Muhtasari
MAD M50C35 PRO IPE ni motor ya drone yenye watu iliyoundwa kama suluhisho la nguvu kubwa ya propulsion kwa drones zenye watu na majukwaa ya UAV yenye uzito mzito, ikiwa na msaada wa mifumo ya voltage ya 12S na 24S.
| Upeo wa nguvu |
30~45kg |
| Upeo wa nguvu |
113.7kg |
| Msaada wa voltage |
12S,24S |
| Uzito |
4300g |
Vipengele Muhimu
- Nguvu iliyopimwa: 30–40 kgf
- Nguvu ya kilele: 92.6 kgf
- Matokeo ya kudumu: 25 kW
- Uzito wa motor: 4360g
- Inasaidia mifumo ya voltage ya 12–24S
Kwa uthibitisho wa usanidi na msaada wa kiufundi (ESC/muafaka wa prop), wasiliana na support@rcdrone.top or tembelea https://rcdrone.top/.
Maelezo ya Kiufundi
Data ya Motor
| Mfano wa Motor |
MAD M50C35 IPE V1.0 |
Idadi ya jozi za nguzo |
31 |
| Stator |
Anti-korozia |
Nyaya ya varnished |
220°C |
| Ukubwa wa Motor |
D:191 × 94 mm |
Nyaya ya Magnet |
180°C |
| Daraja la Ulinzi |
IP35 |
Urefu wa Kebuli |
150 mm (nyaya za enamel zilizopanuliwa) |
| Kuondoa Joto kwa Centrifugal |
NDIYO |
Usawa wa Rotor |
≤20 mg |
| Shimo za Kuweka Propeller |
D:50 M6×6 |
Usawa wa Motor |
≤30 mg |
| Nyota ya Shat |
ND: 25 mm |
Shimo za Kuweka Motor |
D:80 M6×6 |
| Mpira |
NSK 6818ZZCM |
Jaribio la kuvuruga |
1000 V |
Chora na Shimo za Kuweka
| Mashimo ya kufunga motor |
Ø80-M6×6 |
| Mashimo ya kufunga propeller |
Ø50-M6×6 |
| Ukipimo wa nje wa motor |
Ø191 |
| Vipimo vya upande |
83 |
| Vipimo vya hatua/kuhamasisha |
11 |
| Ukipimo wa boss/kipengele |
Ø90 |
| Shat |
Ø25, 35 |
| Kumbukumbu ya muundo wa mashimo |
Ø50-Ø6.2×6 |
9KV (Toleo la Wataalamu wa Sekta)
- Thrust inayopendekezwa ya hover: 30~40 kgf
- Thrust ya juu: 92.6 kgf
- Uzito ulioboreshwa: 4360 g
- Ufanisi: >78%
- Kichwa cha mtihani: MAD M50C35 IPE 9KV + FLUXER PRO 63x22 GLOSSY + FOC IGBT 60A (80-440V)
- Lebo: 400V, MAX 128°C
| RPM/V |
9 KV |
Voltage ya Kawaida |
Betri ya lipo 100S |
| Current bila Load |
0.92A/30V |
Upinzani wa ndani |
58.8mΩ |
| Uzito wa Motor |
4360 g |
Uzito wa Kifurushi cha Bidhaa |
5910g (330 x 265 x 135 mm) |
| Current ya Juu |
49.1 A |
Nguvu ya Juu |
19494W |
| Thrust ya Juu |
92.6 kg |
Torque ya Juu |
63.9 Nm |
| ESC Inayopendekezwa |
FOC IGBT 60A (80-440V) |
Propela Inayopendekezwa |
63x22 |
| Uzito wa UAV wakati wa kupaa |
24S-63"/ 140kg--Quadcopter 210kg--Hexacopter 280kg--Octocopter |
Uzito wa kupaa wa rotor moja |
30kg ~ 40kg |
Jedwali la Utendaji la 9KV (400V)
| Throttle [%] |
Voltage [V] |
Current [A] |
Nguvu ya Kuingiza [W] |
Nguvu ya Kutoka [W] |
Torque [N*m] |
RPM |
Thrust [kgf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
398 |
2.74 |
1090.0 |
696.7 |
7.930 |
839 |
11 |
63.92 |
10.5 |
| 35 |
398 |
3.7 |
1472.0 |
1117.6 |
10.880 |
981 |
16 |
75.93 |
10.7 |
| 40 |
398 |
5.85 |
2328.0 |
1730.3 |
14.820 |
1115 |
21 |
74.33 |
8.8 |
| 45 |
398 |
8.09 |
3219.0 |
