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CEN
EN 2850:2017

EN 2850:2017

Current

Current

The latest, up-to-date edition.

Aerospace series - Carbon fibre thermosetting resin - Unidirectional laminates - Compression test parallel to fibre direction

Published date

18-10-2017

Publisher

Comite Europeen de Normalisation

European foreword
1 Scope
2 Normative references
3 Principle of the method
4 Terms and definitions
5 Designation
6 Test pieces
7 Apparatus
8 Conditioning
9 Procedure
10 Calculation of results
11 Validity
12 Test report
Annex A (normative)
Annex B (normative)
Annex C (informative)

This European Standard defines a method for the determination of stress at failure and Young's modulus in compression of carbon thermosetting resin unidirectional laminates.The method only covers test pieces the axis of which is parallel to the fibre direction.This method covers fibres (or fabrics) other than carbon, when the relevant technical specification explicitly mentions it.

Committee
ASD-STAN
DevelopmentNote
Supersedes PREN 2850. (11/2017)
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current
Supersedes

Standards Relationship
NF EN 2850 : 2017 Identical
DIN EN 2850:1998-04 (Draft) Identical
UNI EN 2850 : 2017 Identical
ONORM EN 2850 : 2017 Identical
NEN EN 2850 : 2017 Identical
SN EN 2850:2018 Identical
I.S. EN 2850:2017 Identical
NS EN 2850 : 2017 Identical
BS EN 2850:2017 Identical
SS EN 2850:2018 Identical
PN EN 2850 : 2018 Identical
UNE-EN 2850:2017 Identical

93/706616 DC : 0 PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL
PREN 2833-1 : 200P2 AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS
SAE AMS 2980/1 : 2014 CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS

EN 2565:2013 Aerospace series - Preparation of carbon fibre reinforced resin panels for test purposes
EN 3783:2013 Aerospace series - Fibre composite materials - Normalisation of fibre dominated mechanical properties
EN 2823:2017 Aerospace series - Fibre reinforced plastics - Determination of the effect of exposure to humid atmosphere on physical and mechanical characteristics
PREN 2372 : 2 AEROSPACE SERIES - NUTS, HEXAGON, THIN, STEEL, CADMIUM PLATED - CLASSIFICATION: 1 100 MPA/235 DEGREES C
EN 2489 : 1995 AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE ACTION OF TEST FLUIDS
EN 2859:2006 Aerospace series - Bolts, normal hexagonal head, close tolerance normal shank, short thread, in alloy steel, cadmium plated, metric series - Classification: 1 100 MPa (at ambient temperature) / 235 °C
EN 2744:1992 Aerospace series - Non metallic materials - Preferred test temperatures
EN 2743:2001 Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials
EN 3228:2010 Aerospace series - Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated - Classification: 900 MPa (at ambient temperature) / 235 °C

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