In comparison to bolted joints, structural bonds are the desirable joining method for light-weight composite structures. To achieve a broad implementation of this technology in safety critical structures, the issues of structural bonds due to their complex and often unpredictable failure mechanisms have to be overcome. The proposed multifunctional bondline approach aims at solving this by adding two safety mechanisms to structural bondlines. These are a design feature for limiting damages to a certain size and a structural health monitoring system for damage detection. The key question is whether or not the implementation of both safety features without deteriorating the strength in comparison to a healthy conventional bondline is possible....
Structural Health Monitoring deals mainly with sensorized structures where sensors can be secondary ...
This article outlines a statistical damage detection engine for the automated characterization of di...
Composite bonded structure is a prevalent portion of today’s aircraft structure. Adequate bond integ...
Based on the experience in the past and the occurrence of in-service damages, the authorities restri...
Disbond arrest features combined with a structural health monitoring system for permanent bondline s...
The use of composite materials in aircraft manufactures increases more and more with the need of lig...
A novel bondline architecture for bonded composite joints is presented. By implementing a distinct r...
Bonded composite joints have many advantages in comparison to conventional fasteners. However, adhes...
Structural health monitoring (SHM) technology may be applied to composite bonded repairs to enable t...
The use of composite structures in engineering applications has proliferated over the past few decad...
Structural health monitoring (SHM) technology may be applied to composite bonded repairs to enable t...
A novel, purpose-designed, thin interlayer glass/carbon-epoxy hybrid composite sensor concept is pre...
This paper introduces the concept of a fail-safe sensor to monitor the structural health of a compos...
An integrable sensor inlay for monitoring crack initiation and growth inside bondlines of structural...
In the development of materials used for constructing aircraft, progress has been made in the produc...
Structural Health Monitoring deals mainly with sensorized structures where sensors can be secondary ...
This article outlines a statistical damage detection engine for the automated characterization of di...
Composite bonded structure is a prevalent portion of today’s aircraft structure. Adequate bond integ...
Based on the experience in the past and the occurrence of in-service damages, the authorities restri...
Disbond arrest features combined with a structural health monitoring system for permanent bondline s...
The use of composite materials in aircraft manufactures increases more and more with the need of lig...
A novel bondline architecture for bonded composite joints is presented. By implementing a distinct r...
Bonded composite joints have many advantages in comparison to conventional fasteners. However, adhes...
Structural health monitoring (SHM) technology may be applied to composite bonded repairs to enable t...
The use of composite structures in engineering applications has proliferated over the past few decad...
Structural health monitoring (SHM) technology may be applied to composite bonded repairs to enable t...
A novel, purpose-designed, thin interlayer glass/carbon-epoxy hybrid composite sensor concept is pre...
This paper introduces the concept of a fail-safe sensor to monitor the structural health of a compos...
An integrable sensor inlay for monitoring crack initiation and growth inside bondlines of structural...
In the development of materials used for constructing aircraft, progress has been made in the produc...
Structural Health Monitoring deals mainly with sensorized structures where sensors can be secondary ...
This article outlines a statistical damage detection engine for the automated characterization of di...
Composite bonded structure is a prevalent portion of today’s aircraft structure. Adequate bond integ...