Product overview
The T-MOTOR AUZ 17*10 is a propeller for electric fixed-wing UAV propulsion. Its 17-inch (432.0mm) diameter and 10-inch (254mm) pitch are combined in a one-piece straight structure with a matte finish. Construction uses resin-based carbon-fiber composite and a PMI foam core, with an average single-blade weight of 28 g. Prepreg molding and a layup tailored to fixed-wing flight provide the structural approach, with fiber orientation supporting bending and torsion resistance. Product porosity is below 1%.
The propeller integrates through a flange mount with an Ø8mm center hole; its mounting holes must match the motor. Recommended motor choices are AT4130 KV230, AT4130 KV300 and AT4130 KV450, with intended aircraft layouts encompassing conventional fixed-wing designs, flying wings and VTOL UAVs. Recommended maxima are 8200 RPM and 8 kg thrust, while the separate limits are 9150 RPM and 10 kg. Operating temperature spans -30°C to 60°C. Performance figures use 22°C ambient temperature and 25 m altitude; results can vary with testing equipment, methodology and environment.
Specifications
| Specification | Value & conditions |
|---|---|
| Product | T-MOTOR AUZ 17*10 fixed-wing UAV propeller |
| Diameter | 17 inches (432.0mm) |
| Pitch | 10 inches (254mm) |
| Material | Resin-based carbon-fiber composite + PMI foam core |
| Surface treatment | Matte |
| Average single-blade weight | 28 g |
| Propeller architecture | One-piece straight propeller |
| Application | Fixed-wing UAV propulsion |
| Recommended maximum rotational speed | 8200 RPM |
| Recommended maximum thrust | 8 kg |
| Mounting interface | Flange mount; Ø8mm center hole |
| Limit rotational speed | 9150 RPM |
| Limit thrust | 10 kg |
| Recommended motors | AT4130 KV230 / AT4130 KV300 / AT4130 KV450 |
| Operating temperature range | -30°C minimum; 60°C maximum |
| Structural manufacturing process | Prepreg with PMI core and molded one-piece forming |
| Product porosity | Below 1% |
| Intended integration layouts | Conventional fixed-wing, flying-wing and VTOL UAV layouts |
| Integration requirement | Match propeller mounting holes to the motor.Motor mounting-hole compatibility must be ensured. |
| Performance data | RPM | Torque (N·m) | Thrust (gf) | Output power (W) | Efficiency (gf/W) 3550 | 0.34 | 1385 | 127.09 | 10.90 3950 | 0.42 | 1743 | 174.01 | 10.02 4350 | 0.51 | 2141 | 232.47 | 9.21 4750 | 0.61 | 2580 | 303.82 | 8.49 5150 | 0.72 | 3059 | 389.43 | 7.85 5550 | 0.84 | 3578 | 490.66 | 7.29 5950 | 0.98 | 4137 | 608.87 | 6.80 6350 | 1.12 | 4737 | 745.42 | 6.36 6750 | 1.28 | 5378 | 901.67 | 5.96 7150 | 1.44 | 6058 | 1078.98 | 5.61 7550 | 1.62 | 6779 | 1278.71 | 5.30 7950 | 1.80 | 7540 | 1502.22 | 5.02 8350 | 2.00 | 8342 | 1750.88 | 4.76 8750 | 2.21 | 9184 | 2026.04 | 4.53 9150 | 2.43 | 10066 | 2329.07 | 4.32Ambient temperature: 22℃; altitude: 25m. Data may vary under different testing standards due to equipment, methodology and environment. |
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