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T-MOTOR MF1604VP Klapppropeller aus Polymer mit manuell verstellbarem Steigungswinkel

About T-MOTOR MF1604VP Polymer Manual Pitch Folding Propeller:

MF1604VP 16.4*5.9 inch polymer manual pitch folding propeller is a new type of propeller designed by T-MOTOR for multi-rotor and drogue UAVs. Compared with traditional propellers, MF1604VP provides a more flexible solution for complex and changeable working conditions and various power requirements, and it can be adjusted manually by changing the positioning block. The MF1604VP adopts an advanced aerodynamic design, which significantly improves flight efficiency at high speed and high altitude. Its large swept back tip and downward curved winglet design effectively improves the vortex distribution of the tip and reduces energy consumption and vibration, making it an ideal choice for professional users in model development and rapid switching between multiple scenarios. The maximum pulling force measured under throttle is 2.8kg (positioning block is 7.5°).

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Top-Highlights

Quick and flexible adjustment of the propeller pitch by changing the positioning block
Advanced large swept-back tip and downward curved winglet design enhance vortex distribution, reduce blade vibration and improve efficiency.
Enhanced blade root design, prolonging the service life of the propeller blades.

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MF1604VP Highlights:

- Adopting new wing shape with large swept back tip and downward curved winglet design to improve the vortex distribution of the tip and realize the double enhancement of pulling force and efficiency;
- Enhanced blade root design, together with improved material formula, greatly improves the service life of alternating load, and is more suitable for the large pulling force working condition and co-axial power mode;
- Smaller change of rotational damping in the whole life cycle of the paddle: compared with the original hard compression assembly method, the gasket paddle root assembly is always in the state of compression, which greatly reduces the wear of the gasket and makes the rotational damping change in the whole life cycle of the paddle smaller and avoids the situation that the rotational tightness of the blade varies with the life span and there is a big difference between the paddle and the vibration, which is more safe and reliable;

Packing List Includes:

● Package size 211*86*42mm
● MF1604VP polymer manual pitch folding Propeller * 1 pair
● MF1604 center positioning block (+2.5°)-CCW*1
● MF1604 center positioning block (+2.5°)-CW*1
● MF1604 Center Positioning Block (-2.5°)-CCW*1
● MF1604 Center Positioning Block (-2.5°)-CW*1
● MF1604 center positioning block (+5°)-CCW*1
● MF1604 Center Positioning Block (+5°)-CW*1
● 20*14*3.3mm pads*2
● M3*10mm cup head socket screws*4

Matching Guide:

T-MOTOR MN4012 KV340 Motor
T-MOTOR MN4014 KV330 Motor
T-MOTOR U7 KV490 Motor
FLAME 60A 12S V2.0 ESC
FLAME 180A 12S V2.0 ESC

MF VP SERIES PROPELLER

Manual Variable-Pitch Series

Simplicity Over Complexity, Consistency in Performance

Specially designed to address the issues of low flight efficiency at high speeds and high altitudes, this series is suitable for aircraft development and professional users requiring rapid switching across multiple scenarios.

tmotor mf1604vp prop consistency in performance

Manual Variable-Pitch Series

Flexible and easy-to-use drone propulsion system enhances flight efficiency in various operating conditions.

Typical application scenarios include high-speed flight, high-altitude flight, adjustments for overall aircraft weight, and fine-tuning of custom propeller performance.

Limitations of Traditional Propellers: Fixed pitch and fixed aerodynamic characteristics leading to limited power and flight condition matching.

Drawbacks of the adjustable propellers available from the market: Low adjustment precision, complicated operation, requires large auxiliary tools, and cannot be quickly adjusted on-site.

T-MOTOR (New) manual adjustable variable-pitch series solution: Designed for complex and changing working conditions with diverse power demands, we provide flexible solutions that allow for quick manual pitch adjustment by simply changing the positioning blocks.

Quick Assembly and Disassembly Precise and Reliable

Quick to replace without requiring professional training—easy to learn and use. The pitch adjustment accuracy remains unaffected by manual operation errors with user-friendly operation.

Methodical Approach

Using calculation tables derived from extensive experimental data, users can quickly find the required pitch angle based on the operating scenario and simple parameters.

(7.5°, 10°, and other positioning blocks are available upon request for customization.)

T-MOTOR MF1604VP Propeller Positioning Block Selection Reference Table

Performance Comparison

The efficiency curve of three positioning blocks (pitches) under different airflow speeds

(Example: MN605 KV170 + FLAME 180A 12S V2.0 + MF2211VP, Flight inclination 30°, S0, S5, S10, S15 respectively represents speed 0m/s, 5m/s, 10m/s, 15m/s, D0, D2.5, D5 respectively represents 0° positioning block, 2.5° positioning block, and 5° positioning block.)

Prototype Propellers Customization

Standard Customization

MOQ 1, with pitch angle customizable to 0.01°.

Assisted Customization

For mass production, engineers assist in determining the angle, and the customized pitch angle can be fixed before leaving the factory.

