Muhtasari
Motor ya MAD X4125 ni ndege drone ya eVTOL inayotolewa katika toleo mbili: 250KV (12S) na 540KV (6S). Imepangwa kwa nguvu ya kudumu ya 2~3 kg na nguvu ya juu hadi 7.1 kgf (inategemea toleo), ikiwa na ulinzi wa IP35 na seti ya vifaa vya kufunga vilivyotolewa.
Vipengele Muhimu
- Mfano wa motor: MAD X4125 IPE V1.0
- Daraja la ulinzi IP35
- Kuondoa joto kwa njia ya katikati: NDIYO
- Stator: Karatasi za chuma za silicon za ubora wa juu / Inakabiliwa na mipako ya fluorine kwa 180C
- Daraja la waya wa varnished: 180C; daraja la sumaku: 150C
- Support voltage variants: 250KV/12S; 540KV/6S
Maelezo
Motor (Kawaida)
| Mfano wa Motor |
MAD X4125 IPE V1.0 |
| Idadi ya jozi za nguzo |
7 |
| Ukubwa wa motor |
D:50 x 74 mm |
| Ngazi ya ulinzi |
IP35 |
| Urefu wa kebo |
Waya ya enamel 100 mm |
| Kuondoa joto kwa nguvu ya katikati |
NDIYO |
| Usawa wa rotor |
≤ 5 mg |
| Usawa wa motor |
≤ 10 mg |
| Shimo za kufunga propela |
D:20 M3 x 4 / M8 nut |
| Shimo za kufunga motor |
D:30 M4 x 4 / D:56 M4 x 4 / D:60 M4 x 4 |
| Vipimo vya shat |
ND: 6 mm |
| Mpira wa kuzaa |
MR126 ZZ x 2 / 696ZZ x 1 |
| Jaribio la kuvuruga |
500 V |
| Stator | Karatasi za chuma za silicon za ubora wa juu / Zinaweza kuhimili mipako ya fluorine kwa 180C |
| Daraja la varnished wire |
180C |
| Daraja la sumaku |
150C |
Drawing ya Kifaa (Vipimo vya Ziada)
| Urefu wa jumla |
74 mm |
| Urefu wa mwili |
50 mm |
| Njia ya mzunguko wa motor |
850 |
| Mpangilio wa nyuma |
830 - M4 x 4 |
| Mpangilio wa mbele wa prop |
820 - M3 x 4 |
| Plate ya prop (OD / shimo la kati / unene) |
870 / 815 / 4 mm |
| Adapter ya prop (urefu wa jumla) |
35 mm |
| Adapter ya prop (urefu wa hatua) |
28 mm, 18 mm |
| Adapter ya prop (kipenyo cha nje) | 828 |
Muhtasari wa Utendaji
| Tofauti |
Nguvu iliyodumu |
Max nguvu |
Voltage ya msaada |
Uzito wa motor |
| 250KV |
2~3 kg |
7.1 kgf |
12S |
345 g |
| 540KV |
2~3 kg |
6.7 kgf |
6S |
347 g |
250KV (12S) Karatasi ya Takwimu
| RPM/V |
250 KV |
| Voltage ya kawaida |
12S betri ya lipo |
| Mzigo wa sasa bila mzigo |
1.2 A / 25 V |
| Upinzani wa ndani |
58 ma9 |
| Uzito wa motor |
345 g |
| Uzito wa bidhaa iliyofungwa |
669 g (180 x 140 x 85 mm) |
| Max. sasa |
47.0 A |
| Max. nguvu |
2036 W |
| Max. nguvu ya kusukuma |
7.1 kg |
| Nguvu iliyopimwa |
300 W |
| ESC inayopendekezwa |
MAD AMPX 80A (5-14S) |
| Propela zinazopendekezwa |
APC15X8, APC16X8 |
| Uzito wa UAV wakati wa kupaa |
12S-16"/ 10kg--Quadcopter; 15kg--Hexacopter; 20kg--Octocopter |
| Uzito wa kupaa wa rotor moja |
2 kg - 3 kg |
250KV Takwimu za Uendeshaji wa Kichambuzi (APC 15X8, AMPX 80A)
| Throttle [%] |
Voltage [V] |
Current [A] |
Nguvu ya Kuingiza [W] |
Nguvu ya Kutoka [W] |
Torque [N*m] |
RPM |
Thrust [gf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
44.56 |
1.33 |
59.0 |
