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T-MOTOR AUZ 19*10

The T-MOTOR AUZ 19*10 is a one-piece carbon-fiber propeller for electric fixed-wing UAVs. Measuring 19 inches in diameter with a 10-inch pitch, it combines a PMI sandwich core, matte finish and flange mounting interface. Average weight is 36 g per propeller.

T-MOTORDrone motor
Material
Resin-based carbon-fiber composite with PMI sandwich core

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Product overview

The T-MOTOR AUZ 19*10 is a one-piece straight propeller for electric fixed-wing UAVs, with a 19-inch diameter and 10-inch pitch. Its resin-based carbon-fiber composite structure incorporates a PMI sandwich core and a matte finish. Integrated prepreg compression molding produces a structure with porosity below 1%. Each propeller weighs an average of 36 g and uses a propeller-hub flange connection with an Ø8mm center hole.

The AUZ 19*10 has a recommended maximum speed of 7950 RPM and recommended maximum thrust of 12 kg, with limit values of 8850 RPM and 15 kg. Its operating temperature range extends from -30°C to 60°C. Recommended motor combinations include AT5220-A/B KV220 and KV380, AT5230-A/B KV200, AT5330-A/B KV220, and AT7215 variants in KV200, KV220, KV245 and KV270. Performance measurements at 22 °C and 25 m altitude are subject to some variation with test equipment, methods, environmental factors and testing standards.

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Specifications

T-MOTOR AUZ 19*10 specifications
SpecificationValue & conditions
Diameter19 inches (482.6mm)
MaterialResin-based carbon-fiber composite with PMI sandwich core
Pitch10 inches (254mm)
Surface finishMatte
Average weight36 gPer individual propeller.
TypeOne-piece straight propeller
Recommended maximum rotational speed7950 RPM
ApplicationFixed-wing UAVs
Recommended maximum thrust12 kg
Mounting interfacePropeller-hub flange connection; Ø8mm center hole
Limit rotational speed8850 RPM
Limit thrust15 kg
Recommended motorsAT5220-A/B KV220; AT5220-A/B KV380; AT5230-A/B KV200; AT5330-A/B KV220; AT7215 KV200; AT7215 KV220; AT7215 KV245; AT7215 KV270
Temperature range-30°C to 60°COperating temperature.
Manufacturing process and porosityIntegrated prepreg compression molding; product porosity below 1%
Performance by rotational speedSpeed (RPM) | Torque (N·m) | Thrust (gf) | Output power (W) | Thrust efficiency (gf/W) 3250 | 0.50 | 1790 | 170.89 | 10.48 3650 | 0.62 | 2289 | 237.95 | 9.62 4050 | 0.76 | 2858 | 323.56 | 8.83 4450 | 0.92 | 3496 | 430.23 | 8.13 4850 | 1.10 | 4203 | 560.47 | 7.50 5250 | 1.30 | 4980 | 716.79 | 6.95 5650 | 1.52 | 5826 | 901.69 | 6.46 6050 | 1.76 | 6741 | 1117.69 | 6.03 6450 | 2.02 | 7726 | 1367.29 | 5.65 6850 | 2.30 | 8780 | 1652.99 | 5.31 7250 | 2.60 | 9904 | 1977.32 | 5.01 7650 | 2.92 | 11097 | 2342.77 | 4.74 8050 | 3.26 | 12359 | 2751.86 | 4.49 8450 | 3.62 | 13691 | 3207.08 | 4.27 8850 | 4.00 | 15092 | 3710.96 | 4.07Ambient temperature 22 °C; altitude 25 m. Results are subject to some variation under different testing standards because of test equipment, methods and environmental factors.

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