Details
| Original language | English |
|---|---|
| Article number | 012006 |
| Number of pages | 11 |
| Journal | IOP Conference Series: Materials Science and Engineering |
| Volume | 942 |
| Issue number | 1 |
| Publication status | Published - 23 Oct 2020 |
Abstract
Keywords
- adhesive, failure, manufacturing, residual stress, in situ properties, thermal imaging, digitalization, composite
ASJC Scopus subject areas
Sustainable Development Goals
Cite this
- Standard
- Harvard
- Apa
- Vancouver
- BibTeX
- RIS
In: IOP Conference Series: Materials Science and Engineering, Vol. 942, No. 1, 012006, 23.10.2020.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
T1 - ReliaBlade Project
T2 - A Materials Perspective towards the Digitalization of Wind Turbine Rotor Blades
AU - Sayer, Florian
AU - Antoniou, Alexandros
AU - Goutianos, Stergios
AU - Gebauer, Ingo
AU - Branner, Kim
AU - Balzani, Claudio
N1 - Funding Information: Fraunhofer IWES and Leibniz University Hannover acknowledge the support provided by the German Federal Ministry for Economic Affairs and Energy (BMWi) grant 0324335A and 0324335B and DTU Wind Energy acknowledge the support from the Danish Energy Agency through the EUDP grant 64018-0068. Both grants is within the joint ReliaBlade project.
PY - 2020/10/23
Y1 - 2020/10/23
N2 - In many industries, digitalization is expected to have a significant economic potential. The digitalization of wind turbine rotor blades including their materials could contribute to accelerate the development of novel and tailored materials, to improve the blades’ reliability, and to make wind energy more cost efficient. However, the digitalization of the blades through their entire life cycle is challenging e.g. due to the dependence of the material properties on the manufacturing process parameters, the complex structural health monitoring and the challenging modelling of blade response under complex loading. In the presented work based on the results of the ReliaBlade project, a theoretical approach is attempted towards describing the blade insitu structural performance, based on the material properties, the blade manufacturing processes and loading history. In the first phase of the ReliaBlade project, an experimental blade for fullscale testing with three pre-defined internal damage modes is designed. Based on these damage modes the digitalization approach towards increasing the blade structural reliability is exemplarily shown.
AB - In many industries, digitalization is expected to have a significant economic potential. The digitalization of wind turbine rotor blades including their materials could contribute to accelerate the development of novel and tailored materials, to improve the blades’ reliability, and to make wind energy more cost efficient. However, the digitalization of the blades through their entire life cycle is challenging e.g. due to the dependence of the material properties on the manufacturing process parameters, the complex structural health monitoring and the challenging modelling of blade response under complex loading. In the presented work based on the results of the ReliaBlade project, a theoretical approach is attempted towards describing the blade insitu structural performance, based on the material properties, the blade manufacturing processes and loading history. In the first phase of the ReliaBlade project, an experimental blade for fullscale testing with three pre-defined internal damage modes is designed. Based on these damage modes the digitalization approach towards increasing the blade structural reliability is exemplarily shown.
KW - adhesive
KW - failure
KW - manufacturing
KW - residual stress
KW - in situ properties
KW - thermal imaging
KW - digitalization
KW - composite
UR - http://www.scopus.com/inward/record.url?scp=85096505519&partnerID=8YFLogxK
U2 - 10.1088/1757-899X/942/1/012006
DO - 10.1088/1757-899X/942/1/012006
M3 - Article
VL - 942
JO - IOP Conference Series: Materials Science and Engineering
JF - IOP Conference Series: Materials Science and Engineering
SN - 1757-8981
IS - 1
M1 - 012006
ER -