The QUICK project will develop and demonstrate a novel, highly robust and reliable fault detection and mechanical isolation system to mitigate the risks of potentially highly dissipative failure modes associated with the high-performance electrical power generator technologies required for future energy-optimised aircraft.
The main objectives are:
- To define the initial requirements and a preliminary architecture of the QUICK system
- To identify and define the concept for the shaft coupling and the overall actuator, through the results of initial mechanical analyses and studies that include characterisation and considerations of available materials
- To define and develop the pre-final concept of the disconnect system, known as Version 1 prototype, including all the accessories, sensors, signal processing and data acquisition systems, all on the basis of reliability analysis
- To accurately model and simulate the behaviour of the whole set-up in order to assess all the operation effects are in play
- To define the actuation and coupling aspects of the QUICK system based on the results of a full mechanical and operational analyses
- To prototype, test and validate a full version of the whole QUICK system in a laboratory environment
- To integrate a working prototype into a realistic environment and thus be able to test and validate the concept in a realistic environment