Hi,
I was viewing the T200 thruster Excel technical data when I start thinking about relation about the data values in it
From what I understand the relation between RPM and thrust seems to be fixed (accounting for statistical errors)
So I started comparing similar RPM/Thrust values from 3 different voltages on T200 like this:
(I choose to compare this part of data because is at the maximum PWM for 12v but of course less than maximum for other voltages)
PWM RPM A V W Kgf g/W
1900 2995 16.91 12 202.9 3.71 18.3
1816 3002 13.54 16 216.6 3.74 17.3
1800 2985 13.12 18 236.2 3.72 15.8
1792 3013 13.47 20 269.4 3.72 13.8
The first thing that i noted is that, for the same RPM/Thrust, as voltage increases the amperage decrease but not proportionally so the power consumption is higher and the efficiency is going down
- Where is these energy wasted? Losses of the motor or ESC that tends to be less efficient at less than 100% throttle?
From technical data:
Full Throttle Current (Power) @ 12 V 17 Amps (205 Watts)
Full Throttle Current (Power) @ Nominal (16 V) 24 Amps (390 Watts)
Full Throttle Current (Power) @ Maximum (20 V) 32 Amps (645 Watts)
- Why if is the voltage increasing the Full Throttle Current is increasing too?
If I understand correct the ESC only limit and regulate the voltage but not the current
I read that more than 20v is not recommended
- Is it possible for example supply it with 20v and just limit the maximum output of PWM ex. 1792 for 20v?
- Could the power control reduced range is bad affecting piloting and maneuvering?
- Is it still less efficient than use a lower voltage, right?
You will forgive me but my knowledge of electric motors is still WIP
Thank you