FluidER project developed and delivered an integrated and autonomous system for sensing and diagnosis of aviation hydraulic fluids. The system enables to have an early warning of degradation signs, in terms of particulate count, viscosity, AN, and water contamination, before the hydraulic fluids exceeds the service limits. The information obtained from the different sensors is used to generate a Diagnosis of the status of both, the fluid itself and the HA equipment, through new health monitoring algorithms.
The integration of health monitoring technologies add intelligence into the system ensuring robust data transmission, meet the reliability requirements and endure environmental requirements from aircraft equipment.
The maintenance cost will be reduced, and maintenance operations will be improved. It is common in the industry to send fluid samples to analyze in laboratory, with the Fluider system this will be reduced.Besides there is an additional advantage, the time to obtain the health state of the fluid is reduced, as the results will be obtained in a matter of minutes, instead of days. Having the Fluider system may increase the number of analysis, as some analysis may not be done because cost or time drawbaks. This has the potential to improve maintenance cost and efficiency of operations.
FluidER system improves Hydraulic Actuators (HA) systems efficiency in terms of:
- Reduced HA maintenance cost and improve maintenance operations efficiency
- Preventing detrimental effects on the equipment lifetime: Preventive and predictive maintenance
- Increased reliability of the hydraulic fluid health monitoring data
- Increased life length of hydraulic actuators
FluidER is completely aligned with the Systems ITD targets (reduction of CO2, NOx, noise) by the improvement of competitiveness contribution to the introduction of full electrical actuator and the reduction of maintenance costs and increase the system data reliability.
FluidER contributes in the WP4.1 “Advanced Landing Systems” and its target of achieving “full electrical main landing gear” by the improvement of the HA reliability and safety and life extension.