FY126 High Tension UAV Multi Shaft Disc Brushless Drone Dc Brushless VTOL Motor For Drone
Parameter:
Motor model:FY126
Structure type:36N40P
Seight:1280g
Dimensions:φ120.2*55 mm
Drawing

TEST REPORT
|
Power configuration Measured date |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY126 KV12 |
120A-HV+ |
P3410 34-inch straight propeller |
VTOL |
13KG-15KG/shaft |
2500W |
33.9KG |
7785W |
|
|
Load test data |
Lithium Battery,Voltage |
|||||||
|
120S,450V |
||||||||
|
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
11948 |
3.7 |
2940 |
1665 |
7.1760 |
5.4084 |
50% |
||
|
14008 |
4.5 |
3110 |
2025 |
6.9175 |
6.2182 |
55% |
||
|
15038 |
5.2 |
3280 |
2340 |
6.4265 |
6.8131 |
60% |
||
|
16995 |
6.2 |
3470 |
2790 |
6.0914 |
7.6785 |
65% |
||
|
19776 |
7.7 |
3730 |
3465 |
5.7074 |
8.8715 |
70% |
||
|
22866 |
9.2 |
3930 |
4140 |
5.5232 |
10.0603 |
75% |
||
|
24926 |
10.9 |
4140 |
4905 |
5.0818 |
11.3147 |
80% |
||
|
30385 |
14.6 |
4530 |
6570 |
4.6248 |
13.8507 |
90% |
||
|
33990 |
17.3 |
4720 |
7785 |
4.3661 |
15.7514 |
100%Hor |
||
|
65%throttle work continuously for 10 minutes,the motor temperature is 70 degrees Celsius,the ESC temperature is 75 degrees Celsius,and the ambient temperature is 25 degrees Celsius |
||||||||
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY126 KV38 |
120A-HV |
G5295 52-inch straight propeller |
|
17KG-20KG/shaft |
2700W |
43KG |
8280W |
|
|
Load test data |
Lithium Battery ,Voltage |
|||||||
|
24S,90V |
||||||||
|
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
14147 |
15 |
1537 |
1350 |
10.4796 |
8.3881 |
50% |
||
|
16922 |
19.7 |
1678 |
1773 |
9.5442 |
10.0907 |
55% |
||
|
20094 |
25.5 |
1822 |
2295 |
8.7556 |
12.0292 |
60% |
||
|
22879 |
31.2 |
1937 |
2808 |
8.1476 |
13.8443 |
65% |
||
|
25673 |
38.1 |
2055 |
3429 |
7.4871 |
15.9353 |
70% |
||
|
28662 |
45.7 |
2161 |
4113 |
6.9686 |
18.1764 |
75% |
||
|
31416 |
53.4 |
2260 |
4806 |
6.5368 |
20.3085 |
80% |
||
|
37536 |
73.6 |
2455 |
6624 |
5.6667 |
25.7675 |
90% |
||
|
43554 |
92 |
2618 |
8280 |
5.2601 |
30.2040 |
100%HoT |
||
|
65%throttle work continuously for 10 minutes,the motor temperature Is 99 degrees Celslus,the ESC temperature ts 48 degrees Celslus,and the ambilent temperature is 25 degrees Celsius. |
||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
||
|
FY126 KV85 |
150A |
F43135 43-inch folding propeller |
|
15KG-18K/shaft |
2250W |
35.1KG |
7165W |
||
|
Load test data |
Lithium Battery:14S |
||||||||
|
Voltage(V) |
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
52.69 |
7810 |
13 |
1445 |
684.97 |
11.4020 |
4.527 |
40% |
||
|
52.67 |
10120 |
18 |
1614 |
948.06 |
10.6744 |
5.610 |
45% |
||
|
52.53 |
12320 |
23 |
1780 |
1208.19 |
10.1971 |
6.482 |
50% |
||
|
52.40 |
15620 |
34 |
1976 |
1781.60 |
8.7674 |
8.610 |
55% |
||
|
52.28 |
17710 |
42 |
2117 |
2195.76 |
8.0655 |
9.905 |
60% |
||
|
52.09 |
