FY85-8314 brushless dc drone motor for UAV surveying mapping VTOL large load high efficiency

Power configuration Measured data

Motor

ESC

propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY85 KV90

80A

6S-14S)

F3080

30 inch folding

propeller

multi-rotor

drone

5.0KG-6.2KG

uniaxia

(Single axis)

11.7KG

2476W

load test data

Lithium Battery :12S      44.4V

Voltage(V)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

44.12

2708

4.42

1464

195.01

13.89

1.27

40%

44.11

3323

6.13

1625

270.39

12.29

1.59

45%

44.11

4086

8.39

1801

370.08

11.04

1.96

50%

44.05

4836

10.97

1963

483.23

10.01

2.35

55%

44.04

5594

13.8

2116

608.19

9.20

2.74

60%

44.02

6214

16.72

2254

736.01

8.44

3.12

65%

43.96

7016

20.19

2387

887.55

7.90

3.55

70%

43.92

7760

24.02

2522

1054.96

7.36

3.99

75%

43.87

8367

27.82

2638

1220.46

6.86

4.42

80%

43.82

9374

32.91

2754

1442.12

6.50

5.00

85%

43.77

9960

37.66

2873

1648.38

6.04

5.48

90%

43.68

10638

42.97

2967

1876.93

5.67

6.04

95%

43.63

11033

48.01

3046

2094.68

5.27

6.57

100%

load test data                                                                  Lithium Battery :12S         48V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

47.74

3040

5.13

1554

244.91

12.41

1.51

40%

47.74

3780

7.07

1732

337.52

11.20

1.86

45%

47.71

4561

9.48

1905

452.29

10.08

2.27

50%

47.67

5361

12.47

2083

594.44

9.02

2.73

55%

47.62

6142

15.29

2241

728.11

8.44

3.10

60%

47.59

6919

18.84

2380

896.60

7.72

3.60

65%

47.56

7779

22.57

2522

1073.43

7.25

4.06

70%

47.49

8583

26.15

2645

1241.86

6.91

4.48

75%

47.44

9454

31.39

2757

1489.14

6.35

5.16

80%

47.37

10065

36.66

2873

173658

5.80

5.77

85%

47.32

10737

41.72

2988

1974.19

5.44

6.31

90%

47.25

11193

47.12

3067

2226.42

5.03

6.93

95%

47.16

11784

52.52

3148

2476.84

4.76

7.51

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY85 KV90

80A

6S-14S)

F32120

32 inch folding

propeller

multi-rotor

drone

4.5KG-6.0KG

uniaxia

(Single axis)

11.9KG

2160W

load test data

Lithium Battery:12S 44.4V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

44.16

2414

3.63

1488

160.30

15.06

1.03

40%

44.12

3056

4.96

1661

218.84

13.96

1.26

45%

44.12

3640

6.65

1858

293.40

12.41

1.51

50%

44.09

4438

8.89

2031

391.96

11.32

1.84

55%

44.06

5098

10.96

2196

482.90

10.56

2.10

60%

44.02

5842

13.53

2342

595.59

9.81

2.43

65%

44.02

6646

16.51

2491

726.77

9.14

2.79

70%

43.98

7236

19.13

2621

841.34

8.60

3.07

75%

43.89

8052

22.63

2775

993.23

8.11

3.42

80%

43.86

9250

27.37

2898

1200.45

7.71

3.96

85%

43.85

10011

31.16

3033

1366.37

7.33

4.30

90%

43.77

10738

35.79

3155

1566.53

6.85

4.74

95%

43.73

11457

40.39

3258

1766.25

6.49

5.18

100%

load test data

Lithium Battery :12S        48V

Voltage(V)

Pulling

Force(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

   47.76

2653

4.03

1585

192.47

13.78

1.16

40%

   47.74

3418

5.62

1787

268.30

12.74

1.43

45%

   47.72

4095

7.53

1988

359.33

11.40

1.73

50%

   47.67

5006

9.87

2169

470.50

10.64

2.07

55%

   47.65

5894

12.54

2337

597.53

9.86

2.44

60%

   47.63

6649

15.39

2493

733.03

9.07

2.81

65%

   47.58

7428

18.11

2615

861.67

8.62

3.15

70%

   47.55

8329

22.17

2769

1054.18

7.90

3.64

75%

   47.49

8776

260

2929

1235.21

7.10

4.03

80%

   47.46

9992

30.56

3064

1450.38

6.89

4.52

85%

   47.38

10780

35.27

3185

1671.09

6.45

5.01

90%

   47.31

11686

40.48

3297

1915.11

6.10

5.55

95%

   47.26

11951

45.71

3410

2160.25

5.53

6.05

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY85 KV110

80A

(6S-14S)

