Engine Power required to lift the Helicopter?

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To design an RC helicopter capable of lifting 25 to 30 kg, the required engine power can be estimated using specific calculations. The force needed for lift is calculated as 294.3 N based on the mass and gravity. Key formulas include calculating the area of the blades, power loading, and thrust loading, with the understanding that 10-15% of the power will be consumed by the tail rotor. The relationship between engine power and blade area is essential for accurate estimations. Understanding aerodynamic principles is crucial for approximating the necessary power for effective helicopter design.
bhaazee
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I want to design a RC helicopter powered by a gas engine. The total mass to be lifted by the helicopter is 25 to 30 Kg. What is the engine power or engine size (in cc) required to lift the helicopter? Can someone please provide me some calculation?

Regards
 
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It would be useful to know the gear ratio involved in going from the engine to the blades.
However once you know this and the power the following formula should help.

Force required to lift = MA = 30*9.81 = 294.3 N

1. Calculate Area of Blades A = Pi*r^2 (ft^2)
2. Calculate Power Loading PL = Power/A
3. Calculate Thrust Loading TL = 8.6859*PL^(-0.3107)
4. Lift = TL * Power

Be aware that 10 - 15% of the power will be used by the tail rotor.

Hope this is useful and gives you a rough idea.
Steve
 
Thnx for the formulae. I have been going through the aerodynamic principles of helis. The relaions are quiet complicated to approximate the values and to find the power required.

Regards
 
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