High-efficiency integrated FOC multi-rotor UAV 64-68KG power system combination suitable for Heavy-Duty UAV FX30-96S
Parameter:
Max thrust：64.8KG (@96S/F5620 folding propeller)
Recommended multi-rotor takeoff weight: 25KG-30KG/uniaxial
Applicable lithium battery：96S
Applicable ambient temperature：-20℃~65℃
Power combination total weight：2800g
Applicable pipe diameter of motor base：Ø50mm
FOC power kit include:
Motor：FY140 KV9
Structure：36N42P
Weight：2180 g
Stator core size：φ138*30 mm
Dimensions：φ147.6*60.4 mm
Spindle diameter：IN: φ15 mm OUT:φ10 mm
Dynamic balance standard：≤15mg
ESC：FOC 96S40A
Driving mode：FOC sine wave
Support lithium battery：48S-100S
PWM throttle pulse width：1100us-1900us
PWM input frequency:50Hz-500Hz
PWM input level：3.3V/5V
Communication interface：CAN*2 (CAN2.0B, 1M bps)
Black：GND，Yellow：CANH-1，Green：CANL-1，Red：CANH-2，Blue：CANL-2
Size： 117*67*37 mm (L*W*H)
Weight：395 g
Working temperature：-20℃~65℃
Class of protection：IPX7
Propeller model：：F5620
Structure：Folding propeller
Length：1425 mm/ 56inches
Pitch：20
Weight：862g/piece Include Propeller base
DRAWING
TEST REPORT
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable models |
Applicable takeoff weight |
Max thrust |
Max power |
|||
|
FY140 KV9 |
FOC 96S40A |
F5620 56 inch folding propeller |
Multi-rotor drone |
25KG-30KG/ uniaxial |
64.8KG |
12.7KW |
|||
|
Load test data |
Lithium Battery ：96S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Accelerator |
||
|
368.00 |
13378 |
3.1 |
1191 |
1140.80 |
11.73 |
9.15 |
40% |
||
|
368.00 |
16706 |
4.2 |
1328 |
1545.60 |
10.81 |
11.11 |
45% |
||
|
368.00 |
20282 |
5.7 |
1462 |
2097.60 |
9.67 |
13.70 |
50% |
||
|
367.90 |
23698 |
7.2 |
1597 |
2648.88 |
8.95 |
15.84 |
55% |
||
|
367.90 |
27877 |
9.2 |
1724 |
3384.68 |
8.24 |
18.75 |
60% |
||
|
367.90 |
31634 |
11.3 |
1851 |
4157.27 |
7.61 |
21.45 |
65% |
||
|
367.80 |
37039 |
14 |
1974 |
5149.20 |
7.19 |
24.91 |
70% |
||
|
367.70 |
39955 |
16.3 |
2096 |
5993.51 |
6.67 |
27.31 |
75% |
||
|
367.40 |
45981 |
19.7 |
2212 |
7237.78 |
6.35 |
31.25 |
80% |
||
|
367.20 |
50071 |
22.9 |
2329 |
8408.88 |
5.95 |
34.47 |
85% |
||
|
366.90 |
55267 |
26.7 |
2443 |
9796.23 |
5.64 |
38.29 |
90% |
||
|
366.60 |
59936 |
30.8 |
2552 |
11291.28 |
5.31 |
42.26 |
95% |
||
|
366.40 |
64843 |
34.9 |
2661 |
12787.36 |
5.07 |
45.89 |
100% |
||
|
The above data comes from the sales laboratory: sea level height, E8-2024X test platform |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable models |
Applicable takeoff weight |
Max thrust |
Max power |
|||
|
FY140 KV9 |
FOC 96S40A |
G6298 62 inch straight paddle |
Multi-rotor drone |
25KG-30KG/ uniaxial |
67.4KG |
13.1KW |
|||
|
Load test data |
Lithium Battery ：96S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Accelerator |
||
|
368.00 |
13777 |
3.2 |
1202 |
1177.60 |
11.70 |
9.35 |
40% |
||
|
368.00 |
17314 |
4.4 |
1339 |
1619.20 |
10.69 |
11.54 |
45% |
||
|
368.00 |
20800 |
5.9 |
1477 |
2171.20 |
9.58 |
14.04 |
50% |
||
|
367.90 |
24472 |
7.6 |
1610 |
2796.04 |
8.75 |
16.59 |
55% |
||
|
367.90 |
29611 |
9.7 |
1739 |
3568.63 |
8.30 |
19.60 |
60% |
||
|
367.90 |
33645 |
12 |
1865 |
4414.80 |
7.62 |
22.60 |
65% |
||
|
367.80 |
38870 |
14.7 |
1991 |
5406.66 |
7.19 |
25.93 |
70% |
||
|
367.60 |
43617 |
17.9 |
2113 |
6580.04 |
6.63 |
29.75 |
75% |
||
|
367.30 |
48507 |
21.4 |
2231 |
7860.22 |
6.17 |
33.65 |
80% |
||
|
366.90 |
53614 |
25.2 |
2351 |
9245.88 |
5.80 |
37.56 |
85% |
||
|
366.60 |
59573 |
29.7 |
2462 |
10888.02 |
5.47 |
42.23 |
90% |
||
|
366.30 |
67498 |
35.5 |
2571 |
13003.65 |
5.19 |
48.30 |
95% |
||
|
366.30 |
67450 |
35.9 |
2585 |
13150.17 |
5.13 |
48.59 |
100% |
||
|
The above data comes from the sales laboratory: sea level height, E8-2024X test platform |
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