EN 2562-1997 en Aerospace Series - Carbon Fibre Reinforced Plastics - Unidirectional Laminates - Flexural Test Parallel to the Fibre Direction《航空航天系列 碳素纤维增强塑料 单向层压塑料 与纤维方向平行的弯曲试验》.pdf
《EN 2562-1997 en Aerospace Series - Carbon Fibre Reinforced Plastics - Unidirectional Laminates - Flexural Test Parallel to the Fibre Direction《航空航天系列 碳素纤维增强塑料 单向层压塑料 与纤维方向平行的弯曲试验》.pdf》由会员分享,可在线阅读,更多相关《EN 2562-1997 en Aerospace Series - Carbon Fibre Reinforced Plastics - Unidirectional Laminates - Flexural Test Parallel to the Fibre Direction《航空航天系列 碳素纤维增强塑料 单向层压塑料 与纤维方向平行的弯曲试验》.pdf(14页珍藏版)》请在麦多课文档分享上搜索。
1、STD*BSI BS EN 25b2-ENGL 1797 Lb2Ybb7 Ob3LOb8 872 W BRITISH STANDARD AEROSPACE SERIES Carbon fibre reinforced plastics - Unidirectional laminates - Flexural test parallel to the fibre direction The European Standard EN 2562 : 1997 has the status of a British Standard ICS 49.025.40 BS EN 2562 : 1997 N
2、O COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGH LAW STDeBSI BS EN 25bZ-ENGL 1777 1b24bb9 Ob310b7 707 BS EN 2662 : 1997 Committees responsible for this British Standard The preparation of this British Standard was entrusted to Technicai Committee ACE/, Aerospace stsuctural reinforced
3、 plastics, upon which the following bodies were represented. British Plastics Federation Minishy of Defence Society of British Aerospace Companies This British Standard, having been prepared under the direction of the Engineering Sector Board, was published under the authority of the Standards Board
4、 and comes inh effect on 15 August 1997 O BSI 1997 Amendments issued since publication I Date Amd. No. 1 Textanected The following BSI references relate to the work on this standard Committee reference ACE164 Draft for comment 88/7224 DC ISBN O 580 26697 4 STD-BSI BS EN 25b2-ENGL 1777 Lb211bb7 Ob310
5、70 q20 BS EN 2662 : 1997 Contents page Inside front cover Nationai foreword ii 2 1 Scope 3 Committees responsible Foreword Specification 3 3 4 2 Nonnative references 3 Definitions 4 Principle 5 Apparatus 4 6 Specimens 5 5 7 Procedure 6 8 Expressionofresults 9 Designation 8 8 10 Testreport i O BSI 19
6、97 _ _ STD-BSI BS EN 25b2-ENGL 1777 = libEiibb9 Ob31071 3b7 W BS EN 2662 : 1997 National foreword This British Standard has been prepared by Technical Committee ACWM and is the English language version of EN 2562 : 1997 Aerospace series - Cut%on fibre reinfmd plastics - Unidirectional laminates - Fl
7、exuml test pa the point on the same diagram corresponding to a stress calculated from PRAO. PR is the load at failure of the specimen. The calculated stresses and strains are those present at the surface of the specimen and parallel to its axis. 4 Principle The method consists of the measurement of
8、the deflection at the central loading nose as a function of the applied load during a flexural test on three supports carried out at constant rate of displacement until failure occurs. The strain parallel to the fibre direction is calculated as a function of the applied stress. 5 Apparatus 5.1 Micro
9、meter with 6 mm diameter flat faces and accurate to 0,Ol mm 5.2 Testing machine, accurate to within 1 % in the load range used 5.3 range used Device for recording the deflection as a function of load, accurate to 1 % in the deflection 5.4 If necessary, heated cabinet, regulated so as to conform to E
10、N 2744 for tests at temperatures other than ambient. 5.5 Thermocouple and recorder for tests at temperatures other than ambient. 5.6 Test fixture See figure 1 and table 1. It shall ensure accurate positioning of the specimen. Misalignment between loading nose and supports shall not exceed 0,l mm. ST
11、D-BSI BS EN 25b2-ENGL 1777 = Lb24bb7 Ob31076 947 Symbols b L Page 5 EN 2562:1997 Type A 2) Type B 10 f 0,2 10 i: 0,2 100 f 1 60 f 1 6 Specimens Take specimens from panels prepared according to EN 2565. 6.1 Shape and dimensions See figure 1 and table 1, - I I Figure 1 Table 1 Dimensions in millimetre
12、s 1 I h 1) I 2 f 0.2 I 2 f 0.2 I l I r1 I 12,5 f 0,l 12,5 0,l r2 I 5 *0,1 I 5 f 0,l 1) If the ply thickness causes any uncertainty regarding the number of layers necessary to obtain a laminate of the required thickness, this number of layers shall be specified in the relevant material standard. 2) T
13、ype A specimens shall be used unless otherwise specified in material standard. 6.2 Number Minimum of five 7 Procedure 7.1 Conditioning EN 2743 for rests in the initial state, EN 2489 for tests after immersion, EN 2823 for tests after exposure to humid atmosphere. _ STD-BSI BS EN 25b2-ENGL 1777 M 1b2
14、4bb7 Ob31077 AA5 M Page 6 EN 2562:1997 7.2 Tests 7.2.1 Determine h by calculating the arithmetic mean of three measurements of the thickness to within 0,Ol mm taken across the width at the centre of the specimen. Measure the width b to within 0,Ol mm at the centre of the specimen. Measure the distan
15、ce between supports to within 0,l mm. 7.2.2 of the test shall conform to the following conditions : For tests at temperatures other than ambient, the period separating the conditioning and start - for specimens which have not been aged or subjected to immersion, the exposure time at the test tempera
16、ture shall be established by preliminary tests ; - for specimens subjected to immersion, see EN 2489 ; - for specimens subjected to humid atmosphere, see EN 2823. 7.2.3 contact with the loading nose, ensuring that its axis is perpendicular to the supports. Locate the specimen in the test fixture, wi
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