Overview
MAD M40C30 PRO IPE ni motor ya drone isiyo na brashi ya uzito mzito iliyoundwa kwa ajili ya VTOL zenye mzigo mkubwa na majukwaa ya UAV ya mizigo. Imewekwa kwa matumizi na propela za nyuzi za kaboni za inchi 47.5–54 na pia inatumika katika ujenzi wa paramotor za umeme na mfumo wa PAV (Kifaa cha Anga Binafsi).
Vipengele Muhimu
- Upeo wa nguvu (kutoka kwa data iliyotolewa): thrust iliyokadiriwa ya kuanguka 20–35 kgf (10KV) / 20–30 kgf (43KV); upeo wa nguvu hadi 73 kgf (10KV) / 80 kgf (43KV)
- Uzito ulioimarishwa: 3460 g
- Ufanisi (lebo): >80% (10KV) / >84% (43KV)
- Daraja la ulinzi wa motor: IP45
- Kuondoa joto kwa njia ya katikati: NDIYO
- Vikundi vya kuongoza vilivyo na ukubwa mkubwa (kwa kupunguza resonance na athari za gyroscopic)
Maelezo ya Kiufundi
Data ya Motor (Kawaida)
| Mfano wa Motor | MAD M40C30 IPE V3.0 | Idadi ya jozi za nguzo | 15 |
| Stator | Inayopambana na kutu | Waya wa varnished Kiwango | 220°C |
| Ukubwa wa Motor | D:151.4 x 81 mm | Digrii ya Magnet | 180°C |
| Digrii ya Ulinzi | IP45 | 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 x 6; D:32 M4 x 4 | Usawa wa Motor | ≤30 mg |
| Nyenzo ya Shat | ND: 25 mm | Shimo za Kuweka Motor | D:65 M6 x 6 |
| Mpira | NSK 6818ZZCM | Jaribio la Kuondoa | 500 V |
Mchoro / Vipimo vya Kuweka (kutoka mchoro)
| Upeo wa nje | Ø151.4 |
| Urefu wa mwili | 81 |
| Alama za vipimo vya ziada | 8; Ø90; 4; Ø25; 22 |
| Mashimo ya kufunga motor | Ø65-M6 x 6 |
| Mashimo ya kufunga propela | Ø50-M6 x 6; Ø32-M4 x 4 |
| Alama ya muundo wa mashimo | Ø50-Ø6.2 x 6 |
10KV Variant (MAD M40C30 IPE PRO 10KV)
- Label: ENERGY EFFICIENT 10KV (Toleo la Wataalamu wa Sekta)
- Recommended hover thrust: 20–35 kgf
- Maximum thrust: 73 kgf
- Optimized weight: 3460 g
- Efficiency (label): >80%
- Test banner setup: FLUXER PRO 54x24 GLOSSY; Recommended ESC: FOC IGBT 30A (80–440V)
- Label: 400V MAX; 132°C
| RPM/V | 10 KV | Nominal Voltage | 100S betri ya lipo |
| No Load Current | 1.8A / 50V | Upinzani wa ndani | 387mΩ |
| Uzito wa Motor | 3460 g | Uzito wa Kifurushi cha Bidhaa | 4616g (260 x 210 x 120 mm) |
| Upeo wa Sasa | 41.6 A | Upeo wa Nguvu | 16532W |
| Upeo wa nguvu | 73 kg | Upeo wa Torque | 47.4 Nm |
| ESC Inapendekezwa | FOC IGBT 30A (80–440V) | Propela Inapendekezwa | 54x24 |
| Uzito wa UAV wakati wa kupaa | 100S-54" / 100kg--Quadcopter; 150kg--Hexacopter; 200kg--Octocopter | Uzito wa rotor mmoja wakati wa kupaa | 20kg ~ 35kg |
Jedwali la Takwimu za Mtihani wa 10KV (400 V input)
| Throttle [%] | Voltage [V] | Current [A] | Input Power [W] | Output Power [W] | Torque [N*m] | RPM | Thrust [kgf] | Ufanisi [%] | Ufanisi [gf/W] |
|---|---|---|---|---|---|---|---|---|---|
| 25 | 398.3 | 1.58 | 629.3 | 430.3 | 4.840 | 849 | 7 | 68.4 | 11.7 |
