Discussion Overview
The discussion revolves around the feasibility of building a device similar to a helicopter that can lift approximately 75 lbs using a fan system. Participants explore the necessary specifications for the fan diameter, RPM, torque requirements for an electric motor, and the overall design considerations for achieving the desired lift height of 1 to 1.5 feet off the ground.
Discussion Character
- Exploratory
- Technical explanation
- Debate/contested
Main Points Raised
- One participant expresses a desire to learn about the physics and engineering required to lift 75 lbs with a fan system, specifying a preference for a 2 ft diameter fan.
- Another participant warns that lifting 75 lbs with a 2 ft diameter fan is not feasible and raises safety concerns regarding the potential dangers of such a project.
- Some participants suggest that the required torque and RPM of the motor are more critical than the RPM alone, emphasizing the importance of rotor assembly weight and balance.
- Concerns are raised about the structural integrity of a fan operating at high RPMs, including potential failures of bearings and the fan itself under load.
- Participants discuss the airflow requirements and the implications of restricting airflow, with one arguing that it would hinder performance rather than help.
- One participant references a specific example of thrust generated by a larger propeller at lower RPMs, suggesting that the OP should consider different configurations.
- There are discussions about the costs and complexities associated with using turbine engines, with some participants cautioning against the OP's lack of technical background for such systems.
Areas of Agreement / Disagreement
Participants generally disagree on the feasibility of the OP's project, with many asserting that lifting 75 lbs with the specified parameters is unrealistic. There is no consensus on a viable approach, and multiple competing views on the requirements and safety considerations remain.
Contextual Notes
Participants highlight limitations related to the OP's understanding of the physics involved, the need for safety precautions, and the technical specifications required for successful lift. There are unresolved mathematical and engineering considerations regarding torque, RPM, and thrust generation.