2360.2 |
18.090 |
1246 |
26 |
73.32 |
8.0 |
| 50 |
398 |
10.23 |
4071.0 |
3107.0 |
21.690 |
1368 |
31 |
76.32 |
7.7 |
| 55 |
398 |
12.7 |
5052.0 |
3993.6 |
25.700 |
1484 |
37 |
79.05 |
7.3 |
| 60 |
398 |
15.38 |
6114.0 |
4991.2 |
29.810 |
1599 |
43 |
81.64 |
7.1 |
| 65 |
398 |
18.79 |
7471.0 |
6168.2 |
34.590 |
1703 |
48 |
82.56 |
6.5 |
| 70 |
398 |
22.56 |
8968.0 |
7369.9 |
38.950 |
1807 |
56 |
82.18 |
6.2 |
| 75 |
398 |
25.18 |
9986.0 |
8364.9 |
42.200 |
1893 |
59 |
83.77 |
5.9 |
| 80 |
397 |
29.22 |
11586.0 |
10498.4 |
49.930 |
2008 |
68 |
90.61 |
5.8 |
| 85 |
397 |
34.95 |
13861.0 |
11991.3 |
54.480 |
2102 |
75 |
86.51 |
5.4 |
| 90 |
396 |
40.04 |
15868.0 |
13572.0 |
59.130 |
2192 |
81 |
85.53 |
5.1 |
| 95 |
397 |
48.14 |
19102.0 |
15072.8 |
63.440 |
2269 |
89 |
78.91 |
4.6 |
| 100 |
397 |
49.14 |
19494.0 |
15334.1 |
63.920 |
2291 |
93 |
78.66 |
4.8 |
34KV (Toleo la Wataalamu wa Sekta)
- Mapendekezo ya nguvu ya kuzunguka: 35~45 kgf
- Nguvu ya juu: 113.7 kgf
- Uzito ulioimarishwa: 4365 g
- Ufanisi: >83%
- Kichwa cha mtihani: MAD M50C35 IPE 34KV + FLUXER PRO 63x22 GLOSSY + AMPX 300A (12-24S)
- Lebo: 24S
| RPM/V |
34 KV |
Voltage ya Kawaida |
Betri ya lipo 24S |
| Mzigo wa Sasa |
3.7A / 30V |
Upinzani wa ndani |
14.7mΩ |
| Uzito wa Motor |
4365 g |
Uzito wa Kifurushi cha Bidhaa |
5915g (330 x 265 x 135 mm) |
| Sasa ya Juu |
251.5 A |
Nguvu ya Juu |
24987W |
| Nguvu ya juu |
113.7 kg |
Torque ya Juu |
78.4 Nm |
| ESC Inayopendekezwa |
MAD AMPX 300A (12-24S) |
Propela Inayopendekezwa |
63x22 |
| Uzito wa UAV wakati wa kupaa |
24S-63"/ 160kg--Quadcopter 240kg--Hexacopter 320kg--Octocopter |
Uzito wa rotor mmoja wakati wa kupaa |
35kg ~ 45kg |
Jedwali la Utendaji la 34KV (24S)
| Throttle [%] |
Voltage [V] |
Current [A] |
Nguvu ya Kuingiza [W] |
Nguvu ya Kutoka [W] |
Torque [N*m] |
RPM |
Thrust [gf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
100.6 |
10.63 |
1069.4 |
855.5 |
8.841 |
924 |
13360 |
80.00 |
12.5 |
| 35 |
100.54 |
15.2 |
1528.2 |
1246.2 |
11.259 |
1057 |
17031 |
81.50 |
11.1 |
| 40 |
100.78 |
21.82 |
2199.0 |
1775.0 |
14.232 |
1191 |
22773 |
80.70 |
10.4 |
| 45 |
100.61 |
30.57 |
3075.6 |
2511.5 |
17.858 |
1343 |
28863 |
81.70 |
9.4 |
| 50 |
100.46 |
42 |
4219.3 |
3534.7 |
22.608 |
1493 |
35262 |
83.80 |
8.4 |
| 55 |
100.58 |
54.55 |
5486.6 |
4706.2 |
27.554 |
1631 |
42642 |
85.80 |
7.8 |
| 60 |
100.56 |
68.22 |
6860.2 |
5919.3 |
32.374 |
1746 |
49381 |
86.30 |
7.2 |
| 65 |
100.52 |
83.9 |
8433.6 |
7198.8 |
36.761 |
1870 |
56551 |
85.40 |
6.7 |
| 70 |
100.4 |
102.19 |
10259.9 |
8889.7 |
42.723 |
1987 |
63961 |
86.60 |
6.2 |
| 75 |
100.27 |
122.51 |
12284.1 |
10566.1 |
48.070 |
2099 |
72525 |
86.00 |
5.9 |
| 80 |
100.2 |
147.52 |
14781.5 |
12591.8 |
54.532 |
2205 |
80002 |
85.20 |
5.4 |
| 85 |
100.08 |
171.25 |