| 30 | 398.4 | 2.46 | 980.1 | 753.2 | 7.010 | 1026 | 11 | 76.8 | 11.0 |
| 35 | 397.9 | 3.92 | 1559.8 | 1223.7 | 9.730 | 1201 | 15 | 78.5 | 9.7 |
| 40 | 397.8 | 5.88 | 2339.1 | 1839.2 | 12.820 | 1370 | 20 | 78.6 | 8.6 |
| 45 | 397.6 | 7.93 | 3153.0 | 2584.9 | 16.070 | 1536 | 25 | 82 | 8.0 |
| 50 | 397.6 | 10.4 | 4135.0 | 3463.0 | 19.510 | 1695 | 31 | 83.7 | 7.4 |
| 55 | 397.7 | 13.47 | 5357.0 | 4479.1 | 23.070 | 1854 | 36 | 83.6 | 6.7 |
| 60 | 397.5 | 17.23 | 6848.9 | 5701.4 | 27.100 | 2009 | 42 | 83.2 | 6.2 |
| 65 | 397.7 | 21.7 | 8630.1 | 7154.5 | 31.630 | 2160 | 49 | 82.9 | 5.7 |
| 70 | 397.5 | 26.8 | 10653.0 | 8787.6 | 36.390 | 2306 | 57 | 82.5 | 5.3 |
| 75 | 397.5 | 33.13 | 13169.2 | 10609.3 | 41.470 | 2443 | 64 | 80.6 | 4.9 |
| 80 | 397.3 | 40.37 | 16039.0 | 12565.8 | 46.600 | 2575 | 72 | 78.3 | 4.5 |
| 85 | 397.4 | 41.6 | 16531.8 | 12870.0 | 47.360 | 2595 | 73 | 77.8 | 4.4 |
10KV maelezo ya mtihani (maana halisi): Takwimu ni thamani za nadharia wakati voltage ya kuingiza ni 400 V (kwa rejea). Katika 25°C bila kifaa kingine cha kupoza: sasa zaidi ya 42 A ni eneo lisilofanya kazi; 10–42 A ni eneo la muda mfupi (takriban 10–30 s) la kufanya kazi; chini ya 10 A ni eneo la kufanya kazi endelevu. Dhibiti muda wa kuendesha motor kulingana na joto la mazingira na hali za kutolea joto.
43KV Tofauti (MAD M40C30 IPE PRO 43KV)
- Lebo: ENERGY EFFICIENT 43KV (Toleo la Wataalamu wa Sekta)
- Mapendekezo ya mvutano wa hover: 20–30 kgf
- Mvutano wa juu zaidi: 80 kgf
- Uzito ulioimarishwa: 3460 g
- Ufanisi (lebo): >84%
- Mpangilio wa bendera ya mtihani: FLUXER PRO 47.5x17.4 GLOSSY; ESC inayopendekezwa: AMPX 300A (12–24S)
- Lebo: 24S MAX; 125°C
| RPM/V | 43 KV | Voltage ya kawaida | Betri ya lipo 24S |
| Current isiyo na mzigo | 4.4A / 30V | Upinzani wa ndani | 20.3mΩ |
| Uzito wa Motor | 3460 g | Uzito wa Bidhaa Iliyofungwa | 4616g (260 x 210 x 120 mm) |
| Current ya Juu | 238 A | Nguvu ya Juu | 22744W |
| Upeo wa nguvu | 80 kg | Upeo wa Torque | 47.7 Nm |
| ESC Inayopendekezwa | MAD AMPX 300A (12–24S) | Propellers Zinazopendekezwa | 47.5x17. |
| Uzito wa kuondoka wa UAV | 24S-47.5" / 100kg--Quadcopter; 150kg--Hexacopter; 200kg--Octocopter | Uzito wa kuondoka wa rotor mmoja | 20kg ~ 30kg |
Jedwali la Takwimu za Jaribio la 43KV (96 V input)
| Throttle [%] | Voltage [V] | Current [A] | Nguvu ya Kuingia [W] | Nguvu ya Kutoka [W] | Torque [N*m] | RPM | Thrust [gf] | Ufanisi [%] | Ufanisi [gf/W] |
|---|---|---|---|---|---|---|---|---|---|
| 30 | 97.62 | 8.85 | 863.9 | 689.4 | 5.255 | 1253 | 8845 | 79.8 | 10.2 |
| 35 | 97.64 | 13.91 | 1358.2 | 1104.2 | 7.193 | 1466 | 12135 | 81.3 | 8.9 |
| 40 | 97.51 | 19.58 | 1909.2 | 1647.7 | 9.468 | 1662 | 15887 | 86.3 | 8.3 |
| 45 | 97.53 | 27.81 | 2712.3 | 2294.6 | 11.884 | 1844 | 20028 | 84.6 | 7.4 |
