EN 2850:2017
Current
The latest, up-to-date edition.
Aerospace series - Carbon fibre thermosetting resin - Unidirectional laminates - Compression test parallel to fibre direction
18-10-2017
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 |
| PNE-FprEN 2850 | 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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