17138.7 |
14472.0 |
59.414 |
2326 |
87814 |
84.40 |
5.1 |
| 90 |
99.9 |
203.99 |
20378.6 |
16845.9 |
66.584 |
2416 |
96733 |
82.70 |
4.7 |
| 95 |
99.58 |
232.09 |
23111.5 |
18677.9 |
71.430 |
2497 |
106740 |
80.80 |
4.6 |
| 100 |
99.36 |
251.48 |
24987.1 |
20739.3 |
78.409 |
2526 |
113654 |
83.00 |
4.5 |
40KV (Toleo la Kitaalamu la Sekta)
- Mapendekezo ya nguvu ya kusimama: 30~40 kgf
- Nguvu ya juu: 90.9 kgf
- Uzito ulioimarishwa: 4337 g
- Ufanisi: >82%
- Kichwa cha mtihani: MAD M50C35 IPE 40KV + CB2 PROP 60x20 MATT + AMPX 300A (12-24S)
- Lebo: 24S, MAX 140°C
| RPM/V |
40 KV |
Voltage ya Kawaida |
Betri ya lipo 24S |
| Mzigo wa Sasa Bila Mzigo |
3.6A/20V |
Upinzani wa ndani |
10mΩ |
| Uzito wa Motor |
4337 g |
Uzito wa Kifurushi cha Bidhaa |
5887g (330 x 265 x 135 mm) |
| Sasa ya Juu |
216.6 A |
Nguvu ya Juu |
20967W |
| Nguvu ya juu |
90.9 kg |
Torque ya Juu |
52.1 Nm |
| ESC Inayopendekezwa |
MAD AMPX 300A (12-24S) |
Propellers Inayopendekezwa |
57x19, 60x20 |
| Uzito wa kuanzia wa UAV |
24S-60"/ 140kg--Quadcopter 210kg--Hexacopter 280kg--Octocopter |
Uzito wa kuanzia wa rotor moja |
30kg ~ 40kg |
Jedwali la Utendaji la 40KV (CB2 PROP 57x19 MATT, 24S, MAX 130°C)
| Throttle [%] |
Voltage [V] |
Current [A] |
Nguvu ya Kuingiza [W] |
Nguvu ya Kutoka [W] |
Torque [N*m] |
RPM |
Thrust [gf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
98.66 |
12.3 |
1213.5 |
910.8 |
8.091 |
1075 |
12865 |
75.10 |
10.6 |
| 35 |
98.68 |
18.03 |
1779.2 |
1361.3 |
10.569 |
1230 |
16662 |
76.50 |
9.4 |
| 40 |
98.54 |
25.34 |
2497.0 |
1991.0 |
13.688 |
1389 |
21496 |
79.70 |
8.6 |
| 45 |
98.53 |
36.78 |
3623.9 |
2921.9 |
17.637 |
1582 |
27746 |
80.60 |
7.7 |
| 50 |
98.37 |
49.01 |
4821.1 |
3998.3 |
21.830 |
1749 |
34236 |
82.90 |
7.1 |
| 55 |
98.3 |
63.68 |
6259.7 |
5276.9 |
26.482 |
1903 |
40549 |
84.30 |
6.5 |
| 60 |
98.17 |
77.5 |
7608.2 |
6398.5 |
29.851 |
2047 |
46604 |
84.10 |
6.1 |
| 65 |
98.17 |
98.03 |
9623.6 |
7949.1 |
34.791 |
2182 |
53790 |
82.60 |
5.6 |
| 70 |
98.01 |
118.31 |
11595.6 |
9438.8 |
38.938 |
2315 |
61280 |
81.40 |
5.3 |
| 75 |
97.92 |
140.81 |
13788.1 |
11195.9 |
43.606 |
2452 |
68220 |
81.20 |
4.9 |
| 80 |
97.94 |
164.23 |
16084.7 |
12996.4 |
48.407 |
2564 |
74006 |
80.80 |
4.6 |
| 85 |
97.83 |
195.21 |
19097.4 |
15201.5 |
54.069 |
2685 |
81462 |
79.60 |
4.3 |
| 90 |
98.12 |
229.66 |
22534.2 |
17847.1 |
60.871 |
2800 |
85765 |
79.20 |
3.8 |
Jedwali la Utendaji la 40KV (CB2 PROP 60x20 MATT, 24S, MAX 140°C)
| Throttle [%] |
Voltage [V] |
Current [A] |
Input Power [W] |
Output Power [W] |
Torque [N*m] |
RPM |
Thrust [gf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
98.47 |
12.4 |
1221.0 |
895.0 |
7.117 |
1201 |
14430 |
73.30 |
11.8 |
| 35 |
98.46 |
19.2 |
1890.4 |
1414.0 |
10.040 |
1345 |
18964 |
74.80 |
10.0 |
