EN 3783:2013
Current
Current
The latest, up-to-date edition.
Aerospace series - Fibre composite materials - Normalisation of fibre dominated mechanical properties
Published date
21-08-2013
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Foreword
1 Scope and field of application
2 Normative references
3 Principle
4 Designation
5 Procedure
6 Test report
This standard describes the procedure for normalisation of fibre dominated mechanical properties. The procedure is valid for carbon, glass and aramid reinforced laminates.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 3783. (09/2013)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NF EN 3783 : 2015 | Identical |
| NBN EN 3783 : 2013 | Identical |
| NEN EN 3783 : 2013 | Identical |
| NS EN 3783 : 2013 | Identical |
| I.S. EN 3783:2013 | Identical |
| PN EN 3783 : 2013 | Identical |
| BS EN 3783:2013 | Identical |
| DIN EN 3783:2013-12 | Identical |
| UNE-EN 3783:2013 | 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 |
| I.S. EN 2833-005:2013 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| EN 2850:2017 | Aerospace series - Carbon fibre thermosetting resin - Unidirectional laminates - Compression test parallel to fibre direction |
| BS EN 2850:2017 | Aerospace series. Carbon fibre thermosetting resin - Unidirectional laminates. Compression test parallel to fibre direction |
| 95/714421 DC : 0 | PREN 2833-3 - AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 180 DEGREE C FOR CONTINUOUS USE UP TO 120 DEGREE C |
| EN 2833-005:2013 | Aerospace series - Glass fibre thermosetting preimpregnates - Technical specification - Part 005: Glass fabric/phenolic resin preimpregnate |
| 93/711194 DC : 0 | PREN 2833-2 - TECHNICAL SPECIFICATION - GLASS FIBRE THERMOSETTING PREIMPREGNATES - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| BS EN 2833-005:2013 | Aerospace series. Glass fibre thermosetting preimpregnates. Technical specification Glass fabric/phenolic resin preimpregnate |
| 95/714422 DC : 0 | PREN 2833-4 - AEROSPACE SERIES - GLASS FIBER THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREE C FOR CONTINUOUS USE UP TO 80 DEGREE C |
| PREN 2833-4 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| I.S. EN 2850:2017 | AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN - UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION |
| EN 2329:1993 | Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of mass per unit area |
| EN 2557:1997 | Aerospace series - Carbon fibre preimpregnates - Determination of mass per unit area |
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