A novel bondline architecture for bonded composite joints is presented. By implementing a distinct rather ductile thermoplastic phase, a physical barrier for growing disbonds is obtained and thus a more fail-safe design, respectively. Furthermore, the joint is established by using two different joining technologies, namely adhesive bonding and thermoset composite welding. A possible manufacturing technique is briefly described and assessed by means of Double Cantilever Beam (DCB) and Single Lap Shear (SLS) tests. The thermoplastic phase constrains disbonds by posing a physical barrier through a discrete change of materials. Thus, a significant increase against crack propagation is observed for DCB tests. However, visual examinations of th...
The approach for joining thermosetting matrix composites (TSCs) proposed in this study is based on t...
<p>The approach for joining thermosetting matrix composites (TSCs) proposed in this study is based o...
Induction welding is an effective technique for joining unidirectional carbon fiber reinforced therm...
Based on the experience in the past and the occurrence of in-service damages, the authorities restri...
Based on the experience in the past and the occurrence of in-service damages, the authorities restri...
Bonded composite joints have many advantages in comparison to conventional fasteners. However, adhes...
The capability of joining two thermoplastic composite parts by welding is a key technology to reduce...
Modern aerospace structures see increasing use of combinations of thermoplastic and thermoset compos...
Single-lap shear (SLS) joints are straightforward to manufacture. This makes them especially attract...
Nowadays bonded joints are state of the art in the assembly of composite aircraft structures. Due to...
Many complex structures such as airplanes are made of dissimilar materials, combining for instance C...
Many complex structures such as airplanes are made of dissimilar materials, combining for instance C...
The use of composite materials in aircraft manufactures increases more and more with the need of lig...
Modern aerospace structures see increasing use of combinations of thermoplastic and thermoset compos...
Research into the fusion bonding of joints containing thermoplastic and/or thermoset composites. A t...
The approach for joining thermosetting matrix composites (TSCs) proposed in this study is based on t...
<p>The approach for joining thermosetting matrix composites (TSCs) proposed in this study is based o...
Induction welding is an effective technique for joining unidirectional carbon fiber reinforced therm...
Based on the experience in the past and the occurrence of in-service damages, the authorities restri...
Based on the experience in the past and the occurrence of in-service damages, the authorities restri...
Bonded composite joints have many advantages in comparison to conventional fasteners. However, adhes...
The capability of joining two thermoplastic composite parts by welding is a key technology to reduce...
Modern aerospace structures see increasing use of combinations of thermoplastic and thermoset compos...
Single-lap shear (SLS) joints are straightforward to manufacture. This makes them especially attract...
Nowadays bonded joints are state of the art in the assembly of composite aircraft structures. Due to...
Many complex structures such as airplanes are made of dissimilar materials, combining for instance C...
Many complex structures such as airplanes are made of dissimilar materials, combining for instance C...
The use of composite materials in aircraft manufactures increases more and more with the need of lig...
Modern aerospace structures see increasing use of combinations of thermoplastic and thermoset compos...
Research into the fusion bonding of joints containing thermoplastic and/or thermoset composites. A t...
The approach for joining thermosetting matrix composites (TSCs) proposed in this study is based on t...
<p>The approach for joining thermosetting matrix composites (TSCs) proposed in this study is based o...
Induction welding is an effective technique for joining unidirectional carbon fiber reinforced therm...