| 40 |
98.33 |
26.8 |
2635.2 |
1976.4 |
12.592 |
1499 |
22645 |
75.00 |
8.6 |
| 45 |
98.33 |
35.8 |
3520.2 |
2678.9 |
15.571 |
1643 |
27640 |
76.10 |
7.9 |
| 50 |
98.43 |
47.4 |
4665.6 |
3601.8 |
19.270 |
1785 |
33945 |
77.20 |
7.3 |
| 55 |
98.35 |
59.8 |
5881.3 |
4593.3 |
23.075 |
1901 |
39362 |
78.10 |
6.7 |
| 60 |
98.26 |
73.1 |
7182.8 |
5753.4 |
31.419 |
2024 |
45693 |
80.10 |
6.4 |
| 65 |
98.43 |
86.5 |
8514.2 |
6777.3 |
32.284 |
2123 |
51637 |
79.60 |
6.1 |
| 70 |
98.42 |
100.8 |
9920.7 |
7847.3 |
33.471 |
2239 |
56700 |
79.10 |
5.7 |
| 75 |
98.49 |
118.4 |
11661.2 |
9200.7 |
37.012 |
2374 |
62129 |
78.90 |
5.3 |
| 80 |
98.47 |
131 |
12899.6 |
10100.4 |
39.211 |
2460 |
67134 |
78.30 |
5.2 |
| 85 |
98.37 |
148.6 |
14617.8 |
11416.5 |
42.112 |
2589 |
72374 |
78.10 |
5.0 |
| 90 |
96.56 |
169.7 |
16386.2 |
12699.3 |
44.935 |
2699 |
78315 |
77.50 |
4.8 |
| 95 |
97.35 |
193 |
18788.6 |
14523.5 |
48.976 |
2832 |
86016 |
77.30 |
4.6 |
| 100 |
96.8 |
216.6 |
20966.9 |
16102.6 |
52.129 |
2950 |
90890 |
76.80 |
4.3 |
Mipangilio Inayopendekezwa
- 34KV ESC Inayopendekezwa: AMPX 300A (12-24S); propeller: CB2 prop 63X22" inchi propeller ya nyuzi za kaboni.
- 40KV ESC Inayopendekezwa: AMPX 300A (12-24S); propeller: CB2 57X19. Mbadala: AMPX 200A (12-24S) na propeller: fluxer pro 60X20.
- 59KV FOC combo Inayopendekezwa: HB40-63X22 seti ya mikono ya drone; HB40-64x20 seti ya mikono ya drone; HB40-60X19 seti ya mikono ya drone; HB40-57X19 seti ya mikono ya drone.
Kilichojumuishwa
- Motor x1
- Propeller Plate x1
- Pin ya Kuweka x1
- 8.0mm Bullet Connector x3
- Tube inayoweza kupungua kwa joto x3
- M6*25 Visu vya Motor x6
- M6*45 Visu vya Prop Adapter x6
- M6*60 Visu vya Propeller x6
- Sticker x2
Maombi
- Mifumo ya propulsion ya drone yenye watu ndani
- ndege za eVTOL, UAV za mizigo, na majukwaa ya paramotor ya umeme
- Miradi inayohitaji mchanganyiko wa ESC + prop uliothibitishwa kwa usanidi wa nguvu kubwa
Maelezo

MAD M50C35 PRO IPE michoro ya motor inaonyesha vipimo vya jumla na mpangilio wa mashimo ya kufunga kusaidia kupanga ufungaji na usakinishaji.

Pakiti ya motor ya MAD M50C35 PRO IPE inajumuisha sahani ya propeller, pini ya kuweka, 8.0mm bullet connectors, tubing inayoweza kupungua kwa joto, visu za kufunga, na stickers za ufungaji.

Data za utendaji wa motor ya MAD M50C35 zinajumuisha kiwango cha 9kW katika 400V, pamoja na takwimu za nguvu na ufanisi na jedwali la maelezo ya kina.

Karatasi ya spesifikas za motor ya MAD M50C35 ina orodha ya mpangilio wa 24S pamoja na data za ufanisi na nguvu, ikiwa ni pamoja na hadi 113.7 kgf nguvu ya juu.

Karatasi ya spesifikas za motor ya drone ya M50C35 40KV ina orodha ya takwimu muhimu kama vile anuwai ya 30–40 kgf, uzito wa 433.7 g, na hadi 82% ufanisi pamoja na mikondo ya utendaji na meza.