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Thread OP
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Discussion
Is the RCTiger MT3506 motor too good to be true?
I'm hoping there's enough experience on these forums to settle this. I've been searching high and low for the best motor to maximize quadcopter flight time. I ran across some data from RCTiger on their MT3506 motor:
http://www.rctigermotor.com/uploadfi...0080440884.jpg These numbers are off the hook. If they are true, it means with 3s8000, and a 1.5kg AUW I could fly for over an HOUR. However, the RCgroups plot they show next to their data, doesn't even come close to the same g/W static thrust efficiency. For example, at 500 g thrust, the user data says 9.1 g/W, pretty ordinary. Their data for a 13x4.5 prop says about 16 g/W @ 500 g thrust. That's a big difference. The distributor said their values came from actual test data. I smell a fish. |
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A similar motor, 5010 from SmartDrones, with 15.7" carbon props, has actually the record for longest flight, 51 min, 4*2200mAh, computed efficiency of 14.7g/W, so could be true...
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Not sure about the data however, I have had a gut feeling for long time that large props spinning slow is the key. I have tried getting APC to make a 16" Slow Fly prop now for more than a year, was told it is on their agenda to do but it is not a high priority.
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Do you happen to know if gemfan makes a 16" or larger in both CW and CCW Slow fly?
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Thread OP
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Quote:
If the manuf. MT3506 data are true, one can get >16 g/W at 500 g thrust. Meaning a new record is possible. |
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Thread OP
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T=kt*p*d^3*w^2 where T=thrust generated by prop kt=a constant p=prop pitch d=prop diameter w=prop rpm P=kp*p*d^4*w^3 where P=power consumed by prop kp=a constant then one can solve for static thrust efficiency (g/W) by dividing T by P, which reduces to : T/P (g/W) = sqrt [(kt^3*p*d)/(kp^2*T)] This shows that as d increases, so does g/W. Also shows that as T decreases, g/W increases. (So you want to make your craft as light as possible, to require the least thrust for hover). It also shows that g/W increases at higher prop pitch, but I think this is just an artifact of the simplification of the Abbott equations. Thus, to maximize flight time, you want to have lightest craft (there are now 2 reasons for this. One is so that you require the least power, the other is that the prop is more efficient!) You also want to use the largest prop possible to generate this required thrust. |
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Thread OP
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BTW, thank you rogue277 for that information.
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I bought 5 of these, and got them a couple of days ago. I also bought some APC 15X4E props to test them with. Haven't touched them yet. Took one of the motors out to look at it. I've never had a motor that looked quite like that. Solid looking ... kind of heavy.
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