T-MOTOR MF1604VP Propeller Standrd Customization

For mass production, engineers assist in determining the angle, and the customized pitch angle can be fixed before leaving the factory.

Technical Drawing

Specification

Model NO.	MF1604VP	T-MOTOR Series	Folding
Weight (Single Blade)	38.3g	Package Weight	158g
Diameter	16.4inch（416.56mm）	Package Size	2118642mm
Pitch	5.9inch（149.86mm）	Material	Polymer+CF
Recommended Thrust	0.5~2.2kg	Recommended Max Thrust	3kg
Ambient Temp	-40℃～65℃	Storage Temp/Humidity	-10℃～50℃/＜85%

Recommendation
Recommended ESC	FLAME 60A 12S V2.0/FLAME 180A 12S V2.0	Recommended Motor	MN4012/MN4014/U7

Positioning Block Selection Reference Table
Flight Speed	0~10m/s	5~15m/s	10~20m/s	15~25m/s	20~30m/s
Positioning Block	0°	2.5°	5°	7.5° (Not Recommended)	10° (Not Recommended)
*Applicable to flight conditions of 0~2000m
Flight Altitude	0~1000m	0~2000m	0~3000m	1000~4000m	2000~5000m
Positioning Block	0°	2.5°	5°	7.5° (Not Recommended)	10° (Not Recommended)
*Applicable to flight conditions below 15m/s
Pitch (Inch)	5.2	6.9	8.7	10.5	12.3
Positioning Block	0°	2.5°	5°	7.5° (Not Recommended)	10° (Not Recommended)