35.8 |
0.114 |
3000 |
602 |
60.70 |
10.2 |
| 35 |
44.53 |
1.84 |
82.0 |
57.0 |
0.155 |
3511 |
774 |
69.50 |
9.4 |
| 40 |
44.50 |
2.66 |
118.4 |
84.9 |
0.206 |
3936 |
1033 |
71.80 |
8.7 |
| 45 |
44.47 |
3.48 |
154.8 |
114.6 |
0.251 |
4352 |
1284 |
74.10 |
8.3 |
| 50 |
44.44 |
4.98 |
221.3 |
175.1 |
0.338 |
4948 |
1641 |
79.10 |
7.4 |
| 55 |
44.41 |
6.65 |
295.3 |
241.8 |
0.421 |
5486 |
2054 |
81.90 |
7.0 |
| 60 |
44.32 |
8.54 |
378.5 |
314.4 |
0.504 |
5963 |
2429 |
83.10 |
6.4 |
| 65 |
44.27 |
10.63 |
470.6 |
396.2 |
0.623 |
6088 |
2812 |
84.30 |
6.0 |
| 70 |
44.20 |
13.02 |
575.5 |
488.5 |
0.686 |
6796 |
3264 |
84.90 |
5.7 |
| 75 |
44.14 |
16.24 |
716.8 |
616.0 |
0.808 |
7283 |
3843 |
85.90 |
5.4 |
| 80 |
44.06 |
19.54 |
861.0 |
748.5 |
0.920 |
7766 |
4235 |
86.90 |
4.9 |
| 85 |
43.98 |
23.11 |
1016.3 |
883.4 |
1.029 |
8202 |
4752 |
86.90 |
4.7 |
| 90 |
43.85 |
27.53 |
1207.1 |
1048.2 |
1.182 |
8469 |
5144 |
86.80 |
4.3 |
| 95 |
43.75 |
32.85 |
1437.3 |
1216.7 |
1.315 |
8836 |
5548 |
84.70 |
3.9 |
| 100 |
43.66 |
39.60 |
1728.8 |
1418.8 |
1.469 |
9225 |
5946 |
82.10 |
3.4 |
250KV Takwimu za Uendeshaji wa Uchambuzi (APC 16X8, AMPX 80A)
| Throttle [%] |
Voltage [V] |
Current [A] |
Input Power [W] |
Output Power [W] |
Torque [N*m] |
RPM |
Thrust [gf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
44.59 |
1.67 |
74.5 |
46.9 |
0.151 |
2956 |
717 |
63.00 |
9.6 |
| 35 |
44.55 |
2.41 |
107.4 |
74.4 |
0.206 |
3454 |
987 |
69.30 |
9.2 |
| 40 |
44.52 |
3.24 |
144.2 |
105.4 |
0.259 |
3879 |
1262 |
73.10 |
8.8 |
| 45 |
44.47 |
4.08 |
181.4 |
144.6 |
0.321 |
4298 |
1538 |
79.70 |
8.5 |
| 50 |
44.46 |
5.79 |
257.4 |
208.4 |
0.407 |
4894 |
1989 |
81.00 |
7.7 |
| 55 |
44.39 |
8.17 |
362.6 |
300.2 |
0.530 |
5404 |
2489 |
82.80 |
6.9 |
| 60 |
44.30 |
10.42 |
461.6 |
376.3 |
0.612 |
5868 |
2966 |
81.50 |
6.4 |
| 65 |
44.21 |
12.96 |
572.9 |
480.3 |
0.729 |
6291 |
3412 |
83.80 |
6.0 |
| 70 |
44.14 |
15.99 |
705.8 |
601.7 |
0.856 |
6710 |
3968 |
85.20 |
5.7 |
| 75 |
44.07 |
19.57 |
862.4 |
720.5 |
0.969 |
7104 |
4484 |
83.50 |
5.2 |
| 80 |
43.94 |
23.84 |
1047.4 |
860.5 |
1.088 |
7554 |
5067 |
82.20 |
4.8 |
| 85 |
43.83 |
28.13 |
1232.9 |
1027.8 |
1.245 |
7886 |
5548 |
83.40 |
4.5 |
| 90 |
43.66 |
33.32 |
1454.7 |
1205.0 |
1.402 |
8209 |
6213 |
82.80 |
4.3 |
| 95 |
43.53 |
39.27 |
1709.2 |
1405.6 |
1.577 |
8512 |
6725 |
82.20 |
3.9 |
| 100 |
43.35 |
46.96 |
2035.9 |
1647.1 |
1.775 |
8862 |
7330 |
80.90 |
3.5 |
250KV Maelezo (kutoka kwenye karatasi ya data)
- Hadithi ya grafu ya uchambuzi: I = sasa, P = nguvu ya kuingiza, b7 = ufanisi wa umeme, T = nguvu, N = kasi ya kuzunguka.
- Maelezo ya hali ya kipimo: data ilipimwa kwa voltage ya kuingiza ya 48 V, joto la 25C, katika kiwango cha baharini; kasi ya kuzunguka ilirekebishwa kwa throttle.
