SUMMARY
The discussion centers on the feasibility of designing a vertical lift engine capable of hovering with a payload of 30 pounds while weighing no more than 5 pounds and consuming between 1-3 kW of power. Participants emphasize that achieving this goal may require innovative approaches beyond traditional drone designs, such as incorporating hovercraft technology or exploring aerodynamic effects like blown wings and the Coanda effect. The consensus suggests that using a skirt could significantly enhance efficiency, reducing power requirements and improving stability. However, the constraints of a small footprint and low power raise concerns about the overall viability of the project.
PREREQUISITES
- Understanding of vertical lift mechanisms and their power requirements
- Familiarity with drone payload capabilities and engine specifications
- Knowledge of hovercraft technology and its efficiency factors
- Basic principles of aerodynamics, including the Coanda effect and momentum curtains
NEXT STEPS
- Research the specifications and capabilities of heavy-lift drones, such as the Freefly Systems Alta 8
- Explore hovercraft design principles, focusing on skirt efficiency and pressure dynamics
- Investigate aerodynamic effects like blown wings and the Magnus effect for potential lift solutions
- Analyze power requirements and efficiency calculations for various lift mechanisms, including electric motors and propellers
USEFUL FOR
Engineers, hobbyists, and researchers interested in vertical lift technology, drone design, and innovative propulsion systems seeking to optimize power efficiency and payload capacity.