FY230 Brushless Motor for UAV VTOL Quadcopter Hexacopter Multicopter

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FY230  KV9

180A-HV+
48-96S

G7622
76 inch straight
propeller

Multi-rotor,drone

VTOL

85KG-100KG/shaft

191KG

57.8KW

Load test data

Lithium Battery : 96S

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

382.60

40459

12.2

1346

4667.72

8.67

  33.11

40%

382.50

49460

16.2

1487

6196.50

7.98

  39.79

45%

382.40

61439

21.8

1650

8336.32

7.37

  48.26

50%

382.20

76554

29.1

1818

11122.02

6.88

  58.42

55%

381.50

91187

37.8

1976

14420.70

6.32

  69.68

60%

380.90

105649

46.7

2105

17788.03

5.94

  80.70

65%

380.30

120803

57.8

2243

21981.34

5.50

  93.57

70%

379.50

137548

72.1

2382

27361.95

5.03

  109.72

75%

378.10

153461

89.1

2508

33688.71

4.56

  128.30

80%

374.50

165861

110.3

2639

41307.35

4.02

  149.47

85%

371.90

178625

134.1

2760

49871.79

3.58

  172.59

90%

364.40

182773

146.3

2806

53311.72

3.43

  181.43

  95%H⁰

364.20

191495

158.8

2893

57834.96

3.31

  190.92

100%HOT

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Rated power

Max thrust

Max Power

FY230 KV13

180A-HV+

G68115
68 inch straight
propeller

Multi-rotor,drone

VTOL

85KG/shaft

15KW

164KG

56.5KW

Load test data

Lithium Battery ,Voltage

96S ,365V

Thrust(g）

Current(A

RPM

Power(W)

Efficiency(g/W)

Torque(N.m)

Note

40110

14

1615

5110

7.849

30.217

40%

47355

18

1788

6570

7.208

35.091

45%

64292

26

2059

9490

6.775

44.016

50%

75758

35

2249

12775

5.930

54.247

55%

89376

43

2419

15695

5.695

61.962

60%

101136

52

2590

18980

5.329

69.984

65%

110880

65

2750

23725

4.674

82.390

70%

123375

78

2890

28470

4.334

94.079

75%

131250

91

3018

33215

3.952

105.104

80%

143850

114

3210

41610

3.457

123.793

85%

155400

137

3375

50005

3.108

141.496

90%

159180

146

3425

53290

2.987

148.590

95%

164115

155

3439

56575

2.901

157.107

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max thrust

Max Power

FY230 KV15

180AHV+

G6298
62 inch straight
propeller

Multi-rotor,drone

VTOL

85KG/shaft

15KW

158KG

59.5KW

Load test data

Lithium Battery ,Voltage

96S     ,365V

Thrust(g）

Current(A)

RPM

Power(W)

Efficiency(g/W)

Torque(N.m)

Note

34860

15

1896

5475

6.367

27.577

40%

47586

21

2169

7665

6.208

33.749

45%

63336

30

2439

10950

5.784

42.875

50%

76052

39

2660

14235

5.343

51.107

55%

87371

48

2814

17520

4.987

59.458

60%

98942

61

3003

22265

4.444

70.806

65%

109410

76

3185

27740

3.944

83.176

70%

120015

94

3349

34310

3.498

97.838

75%

130631

113

3557

41245

3.167

110.737

80%

137928

137

3740

50005

2.758

127.687

85%

150518

150

3798

54750

2.749

137.668

90%

156660

157

3946

57305

2.734

138.688

95%

158865

163

3872

59495

2.670

146.740

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable models

Max thrust

Max power

FY230 KV15

180A-HV+

P4613
46 inch straight
propeller

  Fixed wing aircraft

107KG

40KW

Load test data

Lithium Battery ,Voltage

96S,365V

Thrust(g）

Current(A)

RPM

Power(W)

Efficiency(g/W)

Torque(N.m)

Note

17808

9

1942

3285

5.421

16.154

40%

23320

13

2210

4745

4.915

20.504

45%

29680

18

2504

6570

4.518

25.057

50%

36040

23

2727

8395

4.293

29.399

55%

42400

27

2917

9855

4.302

32.264

60%

47700

34

3131

12410

3.844

37.852

65%

55120

40

3318

14600

3.775

42.022

70%

62540

48

3550

17520

3.570

47.131

75%

72207

57

3721

20805

3.471

53.396

80%

84079

71

4005

25915

3.244

61.795

85%

92464

82

4179

29930

3.089

68.397

90%

99767

97

4380

35405

2.818

77.196

95%

107590

112

4540

40880

2.632

85.992

100%