Abstract
The present paper investigates the generation of cure induced residual stresses during the cure stage of the Vacuum Assisted Resin Transfer Moulding (VARTM) process for the fabrication of ultra-thick components (i.e. 105 mm) for wind turbine blades manufacturing (i.e. root insert). The viscous-elastic material characterisation of the Airstone 780E epoxy resin mixed with the 785H Hardener has been undertaken and the corresponding coupled thermo-mechanical simulation has been implemented using a commercial FE solver. The finding points out that the level of residual stresses generated during the cure stage leads to a spring-in of about 1.3 cm when Manufacturer Recommended Cure Cycle is applied and that improvements in both spring-in and cure time can be obtained by applying different cure cycles.
Original language | English |
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Title of host publication | Proceedings of 2nd CIRP Conference on Composite Material Parts Manufacturing, Sheffield (UK), 2019 |
Editors | Kevin Kerrigan, Paul Mativenga, Hassan El-Dessouky |
Publisher | Elsevier |
Pages | 7-11 |
Number of pages | 5 |
Volume | 85 |
DOIs | |
Publication status | Published - 2019 |
Event | 2nd CIRP Conference on Composite Material Parts Manufacturing - Sheffield, United Kingdom Duration: 10 Oct 2019 → … Conference number: 2 |
Publication series
Name | Procedia CIRP |
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Publisher | Elsevier |
ISSN (Print) | 2212-8271 |
Conference
Conference | 2nd CIRP Conference on Composite Material Parts Manufacturing |
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Abbreviated title | 2nd CIRP CCMPM |
Country/Territory | United Kingdom |
City | Sheffield |
Period | 10/10/19 → … |
Keywords
- Composite
- VARTM
- Thermo-mechanical properties
- Springback