TEI-PD180ST
Turbodiesel Aviation Engine
TEI-PD180ST engine is developing to meet the power needs of MALE (Medium Altitude Long Endurance) class unmanned aerial vehicles.
TEI-PD180ST engine has a single stage turbocharging system, high altitude capability, low fuel consumption and a lightweight aluminum block design. With more power and less weight, it will go ahead of its competitors in the market and bring the capabilities of the platforms to a higher class.
TEI-PD180ST Technical Specifications
| Displacement | 2.1 L |
| Engine Configuration | Straight 4 Cylinder |
| Fuel Supply | Common Rail Diesel Injection |
| Air Induction | Single-Stage Turbocharging |
| Maximum Power | 182 HP (±2) |
| Maximum Continuous Power | 172 HP (±2) |
| Dry Weight | 158 kg |
| Engine Lifespan | 3600 hours |
| Engine Depot-Level Maintenance | 1200 hours |
| Engine Cooling | Water Cooled |
| Fuel Options | JP-8, JET-A1, JP-5, and EN 590 |
| BSFC (@MSL) | 220 g/kWh (±3) |
| Electrical Power | 9 kW (2x4.5 kW) |
| Altitude Power (@20,000 ft) | 170 HP |
| Altitude Power (@30,000 ft) | 115 HP |
| Altitude Power (@40,000 ft) | 75 HP |
| Critical Altitude | 17,000+ ft |
| Maximum Altitude | 45,000 ft |
| Aircraft Configuration | Tractor or Pusher Compatible |
| Engine Control | Redundant ECU (FADEC) |
| FADEC Software | DO-178C DAL-C Certifiable |
| Alternator Control | DO-178C DAL-C Certifiable |