Test Data

Type	Throttle	Voltage (V)	Thrust (gf)	Torque (N*m)	Current (A)	RPM	Power (W)	Efficiency (gf / W)	Operating Temperature (℃)
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (0°)	10%	24	90	0.02	0.30	1405	3	12.43	40 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25℃)
	15%	24	156	0.04	0.50	1748	7	13.13
	20%	24	232	0.05	0.75	2049	11	12.99
	25%	24	315	0.07	1.04	2343	17	12.66
	30%	24	404	0.08	1.42	2627	22	11.92
	35%	24	500	0.10	1.82	2905	30	11.48
	40%	24	616	0.13	2.36	3189	43	10.89
	45%	24	722	0.14	2.97	3469	51	10.17
	50%	24	874	0.17	3.72	3758	67	9.85
	55%	24	988	0.20	4.48	4019	84	9.24
	60%	24	1132	0.22	5.30	4265	98	8.96
	65%	24	1252	0.24	6.17	4501	113	8.51
	70%	24	1380	0.27	7.10	4728	134	8.17
	75%	24	1503	0.29	8.07	4947	150	7.84
	80%	24	1637	0.31	9.14	5154	167	7.55
	85%	24	1768	0.34	10.29	5376	191	7.25
	90%	24	1921	0.37	11.60	5592	217	7.00
	95%	24	2065	0.40	12.92	5801	243	6.77
	100%	24	2275	0.44	14.89	6077	280	6.48
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (+2.5°)	10%	24	126	0.03	0.35	1357	4	14.96	42 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25℃)
	15%	24	200	0.04	0.57	1666	7	14.63
	20%	24	300	0.06	0.89	1996	13	14.14
	25%	24	437	0.08	1.25	2276	19	14.63
	30%	24	527	0.10	1.67	2550	27	13.16
	35%	24	607	0.13	2.16	2817	38	11.73
	40%	24	725	0.15	2.79	3090	49	10.88
	45%	24	854	0.18	3.51	3356	63	10.17
	50%	24	1013	0.21	4.43	3641	80	9.59
	55%	24	1145	0.24	5.29	3875	97	9.07
	60%	24	1304	0.27	6.26	4099	116	8.74
	65%	24	1413	0.29	7.28	4316	131	8.16
	70%	24	1532	0.32	8.42	4517	151	7.65
	75%	24	1671	0.35	9.61	4724	173	7.32
	80%	24	1797	0.38	10.83	4919	196	6.99
	85%	24	2002	0.41	12.23	5114	220	6.91
	90%	24	2147	0.44	13.71	5306	244	6.62
	95%	24	2321	0.48	15.37	5499	276	6.39
	100%	24	2544	0.53	17.68	5754	319	6.11
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (+5°)	10%	24	153	0.03	0.41	1322	4	15.56	47 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25℃)
	15%	24	238	0.05	0.66	1634	9	14.97
	20%	24	343	0.07	1.02	1951	14	14.03
	25%	24	466	0.10	1.42	2169	23	13.70
	30%	24	592	0.12	1.91	2488	31	12.97
	35%	24	696	0.15	2.49	2734	43	11.69
	40%	24	823	0.18	3.20	2995	56	10.75
	45%	24	972	0.21	4.07	3244	71	10.00
	50%	24	1122	0.24	5.00	3477	87	9.40
	55%	24	1281	0.28	6.17	3728	109	8.72
	60%	24	1422	0.31	7.24	3935	128	8.26
	65%	24	1581	0.35	8.46	4135	152	7.86
	70%	24	1708	0.39	9.77	4329	177	7.37
	75%	24	1848	0.42	11.14	4507	198	7.00
	80%	24	1990	0.45	12.60	4693	221	6.67
	85%	24	2138	0.49	14.20	4871	250	6.38
	90%	24	2308	0.53	15.95	5040	280	6.14
	95%	24	2460	0.56	17.75	5221	306	5.89
	100%	23	2709	0.62	20.49	5449	354	5.64
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (+7.5°)	10%	24	195	0.05	0.46	1293	7	17.78	52 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25℃)
	15%	24	276	0.07	0.76	1596	12	15.14
	20%	24	382	0.09	1.16	1901	18	13.73
	25%	24	497	0.12	1.65	2162	27	12.61
	30%	24	625	0.15	2.21	2417	38	11.79
	35%	24	744	0.18	2.87	2647	50	10.82
	40%	24	882	0.21	3.68	2884	63	10.03
	45%	24	1033	0.25	4.64	3123	82	9.27
	50%	24	1168	0.29	5.73	3341	106	7.89
	55%	24	1322	0.33	6.89	3554	123	8.12
	60%	24	1483	0.36	8.18	3758	142	7.62
	65%	24	1642	0.40	9.70	3962	166	7.13
	70%	24	1799	0.44	11.16	4136	191	6.83
	75%	24	1965	0.48	12.72	4309	217	6.53
	80%	24	2132	0.57	14.43	4472	248	6.23
	85%	24	2243	0.56	16.23	4636	272	5.87
	90%	23	2398	0.61	18.25	4798	307	5.59
	95%	23	2583	0.65	20.32	4950	337	5.42
	100%	23	2787	0.71	23.34	5157	383	5.16
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (+10°)	10%	24	185	0.05	0.53	1257	7	14.44	63 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25℃)
	15%	24	269	0.08	0.86	1557	13	13.06
	20%	24	373	0.11	1.36	1858	21	11.48
	25%	24	467	0.14	1.87	2100	31	10.42
	30%	24	581	0.17	2.53	2341	42	9.59
	35%	24	721	0.19	3.15	2583	51	9.56
	40%	24	874	0.23	4.02	2808	68	9.10
	45%	24	1033	0.27	5.08	3040	86	8.51
	50%	24	1168	0.31	6.21	3258	106	7.89
	55%	24	1322	0.35	7.47	3458	127	7.43
	60%	24	1490	0.40	9.07	3669	154	6.92
	65%	24	1641	0.44	10.49	3842	177	6.60
	70%	24	1799	0.48	12.07	4010	202	6.30
	75%	24	1966	0.53	13.78	4178	232	6.04
	80%	24	2132	0.57	15.65	4332	259	5.78
	85%	24	2256	0.61	17.63	4481	286	5.44
	90%	23	2420	0.66	19.72	4633	320	5.23
	95%	23	2563	0.70	21.89	4767	349	5.00
	100%	23	2787	0.76	25.26	4965	395	4.73
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (-2.5°)	10%	24	80	0.02	0.30	1450	3	11.20	37 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25℃)
	15%	24	128	0.03	0.46	1805	6	11.51
	20%	24	186	0.04	0.67	2112	9	11.58
	25%	24	244	0.05	0.89	2404	13	11.44
	30%	24	314	0.07	1.19	2691	20	11.02
	35%	24	398	0.08	1.56	2982	25	10.64
	40%	24	490	0.10	1.99	3292	34	10.27
	45%	24	604	0.12	2.52	3578	45	10.01
	50%	24	718	0.14	3.17	3891	57	9.48
	55%	24	825	0.16	3.79	4155	70	9.12
	60%	24	935	0.18	4.49	4421	83	8.74
	65%	24	1044	0.20	5.23	4670	98	8.39
	70%	24	1149	0.22	5.99	4914	113	8.06
	75%	24	1268	0.24	6.85	5149	129	7.77
	80%	24	1373	0.26	7.70	5382	147	7.50
	85%	24	1490	0.28	8.67	5621	165	7.23
	90%	24	1617	0.30	9.69	5853	184	7.03
	95%	24	1737	0.32	10.80	6090	204	6.78
	100%	24	1904	0.35	12.37	6400	235	6.51
Note: Motor temperature is the bell temperature at 80% throttle. (Date above based on benchtest are for reference only, comparison with that of other motor types is not recommended.)

Analysis Chart

Packing List

Note

(1)Please make sure that screws of cover plates are mounted well.

(2)Do not add force onto the propellers,

(3)Fall-off or experience equivalent impact to propellers will lead to deformation or cracks. in this case,

you will need to replace them with good ones.

(4)NEVER decompose the propellers. Decomposition of which will result in safety issues. Do not use

the propellers in hostile environments containing H20,S02,N02,Cl2,organosilicon,cyanogroup and

phenol.

(5)Keep the propellers away from the mentioned environments in (4).

(6)For long time storage of over 6 months, please keep it in sealed preservation.

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