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Author Topic: Motor selection factors  (Read 1039 times)

Online Dennis Toth

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Motor selection factors
« on: November 19, 2009, 06:49:18 AM »
Guys,

In selecting a motor for a particular size/weight ship I have tried the various "motor calc" programs and found that they don't really fit our situation. They don't allow part throttle (i.e. 70%) operation. The castle calculator can be fooled by adjusting the number of cells to reduce the voltage and I think this works.

Question: when selecting a motor what is the critical parameter  -   amps, watt rating or number of cells?   I thought that the amps would be the most important, then wattage rating. I have been looking at loading the motor (vary the prop size) to a particular static amps  at a particular rpm. It seems this would set the watts and if that fit within the motor spec the number of cells (3 or 4 lipos) would be immaterial. Is this right?

Best,          DennisT

Alan Hahn

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Re: Motor selection factors
« Reply #1 on: November 19, 2009, 10:39:52 AM »
Dennis,
You can fake out the motor programs by simply using 70% of your nominal battery voltage to get an idea about what is going on. That's what I do with DriveCalc.

Onto your question:

The easiest thing to do is just follow the glow tradition and ask others what they use. But here I will try to say a few things.

1) Motor kV and battery selection go hand in hand with rpm selection. Choosing one sets up the other. So that's relatively straight forward. I take nominal 3.7V/Cell, * number of cells*0.8*kV should equal where your rpm selection. You can use 0.7 intstead of 0.8 to be a little more conservative with headroom.

2) Motor size---Lets look at a AXI 2826 and a AXI 2820. They are basically identical designs, except the 2826 has a 26 mm long stator and 26 mm long magnets compared to the 20 mm ones of the 2820. If you wind each one with the same number of identical gauge copper wire, then the kV os the 2826 will roughly be 20/26 times lower than the 2820 motor. So to get the same kV, we would wind the longer motor with fewer number of copper turns. Since there are fewer turns, we can then increase the wire thickness (lower gauge) to fill up the same space.

What this means is that the 2826 motor now has the same kV as the 2820 with fewer winds and thicker wire---so its winding resistance is lower. At the same current to make the torque to turn the prop, the larger motor will make less heat. Sounds like a win-win situation! y1 Go for big!

But we left out the detail about magnetic losses  n1. Every time we commute the current in the motor, we are changing the field inside the stator. This itself creates heat (hysteresis and eddy current losses). The more iron in the motor the more the losses (at the same rpm). So here the bigger motor begins to lose. Also we are carrying around more weight to lift in the vertical.

If you look at the motor calculations, you will see that for any constant voltage input, there is a sweet spot--where the output/input power peaks (just efficiency). It is a relatively broad peak, and it seems to occur at about 80% or so of the max (no-load) rpm point. Above this rpm and magnetic losses dominate, and below it resistive losses dominate. I'd argue that you would like to sit at this sweet spot during level flight.

The efficiency at this sweet spot is on the order of 80% or so maybe higher or lower. So what this means it that if you are inputting 300 watts of power, 60 watts are going into heating up your motor. The main way to shed that heat is through the outer shell. Notice that a longer motor will have a bigger surface area to shed heat than the smaller motor (and also will most likely be a bit more efficient) and so will heat up less.

It is this heating that sets the manufacturer's rating of most motors. At some point, the motor can't shed the heat and things will begin to go downhill fast. Most of the magnets used in our motors will begin the lose (permanently) their magnetism as they heat up. If this occurs, the kV will begin to actually go up. kV rising allows more current to flow into the motor, raising the heating more......bad news time.


I think most of us in CL don't see this problem unless we severely undersize the motors. I use a Scorpion 3020 (similar to AXI 2820) in both my Vector and Nobler. I have used a 3014 in the Nobler, and it felt fine, temperature wise after a flight. It was a bit less efficient (harder on battery) but was also a less weight. I could probably use a 3008 in the Nobler and get away with it, although I would be more worried about efficiency than burning it up. If I flew bigger planes (like Strega), I am sure the 3020 would be on the small size, and 3026 would be a better choice. I am not sure I would need to go even longer to a 3032 or to the next diameter size up, a 40xx motor.

I would claim that for outrunners, most motors in the same size range like a 28xx or 30xx (these are stator diameter/lengths) are basically electrically equivalent in their non-stressed performance. And that is where I think we want to use them.

Sorry for running on so long!

