FY200-96S Brushless DC Motor for Multirotor Drones and VTOL Quadrotor
Parameter:
Model：FY200
Dimensions：Ø195.4*120 mm
Weight：8.7KG
Motor structure:36N42P
ESC：120A-HV+
Support lithium battery：48-96S
Throttle pulse width：1050us-1940us
Compatible signal frequency:50Hz-500Hz
Limiting current: ：120A
(Note: Good cooling and ventilation conditions must be ensured, and the shell temperature should be below 80°C)
PWM（Output signal voltage）：3.3V-5V （compatible）
Protection level：IPX4
Weight：1220g （Include wire）
Size：179*99.6**65.8 mm (L*S*H)
Working temperature：-20℃~65℃
Line definition:Input power cord: 10AWG Ｌ：200mm （Red is the positive pole, black is the negative pole）
Three-phase output line：10AWG Ｌ：200mm（ black）
Signal line
White line:Throttle line
Black line:ground wire
Yellow line:fault signal wire
Blue line:speed signal line
RPM（Conversion formula）：M_RPM=E_FRE*60/P
M_RPM ：Motor speed E_FRE ：Motor electrical frequency、That is the RPM signal frequency.
P : Motor magnet pairs
Red：CANH
Ｇreen：CANL
Propeller：G6298
Weight：0.75KG
Size：L1575 mm
Pitch：9.8
Propeller：G68115
Weight：0.88KG
Size：L1715 mm
Pitch：11.5
DRAWING
TEST REPORT
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated porer |
Max thrust |
Max power |
|
|
FY200 KV10 |
120A-HV+ |
G68115 |
ulti-rotor |
55KG-60KG/shaft |
11KW |
138KG |
39.6KW |
|
|
Load test data |
Lithium Battery /Voltage |
|||||||
|
96S,360V |
||||||||
|
Thrust(g） |
Current(A |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
27810 |
8 |
1386 |
2880 |
9.6563 |
19.84 |
40% |
||
|
33990 |
11 |
1560 |
3960 |
8.5833 |
24.24 |
45% |
||
|
44290 |
16 |
1751 |
5760 |
7.6892 |
31.42 |
50% |
||
|
54590 |
22 |
1931 |
7920 |
6.8927 |
39.17 |
55% |
||
|
65920 |
28 |
2119 |
10080 |
6.5397 |
45.43 |
60% |
||
|
76220 |
35 |
2255 |
12600 |
6.0492 |
53.36 |
65% |
||
|
87550 |
45 |
2420 |
16200 |
5.4043 |
63.93 |
70% |
||
|
101970 |
59 |
2530 |
21240 |
4.8008 |
80.17 |
75% |
||
|
115360 |
72 |
2750 |
25920 |
4.4506 |
90.01 |
80% |
||
|
129780 |
90 |
2915 |
32400 |
4.0056 |
106.15 |
90%Hor |
||
|
138020 |
110 |
2980 |
39600 |
3.4854 |
126.91 |
100%Hor |
||
|
Power configuration Measured data |
||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable Takeoff weight |
Rated porer |
Max thrust |
Max power |
|
|
FY200 KV12 |
120A-HV+ |
G6298 68-inch folding propeller |
multi-rotor |
55KG-60KG/shaft |
10.8KW |
128KG |
40KW |
|
|
Load test data |
Lithium Battery ,Voltage |
|||||||
|
96S,360V |
||||||||
|
Thrust(g） |
Current(A） |
RPM |
Power(W) |
Efficiency(g/W) |
Torque(N.m) |
Note |
||
|
25725 |
8.6 |
1617 |
3096 |
8.3091 |
18.28 |
40% |
||
|
33810 |
12.2 |
1838 |
4392 |
7.6981 |
22.82 |
45% |
||
|
44625 |
17.7 |
2085 |
6372 |
7.0033 |
29.19 |
50% |
||
|
54600 |
24.1 |
2299 |
8676 |
6.2932 |
36.04 |
55% |
||
|
66150 |
31.9 |
2508 |
11484 |
5.7602 |
43.73 |
60% |
||
|
74550 |
36.9 |
2640 |
13284 |
5.6120 |
48.05 |
65% |
||
|
100800 |
51.1 |
2878 |
18396 |
5.4795 |
61.04 |
70% |
||
|
102900 |
63.8 |
3055 |
22968 |
4.4801 |
71.80 |
75% |
||
|
112350 |
81.8 |
3233 |
29448 |
3.8152 |
86.99 |
80% |
||
|
121800 |
103.3 |
3415 |
37188 |
3.2753 |
104.00 |
85% |
||
|
128100 |
111.9 |
3465 |
40284 |
3.1799 |
111.03 |
90%Hor |
||