PREN 6040 : 200P1
Current
The latest, up-to-date edition.
AEROSPACE SERIES - NON-METALLIC MATERIALS - TEST METHOD - ANALYSIS OF THERMOSET SYSTEMS BY HIGH PERFORMANCE - LIQUID CHROMATOGRAPHY (HPLC)
Hardcopy , PDF
English
15-12-1995
1 Scope
2 Normative references
3 Abbreviations
4 Principle of the method
5 Designation of the method
6 Apparatus
7 Test specimen
8 Procedure
9 Presentation of the results
10 Test report
Gives the procedure to be used for the determination of the composition (curing-agent/catalyst, modifier, resin, reaction products) of the soluble components of thermoset systems with or without reinforcement in the uncured state using High Performance Liquid Chromatography (HPLC). Also applies to: sizing systems; fibre reinforced matrix systems (such as prepreg); neat resin systems (such as film adhesives, laminating systems and components such as epoxy resins and hardeners.
| Committee |
AIB/TF6
|
| DocumentType |
Draft
|
| Pages |
10
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Current
|
| Standards | Relationship |
| NF EN 6040 : 2017 PR | Identical |
| DIN EN 6040:2017-06 (Draft) | Identical |
| PREN 6085 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - EPOXY SURFACING FILMS |
| BS EN 4106:2013 | Aerospace series. Non-metallic materials. Structural adhesive systems. Paste adhesive. Technical specification |
| PREN 6084 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - SURFACING FILMS - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS |
| PREN 6044-2 : 200P1 | AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - QUALIFICATION PROGRAMM/BATCH RELEASE TESTING - UNIDIRECTIONAL TAPE 180 DEGREE C CURING CLASS |
| PD CEN/TR 14548:2003 | Adhesives. Guide to test methods and other standards for the general requirements, characterization and safety of structural adhesives |
| SAE AMS3970/3A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Carbon Prepreg |
| PREN 2833-1 : 200P2 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS |
| PREN 6044-1 : 200P1 | AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS |
| PREN 4106 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| SAE AMS2950/1 | Paste Adhesive for Core Restoration Part 1 - General Requirements |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| I.S. CEN TR 14548:2003 | ADHESIVES - GUIDE TO TEST METHODS AND OTHER STANDARDS FOR THE GENERAL REQUIREMENTS, CHARACTERIZATION AND SAFETY OF STRUCTURAL ADHESIVES |
| EN 4106:2013 | Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification |
| I.S. EN 4106:2013 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| 00/702576 DC : 0 | PREN 4107 - AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - FOAMING ADHESIVES - TECHNICAL SPECIFICATION |
| CEN/TR 14548:2003 | Adhesives - Guide to test methods and other standards for the general requirements, characterization and safety of structural adhesives |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
| PREN 2559 : 1988 | CARBON FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF THE RESIN AND FIBRE CONTENT AND THE MASS OF FIBRE PER UNIT AREA |
| EN 2331:1993 | Aerospace series - Textile glass fibre preimpregnates - Test methods for the determination of the resin and fibre content and mass of fibre per unit area |
Access your standards online with a subscription
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.