20350 |
53 |
2260 |
2760.77 |
7.3711 |
11.666 |
65% |
||
|
51.90 |
23650 |
65 |
2426 |
3373.50 |
7.0105 |
13.280 |
70% |
||
|
51.71 |
25630 |
78 |
2510 |
4033.38 |
6.3545 |
15.346 |
75% |
||
|
51.51 |
29150 |
92 |
2637 |
4738.92 |
6.1512 |
17.162 |
80% |
||
|
51.02 |
33488 |
124 |
2914 |
632648 |
5.2933 |
20.734 |
90% |
||
|
50.46 |
35190 |
142 |
3034 |
7165.32 |
4.9112 |
22.554 |
100% |
||
|
60% throttle deactivation for 10 minutes, motor temperature 98℃, battery temperature 69℃, ambient temperature 29℃. |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
||
|
FY126 KV68 |
EP-150AH |
F43135 43-inch folding propeller |
|
16KG-18KG/shaft |
2350W |
39.6KG |
9059W |
||
|
Load test data |
Lithium Battery :18S |
||||||||
|
Voltage(V) |
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
67.56 |
8829 |
10.5 |
1536 |
709.38 |
12.4461 |
4.411 |
40% |
||
|
67.32 |
11227 |
15.8 |
1690 |
1063.66 |
10.5551 |
6.011 |
45% |
||
|
67.01 |
13843 |
22.9 |
1890 |
1534.53 |
9.0210 |
7.754 |
50% |
||
|
66.88 |
16459 |
29.1 |
2050 |
1946.21 |
8.4570 |
9.066 |
55% |
||
|
66.76 |
19293 |
37.2 |
2205 |
2483.47 |
7.7686 |
10.756 |
60% |
||
|
66.61 |
21582 |
45.1 |
2356 |
3004.11 |
7.1842 |
12.177 |
65% |
||
|
66.52 |
24525 |
56.6 |
2508 |
3765.03 |
6.5139 |
14.337 |
70% |
||
|
66.38 |
26487 |
64.8 |
2599 |
4301.42 |
6.1577 |
15.806 |
75% |
||
|
66.23 |
29103 |
76.7 |
2718 |
6079.84 |
5.7291 |
17.849 |
80% |
||
|
66.08 |
30179 |
87.8 |
2820 |
5801.82 |
5.2016 |
19.648 |
85% |
||
|
65.91 |
33063 |
104.3 |
2914 |
6874.41 |
4.8096 |
22.529 |
90% |
||
|
65.83 |
35638 |
119.5 |
3074 |
7866.69 |
4.5302 |
24.439 |
95% |
||
|
65.41 |
39655 |
138.5 |
3192 |
9059.29 |
4.3773 |
27.104 |
100% |
||
|
80% throttle for 10 minutes, motor temperature 93℃, ESC temperature 60℃, ambient temperature 29℃. |
|||||||||
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY126 KV85 |
140A |
F43135 43-inch folding propeller |
VTOL |
12KG-14KG/shaft |
1700W |
31.5KG |
5715W |
|
|
Load test data |
Lithium Battery ,Noltage |
|||||||
|
12S,45V |
||||||||
|
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
9960 |
21 |
1606 |
945 |
10.5398 |
5.6194 |
50% |
||
|
12030 |
28 |
1764 |
1260 |
9.5479 |
6.8214 |
55% |
||
|
13926 |
37 |
1910 |
1665 |
8.3637 |
8.3250 |
60% |
||
|
16562 |
46 |
2056 |
2070 |
8.0012 |
9.6150 |
65% |
||
|
18901 |
57 |
2200 |
2565 |
7.3686 |
11.1344 |
70% |
||
|
21012 |
68 |
2314 |
3060 |
6.8667 |
12.6288 |
75% |
||
|
22969 |
82 |
2458 |
3690 |
6.2247 |
14.3367 |
80% |
||
|
28325 |
110 |
2633 |
4950 |
5.7222 |
17.9539 |
90% |
||
|
31518 |
127 |
2784 |
5715 |
5.5150 |
19.6043 |
100%Hot |
||
|
Power configuration Measured date |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY126 KV40 |
120A-HV |
F43135 43-inch folding propeller |
VTOL |
15KG-18KG/shaft |
2700W |
38.7KG |
8010W |
|
|
Load test data |
Lithium Battery.Voltage |
|||||||
|
