BS EN 6032:2015

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Aerospace series. Fibre reinforced plastics. Test method. Determination of the glass transition temperatures

Published By	Publication Date	Number of Pages
BSI	2015	16

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Categories: 49.025.40 - Rubber and plastics, BSI

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Description

This standard specifies a method to determine the apparent glass transition temperatures of nonmetallic materials.

This standard is applicable to unidirectional tape and woven fabric reinforced plastic or plastic materials like adhesive or neat resin for comparison of the influence on the glass transition temperature resulting from processing-parameters of non-metallic parts, for compatibility tests for checking co-curing effects of different prepreg types or with adhesive.

This standard does not give any directions necessary to meet health and safety requirements. It is the responsibility of the user of this standard to consult and establish appropriate health and safety precautions.

PDF Catalog

PDF Pages	PDF Title
4	Contents Page
5	European foreword
6	1 Scope 2 Normative references 3 Terms and definitions
7	4 Principle of the method 4.1 Method A 4.2 Method B 4.3 Method C 5 Designation of the method
8	6 Apparatus 6.1 Equipment of the dynamic mechanical analysis type with bending and/or torsional/shear loading of the specimen, capable of testing and recording frequency, storage modulus, loss modulus, tan delta and temperature in the ranges used. 6.2 Micrometer with 6 mm fiat faces and accurate to the nearest 0,01 mm. 6.3 Vernier caliper accurate to the nearest 0,1 mm. 7 Test specimen 7.1 Test specimen description 7.2 Test specimen preparation 7.3 Number of test specimens
9	7.4 Ageing of specimen 8 Procedure 8.1 Conditioning 8.2 Determination of dimensions 8.3 Calibration 8.4 Testing 9 Presentation of the results 9.1 Diagram
10	9.2 Determination of Tg-onset 9.3 Determination of Tg-loss 9.4 Determination of Tg-peak (optional) 9.5 Determination of the slope angle ( (optional) 9.6 Quantitative check 10 Test report 10.1 Complete identification of the material tested, including at least material designation, supplier, batch number, roll number, fibre areal weight, filament count, processing details, stacking sequence, test orientation. 10.2 All details regarding specimen preparation including cure parameters. 10.3 The measured specimen dimensions. 10.4 Ageing and/or exposure condition prior to the test.
11	10.5 Date of test, facility and identification of individuals performing the tests. 10.6 Equipment, method and test parameters used including: Displacement amplitude, strain frequency, strain rate. 10.7 Plot of storage modulus, loss modulus and tan delta (optional) versus temperature, the tangents A and B and the points C, L and M according to Figure 1. 10.8 Individual test results of Tg-onset, Tg-Ioss, Tg-peak (optional) and ( (optional). 10.9 Any incident which may have affected the results and any deviation from this standard.
13	Annex A (informative) Equipment A.1 PL-DMTA dynamic Mechanical Thermal Analyser A.2 981/982/983 DMA Dynamic Mechanical Analyser A.3 A.T.M. 3 torsion Pendulum, A.4 Torsiomatic torsion Pendulum, A.5 RDS 7700

Additional information

Status	Definitive
Pages	16
Publication Date	2015-11-30
ISBN	978 0 580 82984 0
Standard Number	BS EN 6032:2015
Title	Aerospace series. Fibre reinforced plastics. Test method. Determination of the glass transition temperatures
Identical National Standard Of	EN 6032:2015
Descriptors	Reinforced materials, Air transport engineering, Specimen preparation, Plastics, Reinforcing materials, Fibres
Publisher	BSI
Committee	ACE/65
ICS Codes	49.025.40 - Rubber and plastics

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BS EN 6032:2015

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