The generation of data-driven prognostics models requires the availability of datasets with run-to-failure trajectories. In order to contribute to the development of these methods, the dataset provides a new realistic dataset of run-to-failure trajectories for a small fleet of aircraft engines under realistic flight conditions. The damage propagation modelling used for the generation of this synthetic dataset builds on the modelling strategy from previous work [1] and incorporates two new levels of fidelity. First, it considers real flight conditions as recorded on board of a commercial jet [2]. Secondly, it extends the degradation modelling by relating the degradation process to the operation history. The dataset was generated with the Commercial Modular Aero-Propulsion System Simulation (C-MAPSS) dynamical model [3]. More details about the generation process can be found in [4].
Aircraft Engine Run-To-Failure Data Set Under Real Flight Conditions
2020-04-20
Miscellaneous
No indication
English
Aircraft turbine engine emissions under simulated supersonic flight conditions
Tema Archive | 1974
|Aircraft Engine Emissions Measurements at Simulated Flight Altitude Conditions
British Library Conference Proceedings | 1997
|