11.30 Max_Wilbrink - AeroDelft.pdf

1、The content in this document is private and confidential.Do not share this document unless specifically authorized by AeroDelft.The MissionProve and promote liquid hydrogen as an alternative to conventional fuels in aviation.“”Founded in 201857 active students35%full time students55.000 work hours a

2、nnuallyNot just Aerospace Engineers400 AlumniThe TeamProject FS Phoenix Project FS PHOENIXGoals:To fly on gaseous hydrogen(GH2)in 2025To fly on liquid hydrogen(LH2)in 2026The AircraftSling 4,Sling AircraftMTOW:920 kgFuel cell electric vehicleMaximum power:95 kWWingspan:9.97 mPermit to Fly CS23Mass o

3、f GH2:2.1 kgMass of LH2:5.3 kgElectric Taxi Test Gaseous Hydrogen Powertrain TestbedUpgraded Testbed Liquid Hydrogen Scaled TestbedThermal Management 49%efficiencyFuel Cell Stack110 kW115 kWTemperature range 65-80 CAeroDelft TMS Challenges Limited space for radiators Optimising aerodynamic design of

4、 ducts&nose cowling Routing of coolant loops Integration into the aircraft Cooling requirements verification Integration with liquid hydrogen systemTMS Wind Tunnel TestingTMS Wind Tunnel TestingFurther steps before first flight on GH2Full flight profile test on gaseous hydrogen-Winter 2024/25 Second wind tunnel test to qualify TMS-March 2025System integration into the aircraft-Spring 2025(High speed)taxi test on gaseous hydrogen-Summer 2025