Hi there folks
Here´s a challenge for powerful minds.
I have a 2KW H-type VAWT with the following characteristics:
Alternator: 48V 3-phase AC (i think its DELTA)
Rotor diameter: 2 m
Blade Height: 2,60 m
Chord length: 0,29 m
Blades: 5
Blade Shape: NACA 0018
Blade area: 3,77 m2
Swept Area: 5,26 m2
Start speed: 3 m/s
Average wind: 11 m/s
Measured TSR: 1.3
Offcourse, the damn thing is only producing 300 watts (54V - 5 amps) at most... and i strongly believe i have a rotor/alternator missmatch. The alt is indeed 2KW (verified) so i focused on the blades... I fine tuned the pitch of the blades to the best angle by trial and error and it climbed from 80 RPM to 130 RPM.
I verified the alternator on a test and it needs to run at 220 RPM to produce 2KW, which i will never reach with this blades unless a hurricane passes over my house. So I figured if i re-build the blades (make them 30% bigger) i might just give the alternator what it needs to run on its full potential.
Having 11 m/s... how would you guys modify the rotor size, blade size and chord length in order to deliver 220 RPM to that thing? I need to achieve a 40% increase in TSR while mantaining the torque and inertia....
Should i build a rotor with lower solidity? or increase the total blade area to get more power (torque) delivered to the alternator?
I´m well aware the problem of low solidity blades is that they have a higher TSR while unloaded, but when loaded they will drop to half the TSR and deliver less torque.... and this is a big, fat, torque-hungry alternator.... So i´m frankly stuck trying to figure this out.
I spent the last 4 days reading about blade design (mostly incomplete theory) and NOBODY seems to have clear concepts, or a specific set of equations and specific guidelines to design Vawt blades proportional to an alternator.
Any ideas?
Pedro