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United States, TX, Grand Prairie
Joined Nov 2005
4,988 Posts
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Quote:
The sound is wicket, I don't blame folk for beating on 16usd rotors... Hey Pete, so the packs you ran the motor on were > 40c? Did you test with a thrust tube? Regards |
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United States, TX, Grand Prairie
Joined Nov 2005
4,988 Posts
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Nope, only ran two minutes though, I didn't have the motor heat sunk correctly and it demagged ....yeah, no burnt windings just demagged cause it got freakin hot.
I ran this combo at a lower cell count yesterday...thing sounds like a really small turbin at that power level in the air very similar whistle and whine ....I know a cam would never capture what these things sound like in person |
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Australia, VIC, Melbourne
Joined Nov 2006
6,243 Posts
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There is nothing 'wrong' with anyone wanting to run one on 6S. Cell count is not about power, that is about efficient power.... OR, also power if you wanted that.
The motor KV is the key point in a Cell count choice. If you only want 1.4Kg, you can get that from 4S, 5S, 6S.... and the 6S way will be more efficient. The less Amps you can run for any given power level the better. More cells means you can run less Amps. If you want 1.7Kg, you are pretty well locked in for 5S or 6S. And if you want 1.9Kg or more... 6S. Though you might even be able to fry up some motor pushing a 4S combo to 2.0kg too.... hehe You would have fun finding a motor of the right KV for 1.4Kg on 6S though! LOL. It would need about 1700kv to 1800kv... which they do exist, but hard to get. (tho Leopard do make plenty of suitable ones right through that area too. 2850 series, or 2860 series). I consider up to about 2.0Kg is totally fine for the stock rotor and housing. They are not showing an inkling of issue to that level. Just balance them up well... like you should to any fan anyway. I have no interest in power over that level... well, maybe to 2.1Kg area approx. - on the bench, which will be less once in-plane use anyway. |
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Australia, VIC, Melbourne
Joined Nov 2006
6,243 Posts
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Not '40C'.... but 174 Amps capable. (5800mAH 30C)
C is not that useful a rating, mentioned on its own. I would prefer to see a number quoted as "Capable Amps", which then makes the actual battery capacity and C rating irrelevant. In these tests all you really want to know is what did the motor WANT to draw, and that the tester had more than that capacity available, because if you know that then you can work out what issues you will have when you use it in any other battery combo. eg A combo tested 'properly' used 70 Amps, running from "200Amps capable", giving 2.0Kg thrust, so that means the motor was unimpeded in attaining the best it could do (whether that means it was run way over specs or not is not important here). Any other person that runs that test, with adequate Amps available, will get the exact same result (within a tolerance range). Because that is what that motor's physical construction, and KV rating, will drive a CS10 in every case that it is given adequate source current (Amps). And a person with a certain aircraft, and certain batteries they already own, might see they don't even want 2.0Kg... so their first best choice is not to use that motor combo at all. They really need less KV to lower the RPM and thus thrust. They can also do the maths on their battery... hmm, it is "90Amps capable", due to its small size and C rating, and thus they will know that the motor WANTS 70A and it is pretty assured their battery will never truly give that out (the stated battery ratings they put on them are dream numbers! LOL), so if they still chose to use that combo it would suffer from voltage sag, and it would run weaker than that 70A test case.... maybe even fluking the lower thrust they wanted to have, but it would be damaging their battery in that process. The only reason it runs lower output, lower RPM, is because the motor load dragged the battery down which means bad for it. If someone tests a motor on inadequate current capability, then those figures are not a lot of use to anyone (almost). Because it is not what it can truly do. Just what it did on their inadequate battery, which would have sagged X amount, been bad for it, and just under-quoted that combos true ability. Even more useful is to do TWO tests.... one with more than enough current capability, to show the true maximum. And then using a typical battery people would probably want to use in such an application - that is because in the majority of these cases people ARE using batteries not truly up to the job of what they are driving. Because to have the truly adequate battery is too heavy for any aircraft the combo is used in. (when we are talking in these high end number regions - not an issue for lower output combos) But you need the 'capable current supply' test to show what the true MAXIMUM need would be. Then you can say "Well I am getting 60A, and X sag, and the battery is X temp... and I know it would run to 70A in an adequate system, so my battery is 'this' far off that ability. Using higher C, or larger capacity, to have 10A more capability would be more correct so as not to damage the battery.". There are a few other factors that come into play in it all (ESC, wiring), but not really important, beyond that outline above. |
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United States, TX, Grand Prairie
Joined Nov 2005
4,988 Posts
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That's like testing the motor with a 3300 55c
Sounds like we should stay below 40c on 3300mah and under packs on the HK motors... The motor is already being taxed so it's no wonder going 50 - 60c gets the windings burning. |
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