Flycci Motor UM8110 long-endurance drone motor for agriculture, photography drones, drone motors

product details

Parameter:

Motor type：UM8110

Structural form：36N42P

Weight：305g

Stator core dimensions：φ81*10 mm

UM8110 KV85

Recommended for lithium battery：12S-14S

Recommended propeller：30-32inches

Multi-rotor take-off weight：3.5KG-4.5KG/shaft

UM8110 KV110

Recommended for lithium battery：12S-14S

Recommended propeller：26-28inches

Multi-rotor take-off weight：3.5KG-4.5KG/shaft

UM8110 KV150

Recommended for lithium battery：12S-14S

Recommended propeller：20-24inches

Multi-rotor take-off weight：3.0KG-4.5KG/shaft

DRAWING

TEST REPORT

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
UM8110 KV195		80A (6S-14S)	P2275 22 inch straight propeller		Vertical takeoff and landing compound wing UAV	5.0KG-6.0KG /uniaxial	12.9KG		3748W
Load test data						Lithium Battery :12S 44.4V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
44.12	2789	7.05		3196	311.05		8.97	0.93	40%
44.07	3416	9.61		3538	423.51		8.07	1.14	45%
44.06	4000	11.87		3812	522.99		7.65	1.31	50%
44.02	4732	15.18		4138	668.22		7.08	1.54	55%
43.99	5615	19.04		4462	837.57		6.70	1.79	60%
43.92	6346	23.59		4776	1036.07		6.13	2.07	65%
43.87	7256	28.43		5065	1247.22		5.82	2.35	70%
43.81	8281	34.79		5360	1524.15		5.43	2.72	75%
43.72	9080	40.81		5635	1784.21		5.09	3.02	80%
43.61	10112	48.27		5879	2105.05		4.80	3.42	85%
43.55	10814	55.25		6119	2406.14		4.49	3.76	90%
43.49	11553	62.72		6336	2727.69		4.24	4.11	95%
43.38	11918	69.76		6570	3026.19		3.94	4.40	100%
Load test data						Lithium Battery :12S 48V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
47.73	3192	7.99		3435	381.36		8.37	1.06	40%
47.69	3769	10.14		3727	483.58		7.79	1.24	45%
47.64	4526	13.44		4085	640.28		7.07	1.50	50%
47.61	5275	16.65		4448	792.71		6.65	1.70	55%
47.57	6191	21.17		4776	1007.06		6.15	2.01	60%
47.53	7195	26.27		5065	1248.61		5.76	2.35	65%
47.43	8034	31.99		5390	1517.29		5.29	2.69	70%
47.38	8965	38.21		5703	1810.39		4.95	3.03	75%
47.31	9933	45.33		5965	2144.56		4.63	3.43	80%
47.19	10786	53.38		6226	2519.00		4.28	3.86	85%
47.08	11604	61.3		6451	2886.00		4.02	4.27	90%
46.98	12352	70.03		6616	3290.01		3.75	4.75	95%
46.86	12909	79.99		6773	3748.33		3.44	5.29	100%
The above figures are from the actual melting room: sea level requires height, E8-2024 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
UM8110 KV195		80A (6S-14S)	P2070 20 inch straight propeller		Vertical takeoff and landing compound wing UAV	4.5KG-5.5KG /uniaxial	12KG		3592W
Load test data						Lithium Battery :14S 51.8V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
51.56	2238	5.84		3817	301.11		7.43	0.75	40%
51.52	2739	7.56		4243	389.49		7.03	0.88	45%
51.52	3248	9.72		4629	500.77		6.49	1.03	50%
51.48	3723	12.03		5002	619.30		6.01	1.18	55%
51.43	4488	14.87		5411	764.76		5.87	1.35	60%
51.42	5185	18.4		5819	946.13		5.48	1.55	65%
51.37	5869	22.44		6239	1152.74		5.09	1.76	70%
51.31	6709	27.12		6631	1391.53		4.82	2.00	75%
51.25	7490	31.92		7023	1635.90		4.58	2.22	80%
51.14	8358	37.79		7387	1932.58		4.32	2.50	85%
51.13	9310	43.76		7707	2237.45		4.16	2.77	90%
51.03	10179	50.12		8010	2557.62		3.98	3.05	95%
50.93	11046	58.61		8338	2985.01		3.70	3.42	100%
Load test data						Lithium Battery :14S 56V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
55.77	2521	6.27		4091	349.68		7.21	0.82	40%
55.76	3002	8.37		4540	466.71		6.43	0.98	45%
55.69	3663	10.67		4976	594.21		6.16	1.14	50%
55.71	4234	13.12		5360	730.92		5.79	1.30	55%
55.64	4892	16.24		5784	903.59		5.41	1.49	60%
55.60	5699	20.32		6226	1129.79		5.04	1.73	65%
55.55	6542	24.84		6647	1379.86		4.74	1.98	70%
55.48	7449	30.11		7076	1670.50		4.46	2.25	75%
55.43	8375	35.8		7465	1984.39		4.22	2.54	80%
55.34	9377	41.97		7834	2322.62		4.04	2.83	85%
55.28	10221	48.59		8170	2686.06		3.81	3.14	90%
55.19	10982	55.15		8512	3043.73		3.61	3.41	95%
55.06	12066	65.25		8828	3592.67		3.36	3.89	100%
The above figures are from the actual melting room: sea level requires height, E8-2024 test platform