- Maelezo ya rejea pekee: Wakati joto la chumba ni 25C na hakuna kifaa kingine cha kupoza, sasa zaidi ya 47 A ni eneo lisilofanya kazi; 13 A hadi 47 A ni eneo la muda mfupi (takriban sekunde 10-30) la kufanya kazi; chini ya 13 A ni eneo la kufanya kazi linalodumu. Dhibiti muda wa kuendesha motor kulingana na joto la mazingira na hali ya kutolea joto.
540KV (6S) Tafsiri ya Kihandisi
| RPM/V |
540 KV |
| Voltage ya kawaida |
Betri ya lipo 6S |
| Sasa bila mzigo |
2.85 A / 10 V |
| Upinzani wa ndani |
13 ma9 |
| Uzito wa motor |
347 g |
| Uzito wa bidhaa iliyofungwa |
671 g (180 x 140 x 85 mm) |
| Upeo wa sasa |
92.5 A |
| Upeo wa nguvu |
1898 W |
| Upeo wa nguvu ya kusukuma |
6.7 kg |
| Nguvu ya pato iliyokadiriwa |
347 W |
| ESC inayopendekezwa |
MAD AMPX 120A (5-14S) |
| Propela zinazopendekezwa |
APC15X8, APC16X8 |
| Uzito wa UAV wakati wa kupaa |
12S-16"/ 10kg--Quadcopter; 15kg--Hexacopter; 20kg--Octocopter |
| Uzito wa kupaa wa rotor moja |
2.5 kg - 3 kg |
540KV Takwimu za Uendeshaji wa Uchambuzi (APC 15X8, AMPX 120A)
| Throttle [%] |
Voltage [V] |
Current [A] |
Input Power [W] |
Output Power [W] |
Torque [N*m] |
RPM |
Thrust [gf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
22.56 |
5.54 |
125.0 |
77.5 |
0.193 |
3842 |
913 |
62.00 |
7.3 |
| 35 |
22.49 |
7.35 |
165.3 |
108.4 |
0.239 |
4326 |
1152 |
65.60 |
7.0 |
| 40 |
22.44 |
10.29 |
230.9 |
162.8 |
0.324 |
4802 |
1563 |
70.50 |
6.8 |
| 45 |
22.36 |
12.68 |
283.5 |
207.8 |
0.377 |
5265 |
1835 |
73.30 |
6.5 |
| 50 |
22.29 |
15.71 |
350.1 |
271.7 |
0.470 |
5516 |
2173 |
77.60 |
6.2 |
| 55 |
22.18 |
18.52 |
410.7 |
330.7 |
0.536 |
5887 |
2441 |
80.50 |
5.9 |
| 60 |
22.08 |
22.63 |
499.7 |
394.2 |
0.595 |
6328 |
2809 |
78.90 |
5.6 |
| 65 |
21.98 |
26.67 |
586.2 |
463.2 |
0.652 |
6787 |
3151 |
79.00 |
5.4 |
| 70 |
21.90 |
32.45 |
710.5 |
549.5 |
0.737 |
7124 |
3617 |
77.30 |
5.1 |
| 75 |
21.79 |
38.29 |
834.1 |
655.0 |
0.840 |
7451 |
4016 |
78.50 |
4.8 |
| 80 |
21.56 |
45.70 |
985.5 |
768.2 |
0.930 |
7885 |
4426 |
78.00 |
4.5 |
| 85 |
21.38 |
51.77 |
1106.7 |
885.4 |
1.020 |
8293 |
4783 |
80.00 |
4.3 |
| 90 |
21.16 |
60.98 |
1290.3 |
1002.5 |
1.120 |
8545 |
5065 |
77.70 |
3.9 |
| 95 |
21.00 |
69.29 |
1454.7 |
1103.5 |
1.205 |
8748 |
5342 |
75.90 |
3.7 |
| 100 |
20.71 |
80.24 |
1661.9 |
1258.4 |
1.345 |
8935 |
5608 |
75.70 |
3.4 |
540KV Takwimu za Uendeshaji wa Uchambuzi (APC 16X8, AMPX 120A)
| Throttle [%] |
Voltage [V] |
Current [A] |
Nishati ya Kuingia [W] |
Nishati ya Kutoka [W] |
Torque [N*m] |
RPM |
Thrust [gf] |
Ufanisi [%] |
Ufanisi [gf/W] |
| 30 |
22.49 |
5.55 |
124.8 |
82.9 |
0.206 |
3843 |
1029 |
66.40 |
8.3 |
| 35 |
22.43 |
8.22 |
184.4 |
126.8 |
0.283 |
4273 |
1428 |
68.80 |
7.8 |
| 40 |
22.36 |
11.34 |
253.6 |
180.3 |
0.367 |
4688 |
1804 |
71.10 |
7.1 |
| 45 |
22.28 |
13.74 |
306.1 |
