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATERIEL AROSPATIAL 88, boulevard Malesherbes, 76008 PARIS - TEL. 45-63-82-85 UDC : Key words : ENGLISH VERSION Aerospace series Carbon fibre preimpre
2、gnates Test method for the determination of the resin and fibre content and the mass of fibre per unit area Srie arospatiale Luft- und Raumfahrt Mthode dessai Prfverfahren pour la dtermination zur Bestimmung Primprgns de fibres de carbone Kohlenstoffaser-Prepreg de la teneur en rsine et en fibres et
3、 de la masse surfacique de la fibre des Harz -und Fasermasseanteiis und der flchenbezogenen Fasermasse This Aerospace Series pre-standard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Arospatial), It is published on green paper for the needs
4、of AECMA-Members. It has been technically approved by the experts of the concerned AECMA Commission following comment by the Member countries. Subsequent to the publication of this pre-standard, the technical content shall not be changed to an extent that interchangeability is affected, physically o
5、r 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 (European Committee for Standardizatio
6、n) for final vote. Nota - Extra copies can be supplied by B.N.A.E. - 8, rue Moreau-Vauthier - 92100 BOULOGNE-BILLANCOURT Edition approved for publication Comments should be sent within six months C7 Chairman after the date of publication decision 88, Bd. Malesherbes 17th October 1988 A.E.C.M.A. Mr.
7、BEZAUD 75008 PARIS - FRANCE aecma 1988 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 PREN2557 88 101Z3Ll 0003Lf85 T prEN 2559 Page 2 Contents 1
8、 2 3 4 5 6 7 8 9 10 11 Scope and field of application References Definitions Principle of the method Designation of the method Apparatus Standard atmosphere for conditioning and testing Sampling and test specimens Procedure Calculation and expression of results Test report 0619XSP1387T5 Copyright As
9、sociation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN2559 88 LOL23LJ C10039p8b L prEN 2559 Page 3 1 Scope and field of application This ctcindard specifies a
10、Iuettiod for determining the resin content (with or without volatiles) and fi.bre content and mass of fibre per uni area of a carbon fibre preimpregnate, for aerospace use. 1.1 If the material to be tested contnfns only carbon and a resin which is completely combustible (urder the conditions of this
11、 test methcd) , the resiti content is equal to the loss on wet combustion (see note below). 1.2 As an alternative to clause 1.1 , the resin cor,tent is equal to the loss or; sclvent extraction (see note below). Eiote : The carbon used as a reinforcement can be coated with 2 resin cLze and in this ca
12、se, this will be eliminated during wet corfibuston or solvent extraction and thereiore included in the result. 1.3 This stardurd does not give any directions iiecessary to meet the health and safety requirements. It is the resyonsibilPty cf the use+ of this stnndard to cortsult nd establish appropri
13、ate health and safety precautlmo . 0 2 Referciices EN 2557 Aerospace series - Carbon fibre preimpregnates - Test method for the determimtion of mass per unit area i EN 2558 Aerospace series - Carbon Eibre preimpregnates - Test method for the determination of the pezceiltage of olat ti le matter 1) E
14、N 2743 Aerospace series -a Reinforced plastics - Standard atmospheres for conditioning and testing 1) 3 l)eiiriitionc k cerbon fibre pxeimpregnate with a thermosettfng or thernoplastic resin is a material thuc can be purchased in the form o a synthetic resin impregnated carbon fibre ur.idirectioni s
15、heet, tape or woven fabric aiid iised for the narturacturc of moulded conponents. 8 4 Principle of the metlics 4.1 Vet: coinbustLon method DetermLiiation of the difference in Ioass by mzns of weighing Sefore 2nd after removal of the resin by it wet combustion method, employing coricentraied auiphuri
16、c aclci md hydrogeiz peroxide solution, to constant nass. i) In preperatior, 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 PREN2557 88 m LOL231
17、L 0003487 3 m prEN 2559 Page 4 4.3 Solvent extraction nethod. Determination of the. difference in muss by means cf weighir,g before aiid nfter extraction of the resin with methyl ethyl ketone or other suitable solvent, as agreed between the purchoser and the supplier, to constant mass. Two variants
18、are possible : 4.2.1 A standard method of extraction using a Soxhlet. 4.2.2- A fsster method of extraction by soakiiig and decantution. 5 Designation of the method Carbon fibre preimpregnates Test method for the determinstion of the resin and fibre content and the mass of fibre per unit area EN 2559
19、 - A Title description Standard number Method of test procedure (see table 1) Table 1 Principle Procedure Wet combustion (see clause 4.1) See clause 9.1 Solvent extraction using Soxhlet (see clause 4.2.1) See clause 9.7 Solvent extraction by soaking and decantation See clause 3.3 (see clause 4.2.2)
20、6 Apparat u s Gal 6.2 Template of standrd specimen 6.3 Accillary items such as sharp cutting knife and tweezers 6.4 Wet combustion method 6.4.1 250 ml double necked pear shaped flask with : 6.4.1.1 6.4.1.2 a water pump coiinected to the other. Ealance with an accuracy of 0,l mg 50 nil dropping funne
21、l to one neck and 0619XSP1267T5 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 PREN2557 8 LOL23LL 0003488 5-a I prEN ?559 Page 5 O 1 0619XSP1387
22、T5 6.4.3 Heat source with suitable temperature control 6.4.3 400 ml beaker 6.4.4 20 ml sintered glass crucible (11 3 porosity) 6.4.5 Desiccator containing a suitable drying agent (for example silica gel, calcium chloride or phosphorus pentoxide) 6.4.G Concentrated sulfuric acid (specific gravity 1,8
23、4) 6.4.7 Hydrogen peroxide solution (30% to 50% w/v) 6.4.8 Acetone (propanone) 6.4.9 Distilled water 6.4.10 Suitable protective clothing, including rubber gloves, for haridling hydrogen peroxide and sulphuric acid solutions and a safety screen for eye protection. 6.5 Solvent extraction using a Sohxl
24、et 6.5.1 Single thickness extraction thimble, nominal diameter 30 to 31 mm, nominal length 60 to 80 mm. 6.5.2 Electric oven capable of maintaining a tempereture of 105C with an accuracy of 4, 5C 6.5.3 A suitable extraction apparatus of the Sohxlet t:ype, comprising a condenser, siphon tube and flask
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