| 50 | 97.37 | 36.2 | 3524.8 | 3038.4 | 14.322 | 2026 | 24035 | 86.2 | 6.8 |
| 55 | 97.34 | 48.61 | 4731.7 | 4031.4 | 17.327 | 2222 | 28990 | 85.2 | 6.1 |
| 60 | 97.15 | 62.96 | 6116.6 | 5254.1 | 20.751 | 2418 | 34384 | 85.9 | 5.6 |
| 65 | 97.05 | 78.27 | 7596.1 | 6532.6 | 23.995 | 2600 | 39773 | 86 | 5.2 |
| 70 | 96.83 | 92.43 | 8950.0 | 7616.4 | 26.259 | 2770 | 45158 | 85.1 | 5.0 |
| 75 | 96.73 | 104.38 | 10096.7 | 8562.0 | 27.859 | 2935 | 49681 | 84.8 | 4.9 |
| 80 | 96.54 | 122.47 | 11823.3 | 9836.9 | 30.412 | 3089 | 55621 | 83.2 | 4.7 |
| 85 | 96.27 | 154.38 | 14862.2 | 12201.8 | 36.021 | 3235 | 62008 | 82.1 | 4.2 |
| 90 | 96.04 | 182.54 | 17531.1 | 14095.0 | 39.789 | 3383 | 66104 | 80.4 | 3.8 |
| 95 | 95.73 | 211.35 | 20232.5 | 15943.2 | 43.527 | 3498 | 73163 | 78.8 | 3.6 |
| 100 | 95.62 | 237.86 | 22744.2 | 17899.7 | 47.656 | 3587 | 80125 | 78.7 | 3.5 |
43KV nota ya mtihani (maana halisi): Takwimu ni thamani za nadharia wakati voltage ya kuingiza ni 96 V (kwa rejea). Katika 25°C bila kifaa kingine cha kupoza: sasa zaidi ya 238 A ni eneo lisilofanya kazi; 60–238 A ni eneo la muda mfupi (takriban sekunde 10–30) la kufanya kazi; chini ya 60 A ni eneo la kufanya kazi endelevu. Dhibiti muda wa kuendesha motor kulingana na joto la mazingira na hali za kutolea joto.
Mipangilio Inayopendekezwa
- 43KV: ESC AMPX 300A (12–24S); propela FLUXER PRO 47.5x17.4 (mng'aro)
- 35KV: propela HB30-54x24
- 10KV + FOC ESC combo: propela HB30-54x24; HB30-CB2 47.5x18.5; HB30 47.5x17.4; HB30-52x19
Ni Nini Imejumuishwa
- Motor x1
- Propeller Plate x1
- Pin ya Kuweka x1
- 8.0mm Bullet Connector x3
- Tube ya Kupunguza Joto x3
- M6*25 Screws za Motor x6
- M6*35 Screws za Prop Adapter x6
- M6*40 Screws za Propeller x6
- Sticker x2
Matumizi
- Drones za mizigo zisizo na rubani na majukwaa ya VTOL
- Mifumo mikubwa ya UAV multirotor
- Ujenzi wa paramotor ya umeme na mfumo wa PAV
Kuhusu maswali ya ulinganifu (ESC, propeller, wiring, au uunganisho), wasiliana na msaada kwa support@rcdrone.top au tembelea https://rcdrone.top/ .
Maelezo

Vipimo vya motor isiyo na brashi ya MAD M40C30 PRO IPE na muundo wa Φ50 wa kufunga husaidia kuthibitisha ulinganifu kwenye fremu yako na mlango wa motor.

Motor ya drone isiyo na brashi ya MAD M40C30 PRO IPE inajumuisha sahani ya propela, pini ya kuweka, viunganishi vya bullet 8.0mm, joto la kupunguza, viscrew, na vichapo vya kufunga.

Motor isiyo na brashi ya MAD M40C30 PRO IPE ina kiwango cha 10KV na inajumuisha chati ya utendaji yenye vipimo muhimu kama vile 400V max.

Motor isiyo na brashi ya MAD M40C30 PRO IPE imeorodheshwa kwa 43KV ikiwa na msaada wa 24S na anuwai ya nguvu ya 20–30 kgf kwa ujenzi wa drone mzito.
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