230.9 |
0.444 |
4966 |
2055 |
75.40 |
6.7 |
| 50 |
22.19 |
16.56 |
367.5 |
276.4 |
0.490 |
5386 |
2402 |
75.20 |
6.5 |
| 55 |
22.07 |
20.03 |
442.0 |
347.1 |
0.577 |
5747 |
2753 |
78.50 |
6.2 |
| 60 |
21.96 |
25.64 |
563.1 |
445.9 |
0.692 |
6157 |
3256 |
79.20 |
5.8 |
| 65 |
21.87 |
31.12 |
680.6 |
520.8 |
0.757 |
6573 |
3708 |
76.50 |
5.5 |
| 70 |
21.70 |
37.78 |
820.0 |
639.1 |
0.885 |
6896 |
4161 |
77.90 |
5.1 |
| 75 |
21.54 |
45.42 |
978.2 |
771.1 |
1.005 |
7329 |
4685 |
78.80 |
4.8 |
| 80 |
21.35 |
53.28 |
1137.4 |
904.9 |
1.133 |
7629 |
5226 |
79.60 |
4.6 |
| 85 |
21.16 |
62.11 |
1314.4 |
991.4 |
1.191 |
7945 |
5624 |
75.40 |
4.3 |
| 90 |
20.95 |
72.06 |
1509.9 |
1111.3 |
1.280 |
8291 |
6056 |
73.60 |
4.0 |
| 95 |
20.72 |
84.24 |
1744.9 |
1279.3 |
1.452 |
8415 |
6364 |
73.30 |
3.7 |
| 100 |
20.52 |
92.53 |
1898.4 |
1370.3 |
1.527 |
8571 |
6784 |
72.20 |
3.6 |
540KV Maelezo (kutoka kwenye karatasi ya data)
- Hadithi ya grafu ya uchambuzi: I = sasa, P = nguvu ya kuingiza, b7 = ufanisi wa umeme, T = nguvu ya kusukuma, N = kasi ya kuzunguka.
- Kumbukumbu ya hali ya kipimo: data ilipimwa kwa voltage ya kuingiza ya 24 V, joto la 25C, katika kiwango cha baharini; kasi ya kuzunguka ilirekebishwa kwa throttle.
- Kumbukumbu ya rejea pekee: Wakati joto la chumba ni 25C na hakuna kifaa kingine cha kupoza, sasa zaidi ya 92 A ni eneo lisilofanya kazi; 31 A hadi 92 A ni eneo la muda mfupi (takriban sekunde 10-30) la kufanya kazi; chini ya 31 A ni eneo la kufanya kazi endelevu. Dhibiti muda wa kufanya kazi wa motor kulingana na joto la mazingira na hali ya kutolea joto.
Nini Kimejumuishwa
- Motor x1
- Prop Adapter x1
- 4.0 mm Bullet Connector x3
- Prop Plate x1
- Shaft Locking Collar x1
- Cross Plate x1
- M8 Nut x1
- M3*3 Machine Screw x1
- Heat Shrinkable Tube x3
- M3*8 Prop Adapter Screws x4
- M4*8 X-Mount Installation Screw x4
- M3*8 Motor Screws x4
- Sticker x2
Maombi
- mifumo ya propulsion ya ndege ya eVTOL
- Multirotors (quadcopters, hexacopters, octocopters) kama ilivyoelezwa katika karatasi ya data
Kwa uchaguzi na uthibitisho wa ufanisi (bateri/ESC/mpropeller kuendana), wasiliana na [email protected] or tembelea https://rcdrone.top/.
Maelezo

MAD X4125 IPE V1.0 orodha ya michoro ya motor ya ndege ya eVTOL inaonyesha vipimo muhimu na muundo wa mashimo ya kufunga kwa usakinishaji sahihi.

MAD X4125 IPE V1.0 motor kit inajumuisha adapter ya prop, sahani ya msalaba, nut ya prop, collar ya kufunga shat, viunganishi vya bullet, na viscrew vya kufunga kwa ajili ya usakinishaji.

MAD X4125 250KV eVTOL ndege drone motor imeorodheshwa kwa mipangilio ya 12S (20–30V) ikiwa na uzito wa 345g na ufanisi zaidi ya 82%.

MAD X4125 IPE V1.0 motor imeorodheshwa kwa 540KV na inajumuisha curve ya ufanisi pamoja na meza za utendaji za kina kwa ajili ya rejeleo la mipangilio.