24S,90V |
||||||||
|
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
11985 |
14.1 |
1819 |
1269 |
9.4444 |
6.6624 |
50% |
||
|
14535 |
19.1 |
2010 |
1719 |
8.4555 |
8.1674 |
55% |
||
|
17646 |
25 |
2189 |
2250 |
7.8427 |
9.8161 |
60% |
||
|
20074 |
30.8 |
2336 |
2772 |
7.2416 |
11.3324 |
65% |
||
|
22746 |
37.7 |
2478 |
3393 |
6.7038 |
13.0763 |
70% |
||
|
24990 |
43.1 |
2597 |
3879 |
6.4424 |
14.2643 |
75% |
||
|
28050 |
53 |
2750 |
4770 |
5.8805 |
16.5649 |
80% |
||
|
34711 |
73 |
3050 |
6570 |
5.2832 |
20.5716 |
90% |
||
|
38780 |
89 |
3210 |
8010 |
4.8415 |
23.8304 |
100%Hor |
||
|
65%throttle work continuously for 10 minutes,the motor temperature is 88 degrees Celsius,the ESC temperature is 58 degrees Celsius,and the ambient emperature is 25 degrees Celsius. |
||||||||
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY126 KV75 |
140A |
F43135 43-inch folding propeller |
multirotor,drone VTOL |
14KG-16KG/shaft |
2500W |
33KG |
6273W |
|
|
Load test data |
Lithium Battery ,Voltage |
|||||||
|
14S,52.5V |
||||||||
|
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
11742 |
23.4 |
1768 |
1228.5 |
9.5580 |
6.6358 |
50% |
||
|
14111 |
31.1 |
1942 |
1632.75 |
8.6425 |
8.0292 |
55% |
||
|
15965 |
38.2 |
2065 |
2005.5 |
7.9606 |
9.2748 |
60% |
||
|
18746 |
47.8 |
2222 |
2509.5 |
7.4700 |
10.7857 |
65% |
||
|
20806 |
57.6 |
2346 |
3024 |
6.8803 |
12.3100 |
70% |
||
|
23381 |
68.8 |
2453 |
3612 |
6.4731 |
14.0622 |
75% |
||
|
25544 |
77.5 |
2576 |
4068.75 |
6.2781 |
15.0841 |
80% |
||
|
28850 |
102.5 |
2800 |
5381.25 |
5.3612 |
18.3539 |
90% |
||
|
33055 |
119.5 |
2992 |
6273.75 |
5.2688 |
20.0248 |
100%Ho |
||
|
65%throttle work continuously for 10 minutes,the motor temperature is 86 degrees Celsius,the ESC temperature is 74 degrees Celsius,and the ambient temperature is 25 degrees Celsius |
||||||||
|
Power confiquration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY126 KV70 |
200A |
48*17.5 48-inch folding propeller |
|
17KG - 19KG/shaft |
2850KW |
41.6KG |
7884W |
|
|
Load test date |
Lithium Battery ,Voltage |
|||||||
|
14S,54V |
||||||||
|
Thrust(g) |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
12772 |
22 |
1603 |
1188 |
10.7508 |
7.0776 |
50% |
||
|
15759 |
30 |
1806 |
1620 |
9.7278 |
8.5664 |
55% |
||
|
18952 |
40 |
1965 |
2160 |
8.7741 |
10.4977 |
60% |
||
|
22104 |
51 |
2122 |
2754 |
8.0261 |
12.3943 |
65% |
||
|
25081 |
62 |
2236 |
3348 |
7.4912 |
14.2994 |
70% |
||
|
31518 |
89 |
2465 |
4806 |
6.5581 |
18.6196 |
80% |
||
|
37286 |
126 |
2693 |
6804 |
5.4800 |
24.1286 |
90% |
||
|
41622 |
146 |
2808 |
7884 |
5.2793 |
26.8135 |
100%HoT |
||
|
65%throttle work continuously for 15 minutes,the motor temperature is 92 degrees Celsius,the ESC temperature is 59 degrees Celsius,and the ambient emperature is 25 degrees Celsius. |
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PACKAGE


