DESIGN: AeroVantage ~ Motor - Full-size - Cooling

• General:
• Pump:
• How is it to be driven? It could be practical to drive it of the main motor.
• Should its flow volume vary with the temperature of the coolant?
• Front PropRotor:
• Radiator:
• Consider of having two or four of the arms of the transition mechanism serve as the radiator.
• The arms will be cooled by the downwash of the PropRotor during cruise..
• The forward facing openings, on each side of the fuselage, could serve as inlets to transfer the remote velocity airflow to the arms, which are enclosed in the fuselage.
• Rear PropRotor:
• Free air flows between motor and cladding to a radiator that is located just behind.
• A fan could be part of the rotor hub and its vanes could be spring loaded and have their pitch increase as the remote velocity increases.
• Radiator:
• Wild idea; Consider having the cladding act as the radiator, with the air flowing from inside to outside and become the boundary flow???

Same Page ~ Different Craft: ~

General Information: ~ OTHER: Electrical - Motor - Cooling

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