FY180-96S Brushless Motor UAV for large scale multi rotorelectric paraglider,large agricultural VTOL
Parameter:
Applicable lithium battery：FY180-96S (Suitable for multi-rotor drone power)
Model：FY180 KV11 KV9
Weight：4.5KG
Dimensions：Ø150*108 mm
Internal resistance:197mῼ
ECS：100A-HV+
Weight：1.445KG
Dimensions：160*68*78 mm
Propeller:
Model: G5295
Structure: One-piece carbon fiber propeller (bright)
Length: 1320 mm 52 inches
Thread pitch: 9.5 inches
Weight: 519 g
Model: G6298
Structure: One-piece carbon fiber propeller (bright)
Length: 1575 mm 62 inches
Thread pitch: 9.8 inches
Weight: 769 g
DRAWING
TEST REPORT
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY180 KV9 |
100A-HV+V2 |
G6298 |
VTOL UAV / |
35KG-40KG/shaft |
5900W |
86.1KG |
16.4KW |
|
|
Load test data |
Lithium Battery ,Voltage |
|||||||
|
96S 360V |
||||||||
|
Thrust(g） |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
15330 |
3.9 |
1282 |
1404 |
10.92 |
10.4588 |
40% |
||
|
19950 |
5.2 |
1415 |
1872 |
10.66 |
12.6343 |
45% |
||
|
25200 |
7.4 |
1579 |
2664 |
9.46 |
16.1122 |
50% |
||
|
30450 |
9.7 |
1726 |
3492 |
8.72 |
19.3213 |
55% |
||
|
35700 |
12.3 |
1867 |
4428 |
8.06 |
22.6499 |
60% |
||
|
42000 |
15.4 |
2006 |
5544 |
7.58 |
26.3934 |
65% |
||
|
46200 |
18.3 |
2124 |
6588 |
7.01 |
29.6212 |
70% |
||
|
53550 |
22.3 |
2256 |
8028 |
6.67 |
33.9838 |
75% |
||
|
60900 |
26.7 |
2357 |
9612 |
6.34 |
38.9455 |
80% |
||
|
73500 |
36.3 |
2600 |
13068 |
5.62 |
47.9998 |
90% |
||
|
86100 |
45.8 |
2750 |
16488 |
5.22 |
57.2583 |
100% |
||
|
65% throttle continuous operation for 10 minutes, motor temperature 98℃, ESC temperature 48℃, ambient temperature 25℃. |
||||||||
|
The above mentioned information comes from the experiment: high sea level, 5-2022 test platform. |
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|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY180 KV13 |
100A-HV+V2 |
G5295 |
VTOL UAV / |
38KG-45KG/shaft |
7000W |
94KG |
26.6KW |
|
|
Load test data |
Lithium Battery ,Voltage |
|||||||
|
96S 360V |
||||||||
|
Thrust(g） |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
18444 |
5 |
1756 |
1800 |
10.25 |
9.79 |
40% |
||
|
23638 |
7 |
1951 |
2520 |
9.38 |
12.34 |
45% |
||
|
25864 |
10 |
2154 |
3600 |
7.18 |
15.96 |
50% |
||
|
36146 |
14 |
2391 |
5040 |
7.17 |
20.13 |
55% |
||
|
42930 |
18 |
2611 |
6480 |
6.63 |
23.70 |
60% |
||
|
51092 |
23 |
2827 |
8280 |
6.17 |
27.97 |
65% |
||
|
59042 |
28 |
3006 |
10080 |
5.86 |
32.02 |
70% |
||
|
63706 |
34 |
3178 |
12240 |
5.20 |
36.78 |
75% |
||
|
72398 |
41 |
3373 |
14760 |
4.91 |
41.79 |
80% |
||
|
80348 |
50 |
3540 |
18000 |
4.46 |
48.56 |
85% |
||
|
86178 |
62 |
3758 |
22320 |
3.86 |
56.72 |
90% |
||
|
90206 |
71 |
3876 |
25560 |
3.53 |
62.98 |
95% |
||
|
94552 |
74 |
3995 |
26640 |
355 |
63.68 |
100% |
||
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY180 KV13 |
100A-HV+V2 |
P4614 |
VTOL,UAV, |
33KG-40KG/shaft |
7800W |
94KG |
27.9KW |
|
|
Load test data |
Lithium Battery,Voltage |
|||||||
|
96S 360V |
||||||||
|
Thrust(g） |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
14628 |
4.8 |
1743 |
1728 |
8.47 |
9.47 |
40% |
||
|
18974 |
6.5 |
1937 |
2340 |
8.11 |
11.54 |
45% |
||
|
22684 |
9.2 |
2179 |
3312 |
6.85 |
14.52 |
50% |
||
|
28196 |
12.6 |
2417 |
4536 |
6.22 |
17.92 |
55% |
||
|
33178 |
16.5 |
2630 |
5940 |
5.59 |
21.57 |
60% |
||
|
38796 |
20.8 |
2822 |
7488 |
5.18 |
25.34 |
65% |
||
|
44096 |
25.4 |
2998 |
9144 |
4.82 |
29.13 |
70% |
||
|
51304 |
31.3 |
3209 |
11268 |
4.55 |
33.53 |
75% |
||
|
58618 |
38.1 |
3408 |
13716 |
4.27 |
38.44 |
80% |
||
|
66462 |
45.7 |
3590 |
16452 |
4.04 |
43.77 |
85% |
||
|
75472 |
54.3 |
3780 |
19548 |
3.86 |
49.39 |
90% |
||
|
84058 |
64.5 |
3966 |
23220 |
3.62 |
55.91 |
95% |
||
|
94870 |
77.7 |
4218 |
27972 |
3.39 |
63.33 |
100% |
||
|
70% throttle continuous operation for 10 minutes, motor temperature 105℃, ESC temperature 58℃, ambient temperature 30℃. |
||||||||
|
The above data comes from the laboratory: sea level height, E5-2022 agent testing platform. |
||||||||
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated power |
Max thrust |
Max power |
|
|
FY180 KV11 |
100A-HV+V2 |
G5295 |
VTOL UAV ,Multirotor drone |
35KG-40KG/shaft |
6200W |
84KG |
19.6KW |
|
|
Load test data |
Lithium Battery ,Voltage |
|||||||
|
96S 360V |
||||||||
|
Thrust(g） |
Current(A) |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
17850 |
5.3 |
1685 |
1908 |
9.355 |
10.8139 |
40% |
||
|
21000 |
6.7 |
1832 |
2412 |
8.706 |
12.5735 |
45% |
||
|
25200 |
9.2 |
2025 |
3312 |
7.609 |
15.6196 |
50% |
||
|
30450 |
11.6 |
2203 |
4176 |
7.292 |
18.1030 |
55% |
||
|
35700 |
14.5 |
2369 |
5220 |
6.839 |
21.0431 |
60% |
||
|
40950 |
17.2 |
2532 |
6192 |
6.613 |
23.3545 |
65% |
||
|
47250 |
21.2 |
2711 |
7632 |
6.19 |
26.8851 |
70% |
||
|
54600 |
26.3 |
2886 |
9468 |
5.767 |
31.3304 |
75% |
||
|
61950 |
31.1 |
3045 |
11196 |
5.533 |
35.1139 |
80% |
||
|
73500 |
41.3 |
3300 |
14868 |
4.944 |
43.0271 |
90% |
||
|
84000 |
54.6 |
3550 |
19656 |
4.274 |
52.8774 |
100% |
||
|
The above mentioned information comes from the experiment: high sea level, 5-2022 test platform |
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