Online Dennis Toth

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Re: Motor selection factors
« Reply #2 on: November 20, 2009, 05:47:19 AM »
Alan,

Thanks for the explanation, what I am trying to do is use 4S1p 2100mah pack in a smaller ship of about 36oz and 450 sq in. I have been looking at the AXI 2814-16 which weighs 3 3/4 oz. I have also been looking at the Scorpion 3014 and the Turnigy 35-xx in the same size range. The Scorpion is 4.4oz and the Turnigy is 3.8oz, the Turnigy has a max continuous amps of 23 which should work for this as I plan to use a 9" - 10" prop and adjust load to 18amps or so. However, in the Turnigy tech data it shows 3 lipos for this motor. If the amps stay at 18 and at this load the rpm is 70% of full no load does the # of cells present any problem?

Best,        DennisT

Alan Hahn

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Re: Motor selection factors
« Reply #3 on: November 20, 2009, 08:23:42 AM »
The short answer is it is amps that matter (probably what you wanted to hear from the first question!). This is basically a resistive heating issue.

There are some "details" because at partial throttle, the current you measure is the average current from the battery, but the heating is not equal to simply using the average current.

So to make your short question longer (!! y1), to really get a handle on what the motor is doing, imagine that you had the ESC hooked up to an adjustable power supply, and the throttle for the ESC was wide open. Then you would dial in the voltage to get the rpm you want to spin the prop at to make the power. The amps you measure there are the actual motor amps.

Now at partial throttle (and to make it easy, lets say you are running at 50% throttle). If you are measuring an average current of 20 amps, what actually is going on is that half the time the current is actually 40 amps, and the other half is zero amps. During the on time the heating is 4 times the heat you would get using the average to calculate the heat (since resistive heating goes as the square of the current). However during the off period there is no resistive heating. So the net heating is the average of 4 and 0 or 2, which means the actual heat is twice what you would have thought your average current was giving you. Thus the motor is seeing a heating equivalent to an effective current which is square root of 2 times (~1.4x) higher than what your average current measurement is.

At 70% throttle the effective heating would be like having a current sqrt(1/.7) or ~1.2 times higher than the average value.

So in your case, the 18 average amps at 70% would be like running 21 amps.

And now another comment--I don't think Turnigy gives you much margin, so I would say that it is too small for this application. What are the specs on the AXI and Scorpion? Scorpion should have a prop chart that would tell you how much current it is pulling statically with most props.

I fly my SuperClown (28oz) with a 3014 and a 10-7 prop, and it is ok. I use a 3s2100 pack for that. I have also flown my Nobler (44oz) with a 3014 and a 4s2100 pack, and as I recall, the motor didn't have any issues with that (but that was before I wrote this reply!).

Here are the Scorpion SII-3014-1040 motor prop charts for a 3s, and 4s/5s pack voltages. Notice that it is running WOT for voltages nominally consistent with the battery output voltage at load. The color code is given at the bottom of the 4s/5s graphic.

Online Dennis Toth

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Re: Motor selection factors
« Reply #4 on: November 20, 2009, 10:13:56 AM »
Alan,

Thanks, the average amp point is something I didn't think of, it makes lots of sense.

Best,            DennisT

Offline Howard Rush

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Re: Motor selection factors
« Reply #5 on: November 20, 2009, 10:47:19 AM »
I looked at that prop chart and wondered, of course, at what airspeed and density the testing was done.  Then I saw in the title, "Wind - 13T Delta (11 x 0.25mm Wire)"  I was puzzled at first, not recognizing that specification for wind speed.  Then I saw the wire part and realized that they were using a hot-wire anemometer to measure wind speed, and that T Delta must be some hot-wire anemometry standard.  It took about five minutes for me to figure out that it was a different wInd, at which point, as you Web people say, I LMAO.
The Jive Combat Team
Making combat and stunt great again

Offline walterbro

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Re: Motor selection factors
« Reply #6 on: November 20, 2009, 01:05:41 PM »
Hi Dennis - You mentioned that the motocalc programs don't allow you to use
different throttle options. I have been using MOTOCALC for the last 5years and always use the throttle option to check my rpm,pitch,speed,amps, volts,run time,
and flight climb performance. This works for single motors and twin motors.
  After you select compare, close that window and the next window will allow you to click on the throttle on the upper right of the screen. As you click the throttle drops 1% and shows all the calculated values for 99%. The next click 98% and so on. This will help in prop selection and motor comparisons. I also check my bench test values and project changes by using higher and lower throttle settings. You will need to know that static values is what is computed. Flight values will be reduced in power depending on variables associated with your model.
   You can do a lot of "What-Ifs" during the non-flying season with this tool.

Sincerely, Walt Brownell

     


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