Power configuration Measured data
Motor	ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM8110 65KV	60A	F34112 34inch folding propeller		Multi-rotor drone	3KG-3.5KG/shaft	250W	7KG	800W
Load test data					Lithium Battery ,Voltage
					12S ,44V
Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
1547	1.73		1016	76.12		20.3232	0.72	40%
1939	2.46		1131	108.24		17.9139	0.91	45%
2378	3.23		1255	142.12		16.7323	1.08	50%
2805	3.98		1359	175.12		16.0176	1.23	55%
3284	5.14		1461	226.16		14.5207	1.48	60%
3699	6.16		1559	271.04		13.6474	1.66	65%
4251	7.65		1659	336.6		12.6292	1.94	70%
4836	9.03		1757	397.32		12.1715	2.16	75%
5369	10.68		1852	469.92		11.4253	2.42	80%
6193	14.32		2029	630.08		9.8289	2.97	90%
6970	18.1		2183	796.4		8.7519	3.48	100%
63% throttle force 4KG continuous operation for 15 minutes, motor temperature 59℃, ESC temperature 43℃, ambient temperature 25℃
The above data comes from the actual inspection room, sea level, C2-2023 test platform

Power configuration Measured data
Molor	ESC	Propelle		Applicable models	Applicable takeofl weight	Rated power	Max thrust	Max power
UM8110 100KV	60A	G2995 29inch straight propeller		Multi-rotor drone	3KG-4KG/shaft	380W	7.7KG	1080W
Load test data					Lithium Battery ,Voltage
Load test data					12S ,44V
Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
1682	2.42		1565	106.48		15.7964	0.65	40%
2045	3.17		1728	139.48		14.6616	0.77	45%
2477	4.32		1882	190.08		13.0314	0.96	50%
2943	5.4		2072	237.6		12.3864	1.10	55%
3594	7.18		2238	315.92		11.3763	1.35	60%
4067	8.73		2408	384.12		10.5878	1.52	65%
4576	10.55		2559	464.2		9.8578	1.73	70%
5135	12.5		2692	550		9.3364	1.95	75%
5617	14.58		2829	641.52		8.7558	2.17	80%
6713	19.5		3079	858		7.8240	2.66	90%
7650	24.42		3300	1074.48		7.1197	3.11	100%
The above data comes from the actual inspection room, sea level, C2-2023 test platform

Power configuration Measured data
Molor	ESC	Propelle		Applicable models	Applicable takeofl weight	Rated power	Max thrust	Max power
UM8110 85KV	60A	G2995 29inch straight propeller		Multi-rotor drone	3KG-4KG/shaft	380W	8.4KG	1200W
Load test data					Lithium Battery ,Voltage
Load test data					14S ,52.5V
Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
1737	2.28		1600	119.70		14.5113	0.71	40%
2094	2.84		1767	149.10		14.0443	0.81	45%
2563	3.75		1937	196.88		13.0184	0.97	50%
3040	4.9		2131	257.25		11.8173	1.15	55%
3689	6.4		2312	336.00		10.9792	1.39	60%
4171	7.7		2486	404.25		10.3179	1.55	65%
4754	9.64		2647	506.10		9.3934	1.83	70%
5219	11.26		2795	591.15		8.8286	2.02	75%
5918	13.15		2942	690.38		8.5722	2.24	80%
7149	17.7		3218	929.25		7.6933	2.76	90%
8438	23.05		3460	1210.13		6.9728	3.34	100%
The above data comes from the actual inspection room, sea level, C2-2023 test platform

Power configuration Measured data
Molor	ESC	Propelle		Applicable models	Applicable takeofl weight	Rated power	Max thrust	Max power
UM8110 100KV	60A	P3095 30inch straight propeller		Multi-rotor drone	3.5KG-4.5KG/shaft	470W	8.4KG	1300W
Load test data					Lithium Battery ,Voltage
					12S ,44V
Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
2105	3		1509	132		15.9470	0.84	40%
2537	4.23		1660	186.12		13.6310	1.07	45%
3003	5.64		1809	248.16		12.1011	1.31	50%
3598	7.05		1963	310.2		11.5990	1.51	55%
4185	8.95		2123	393.8		10.6272	1.77	60%
4845	11.14		2256	490.16		9.8845	2.07	65%
5290	13.3		2408	585.2		9.0396	2.32	70%
5929	15.6		2514	686.4		8.6378	2.61	75%
6419	18.11		2618	796.84		8.0556	2.91	80%
7479	23.61		2843	1038.84		7.1994	3.49	90%
8397	29.5		2986	1298		6.4692	4.15	100%
63% throttle force 4KG continuous operation for 15 minutes, motor temperature 59℃, ESC temperature 43℃, ambient temperature 25℃
The above data comes from the actual inspection room, sea level, C2-2023 test platform