Flycci Motor FX18 combined power system 33KG-36KG thrust motor ESC propeller suitable for heavy multi-rotor drones
Parameter:
Max thrust：
33KG (@14S/F40132 folding propeller)
36.1KG (@14S/F40135 folding propeller)
Recommended multi-rotor takeoff weight: 15KG-18KG/uniaxial
Applicable lithium battery：14S
Applicable ambient temperature：-20℃~65℃
Power combination total weight：
2.25KG (@F40132 folding propeller)
2.32KG (@F403135 folding propeller)
Applicable pipe diameter of motor base：Ø40mm/Ø45mm
FOC power kit include:
Motor：FY126 KV85
Structure：36N40P
Weight：1280g
Stator core size：φ110*23 mm
Dimensions：φ120.1*55 mm
Spindle diameter：IN: φ15 mm OUT:φ10 mm
Dynamic balance standard：≤15mg
ESC：FOC 14S230A
Driving mode：FOC sine wave
Support lithium battery：12S-14S
PWM throttle pulse width：1100us-1900us
PWM input frequency:50Hz-500Hz
PWM input level：3.3V/5V
Communication interface：CAN
Yellow：CANH-1，Blue：CANL-2
Size： 120*48*34 mm (L*W*H)
Working temperature：-20℃~65℃
Class of protection：IPX7
Propeller model：：F40132
Structure：Folding propeller
Length：L1016 mm /40inches
Weight：430g/piece Include Propeller base (153g/ Single propeller)
Propeller model：：F43135
Structure：Folding propeller
Lngth：L1080 mm /42.5 inches
Weight：481g/piece Include Propeller base (175g/ Single propeller)
DRAWING
TEST REPORT
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable models |
Applicable takeoff weight |
Max thrust |
Max power |
|||
|
FY126 KV85 |
FOC 14S230A |
F40132 40 inch folding propeller |
multi-rotor drone |
15KG-18KG/ uniaxial |
33KG |
6.9KW |
|||
|
Load test data |
Lithium Battery ：14S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Accelerator |
||
|
53.50 |
10187 |
21.3 |
2187 |
1139.55 |
8.94 |
4.30 |
40% |
||
|
53.50 |
12415 |
28.3 |
2399 |
1514.05 |
8.20 |
5.20 |
45% |
||
|
53.40 |
14629 |
35.8 |
2593 |
1911.72 |
7.65 |
6.20 |
50% |
||
|
53.30 |
16720 |
43.9 |
2771 |
2339.87 |
7.15 |
7.10 |
55% |
||
|
53.20 |
18652 |
52.5 |
2939 |
2793.00 |
6.68 |
8.00 |
60% |
||
|
53.10 |
20902 |
61.9 |
3091 |
3286.89 |
6.36 |
8.90 |
65% |
||
|
53.00 |
22945 |
71.9 |
3239 |
3810.70 |
6.02 |
9.90 |
70% |
||
|
52.80 |
24764 |
81.9 |
3342 |
4324.32 |
5.73 |
10.80 |
75% |
||
|
52.70 |
26769 |
93.1 |
3499 |
4906.37 |
5.46 |
11.70 |
80% |
||
|
52.50 |
29393 |
107.3 |
3613 |
5633.25 |
5.22 |
12.90 |
85% |
||
|
52.40 |
31201 |
119.2 |
3722 |
6246.08 |
5.00 |
13.80 |
90% |
||
|
52.30 |
32573 |
129.8 |
3815 |
6788.54 |
4.80 |
14.50 |
95% |
||
|
52.20 |
33003 |
132.6 |
3814 |
6921.72 |
4.77 |
14.70 |
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 |
|||
|
FY126 KV85 |
FOC 14S230A |
F43135 43 inch folding paddle |
multi-rotor drone |
15KG-18KG/ uniaxial |
36.1KG |
8.2KW |
|||
|
Load test data |
Lithium Battery ：14S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Accelerator |
||
|
53.40 |
10354 |
20.8 |
1764 |
1110.72 |
9.32 |
5.30 |
40% |
||
|
53.40 |
13076 |
28.7 |
1953 |
1532.58 |
8.53 |
6.60 |
45% |
||
|
53.30 |
15025 |
36.6 |
2131 |
1950.78 |
7.70 |
7.70 |
50% |
||
|
53.20 |
17295 |
46.1 |
2297 |
2452.52 |
7.05 |
9.00 |
55% |
||
|
53.00 |
19833 |
57.1 |
2451 |
3026.30 |
6.55 |
10.30 |
60% |
||
|
52.90 |
22149 |
67.9 |
2600 |
3591.91 |
6.17 |
11.50 |
65% |
||
|
52.70 |
24820 |
81.3 |
2738 |
4284.51 |
5.79 |
12.90 |
70% |
||
|
52.60 |
26038 |
92.1 |
2869 |
4844.46 |
5.37 |
13.70 |
75% |
||
|
52.40 |
28467 |
106.9 |
2993 |
5601.56 |
5.08 |
15.00 |
80% |
||
|
52.30 |
30908 |
122.6 |
3113 |
6411.98 |
4.82 |
16.20 |
85% |
||
|
52.00 |
33760 |
141.2 |
3224 |
7342.40 |
4.60 |
17.60 |
90% |
||
|
51.90 |
35520 |
156.1 |
3279 |
8101.59 |
4.38 |
18.20 |
95% |
||
|
51.80 |
36130 |
160.1 |
3299 |
8293.18 |
4.36 |
18.40 |
100% |
||
|
The above data comes from the sales laboratory: sea level height, E8-2024X test platform |
|||||||||