MT4114 high quality brushless drone UAV multirotor motor
drawing
test report
No. |
Prop（inch） |
Throttle（%） |
Voltages（V） |
Load Current（A） |
Power |
Thrust |
Efficiency |
Temperature |
MT4114-330KV |
CF1555TM |
50% |
22.2 |
2.8 |
62.2 |
680 |
10.94 |
42℃ |
65% |
22.2 |
5.2 |
115.4 |
1080 |
9.36 |
|||
75% |
22.2 |
7.2 |
159.8 |
1360 |
8.51 |
|||
85% |
22.2 |
10.1 |
224.2 |
1710 |
7.63 |
|||
100% |
22.2 |
13.4 |
297.5 |
2070 |
6.96 |
|||
CF1650 |
50% |
22.2 |
3.1 |
68.8 |
690 |
10.03 |
44℃ |
|
65% |
22.2 |
5.8 |
128.8 |
1100 |
8.54 |
|||
75% |
22.2 |
8.5 |
188.7 |
1390 |
7.37 |
|||
85% |
22.2 |
11.5 |
255.3 |
1730 |
6.78 |
|||
100% |
22.2 |
15.9 |
353.0 |
2140 |
6.06 |
|||
CF1855TM |
50% |
22.2 |
5.1 |
113.2 |
1050 |
9.27 |
53℃ |
|
65% |
22.2 |
10.4 |
230.9 |
1680 |
7.28 |
|||
75% |
22.2 |
14 |
310.8 |
2080 |
6.69 |
|||
85% |
22.2 |
19.1 |
424.0 |
2530 |
5.97 |
|||
100% |
22.2 |
25.4 |
563.9 |
3080 |
5.46 |
|||
MT4114-400KV |
Prop（inch） |
Throttle（%） |
Voltages（V） |
Load Current（A） |
Power |
Thrust |
Efficiency |
Temperature |
CF1650 |
50% |
18.5 |
3 |
55.5 |
500 |
9.01 |
42℃ |
|
65% |
18.5 |
5.7 |
105.5 |
860 |
8.16 |
|||
75% |
18.5 |
8.1 |
149.9 |
1110 |
7.41 |
|||
85% |
18.5 |
11.2 |
207.2 |
1460 |
7.05 |
|||
100% |
18.5 |
15.6 |
288.6 |
1830 |
6.34 |
|||
CF1555TM |
50% |
22.2 |
3.6 |
79.9 |
780 |
9.76 |
44℃ |
|
65% |
22.2 |
6.7 |
148.7 |
1200 |
8.07 |
|||
75% |
22.2 |
9.4 |
208.7 |
1540 |
7.38 |
|||
85% |
22.2 |
13.1 |
290.8 |
1950 |
6.71 |
|||
100% |
22.2 |
17.7 |
392.9 |
2410 |
6.13 |
|||
CF1650 |
50% |
22.2 |
4 |
88.8 |
710 |
8.00 |
45℃ |
|
65% |
22.2 |
7.6 |
168.7 |
1260 |
7.47 |
|||
75% |
22.2 |
11 |
244.2 |
1630 |
6.67 |
|||
85% |
22.2 |
15.1 |
335.2 |
2010 |
6.00 |
|||
100% |
22.2 |
20.9 |
464.0 |
2510 |
5.41 |
|||
Notes: The test condition oftemperature is motor surface temperature in 100% throttle while the motor run 15 s.environment temperature 26℃ | ||||||||
detail
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