Discussion Overview
The discussion revolves around the feasibility of designing a vertical lift engine capable of hovering and lifting approximately 30 pounds while adhering to specific constraints, including a weight limit for the engine itself and minimal power consumption. Participants explore various concepts, including drone technology, hovercraft designs, and alternative aerodynamic effects.
Discussion Character
- Exploratory
- Technical explanation
- Debate/contested
- Conceptual clarification
Main Points Raised
- One participant proposes designing a vertical lift engine that weighs 5 pounds or less and consumes 1-3 kW of power to lift 30 pounds one foot off the ground.
- Some participants suggest that achieving hover with a drone-like design may be possible, referencing existing drones that can lift similar weights.
- There is a discussion about the potential benefits of incorporating a skirt to reduce power requirements, with some arguing that a skirtless design may lead to inefficiencies.
- One participant expresses a preference for a skirtless design for aesthetic reasons and explores alternative aerodynamic concepts like blown wings and momentum curtains.
- Concerns are raised about the efficiency of a smaller footprint design compared to larger multi-rotor configurations, with some participants questioning the feasibility of the proposed constraints.
- There is a debate about the definition of a "lift engine," with participants suggesting various mechanisms, including motor-driven propellers and aerodynamic devices.
- Some participants highlight the importance of effective wing loading and the challenges of achieving stability with a single rotor design.
Areas of Agreement / Disagreement
Participants express differing views on the feasibility of the proposed design, with some believing it may be possible under certain conditions, while others argue that the constraints may render it impractical. No consensus is reached regarding the best approach or the definition of a lift engine.
Contextual Notes
Participants note limitations related to the efficiency of hovercraft designs, the impact of footprint size on performance, and the potential need for more powerful lift sources like gas turbines. There are unresolved questions about the specific requirements for the hover height and the implications of various design choices.