HEROPS aims to introduce climate-neutral propulsion into regional aircraft by developing MTU’s Flying Fuel Cell (FFC) propulsion system concept for entry into service in 2035. This disruptive hydrogen-electric propulsion system uses fuel cells as sole power source and a liquid hydrogen fuel system, without the need for high-power batteries. Integration of both the fuel cell system and the electric propulsion unit into a compact engine nacelle will ensure an efficient system at high power-to-weight ratio. HEROPS targets to demonstrate a 1,2 MW propulsion system based on a scalable 600 kW core module at TRL4. The core module and all further sub-systems will be validated up to TRL5. Complemented by simulation and electrical network testing of the overall modularised system, scalability to the 2 – 4 MW power level will be confirmed. The certification programme will build upon on-going certification activities, enabling timely maturation of the aviation-native HEROPS technology against relevant certification requirements. The two-phase approach of the overall programme - including extensive development, test and validation cycles at each stage - is expected to advance the FFC concept to TRL6 for integration and demonstration on a regional aircraft by 2028.
Hydrogen-Electric Zero Emission Propulsion System, HEROPS / Di Stasio, M., Della Vecchia, P.. - (2024). (Hydrogen-Electric Zero Emission Propulsion System 01/01/2024).
Hydrogen-Electric Zero Emission Propulsion System, HEROPS
mario di stasio;pierluigi Della Vecchia
2024
Abstract
HEROPS aims to introduce climate-neutral propulsion into regional aircraft by developing MTU’s Flying Fuel Cell (FFC) propulsion system concept for entry into service in 2035. This disruptive hydrogen-electric propulsion system uses fuel cells as sole power source and a liquid hydrogen fuel system, without the need for high-power batteries. Integration of both the fuel cell system and the electric propulsion unit into a compact engine nacelle will ensure an efficient system at high power-to-weight ratio. HEROPS targets to demonstrate a 1,2 MW propulsion system based on a scalable 600 kW core module at TRL4. The core module and all further sub-systems will be validated up to TRL5. Complemented by simulation and electrical network testing of the overall modularised system, scalability to the 2 – 4 MW power level will be confirmed. The certification programme will build upon on-going certification activities, enabling timely maturation of the aviation-native HEROPS technology against relevant certification requirements. The two-phase approach of the overall programme - including extensive development, test and validation cycles at each stage - is expected to advance the FFC concept to TRL6 for integration and demonstration on a regional aircraft by 2028.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.