F2880

28 inch folding

propeller

multi-rotor

   drone

4.0KG-5.5KG

uniaxia

(Single axis)

11.4KG

3221W

load test data

Lithium Battery :12S   44.4V

Voltage(V)

Pulling

Force(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

44.14

2031

6.02

1824

265.72

7.64

1.39

40%

44.11

2791

8.83

2046

389.49

7.17

1.82

45%

44.08

3449

11.72

2251

516.62

6.68

2.19

50%

44.02

4201

15.12

2446

665.58

6.31

2.60

55%

44.02

4816

18.42

2608

810.85

5.94

2.97

60%

43.95

5470

22.4

2777

984.48

5.56

3.39

65%

43.88

6147

26.54

2941

1164.58

5.28

3.78

70%

43.85

6888

32.26

3099

1414.60

4.87

4.36

75%

43.77

7845

37.86

3226

1657.13

4.73

4.91

80%

43.73

8667

43.56

3379

1904.88

4.55

5.38

85%

43.62

9256

49.73

3530

2169.22

4.27

5.87

90%

43.55

9894

56.13

3638

2444.46

4.05

6.42

95%

43.47

10530

62.36

3752

2710.79

3.88

6.90

100%

load test data

Lithium Battery:12S         48V

Voltage(V)

Pulling

Force(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

   47.75

2504

7.19

1953

343.32

7.29

1.68

40%

   47.68

3153

9.94

2190

473.94

6.65

2.07

45%

   47.68

3947

13.35

2399

636.53

6.20

2.53

50%

   47.63

4853

17.15

2605

816.85

5.94

2.99

55%

   47.57

5383

20.35

2759

968.05

5.56

3.35

60%

   47.53

6185

25.08

2929

1192.05

5.19

3.89

65%

   47.47

7262

30.54

3086

1449.73

5.01

4.49

70%

   47.41

7329

35.08

3258

1663.14

4.41

4.88

75%

   47.34

8416

40.89

3421

1935.73

4.35

5.40

80%

   47.26

9210

47.05

3568

2223.58

4.14

5.95

85%

   47.18

9975

53.98

3692

2546.78

3.92

6.59

90%

   47.07

10770

60.59

3785

2851.97

3.78

7.20

95%

   47.02

11489

68.51

3863

3221.34

3.57

7.96

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY85 KV110

80A

(6S-14S)

P3095

30 inch straight

propeller

multi-rotor

drone

5.0KG-6.5KG

uniaxia

(Single axis)

13.8KG

2851W

load test data

Lithium Battery :12S 44.4V

Voltage(V)

Pulling

Force(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

44.15

2978

5.22

1878

230.46

12.92

1.17

40%

44.12

3734

7.34

2128

323.84

11.53

1.45

45%

44.09

4678

9.97

2339

439.58

10.64

1.79

50%

44.05

5416

12.75

2541

561.64

9.64

2.11

55%

44.05

5996

15.05

2702

662.95

9.04

2.34

60%

43.97

6792

18.36

2901

807.29

8.41

2.66

65%

43.96

7673

22.34

3086

982.07

7.81

3.04

70%

43.91

8764

26.98

3236

1184.69

7.40

3.50

75%

43.86

9520

31.41

3394

1377.64

6.91

3.88

80%

43.77

10367

37.37

3560

1635.68

6.34

4.39

85%

43.72

11292

43.17

3719

1887.39

5.98

4.85

90%

43.64

12232

49.25

3848

2149.27

5.69

5.33

95%

43.56

12995

55.69

3965

2425.86

5.36

5.84

100%

load test data

Lithium Battery :12S        48V

Voltage(V)

Pulling

Force(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W

Torque

(N.m)

accelerator

47.76

3406

5.91

2014

282.26

12.07

   1.34

40%

47.73

4394

8.52

2270

406.66

10.81

   1.71

45%

47.69

5321

11.27

2491

537.47

9.90

   2.06

50%

47.65

6027

13.68

2671

651.85

9.25

   2.33

55%

47.63

6930

17.2

2876

819.24

8.46

   2.72

60%

47.59

7900

21.04

3070

1001.29

7.89

   3.11

65%

47.54

8876

25.04

3251

1190.40

7.46

   3.50

70%

47.47

9752

30.05

3433

1426.47

6.84

   3.97

75%

47.44

10500

34.89

3611

1655.18

6.34

   4.38

80%

47.35

11361

40.84

3771

1933.77

5.88

   4.90

85%

47.27

12195

46.81

3929

2212.71

5.51

   5.38

90%

47.21

12826

52.83

4068

2494.10

5.14

   5.86

95%

4,711

13869

60.53

4181

2851.57

4.86

   6.51

100%