Calling airship designers to consider various solutions for fueling light Vertical Takeoff and Landing (VTOL) aircraft, in relation with the focus on electric propulsion systems due to the Energy Resilience Challenge section which is about deploying microgrid technologies. Here are the key takeaways for fueling these light VTOL aircraft:
Distributed Electric Propulsion (DEP): This is the preferred method as it splits the propulsion system into multiple electric motors and propellers/fans. This offers redundancy, improved efficiency in both vertical flight and forward flight, and allows for a compact design. (mentioned in Aeroteq - 007, 008, 009)
Thrust Augmentation: This technique uses the relative position between the thrust-producing element (propeller/fan) and the wings or fuselage to increase lift and reduce battery weight. This is crucial for electric VTOL as battery weight is a major limitation. (mentioned throughout the document)
Reduced Rotor Footprint: Designs that protect rotors or minimize their footprint during takeoff and landing are highlighted for safety reasons, especially in urban environments. (mentioned in Aeroteq - 001, 002, 005, 006, 010)
Here's a table summarizing the most promising VTOL concepts presented:
Could alternative solutions like gasoline engines and multi-rotor configurations be made more efficient while overcoming safety concerns?
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