TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
Product Details
| Output Shaft Power: | 600-kw---1300kw | Overall Pressure Ratio: | 8.8--13.5 (kg/kW·h) |
|---|---|---|---|
| Specific Fuel Consumption: | ≥ 0.35---≥ 0.29 | Output Shaft Speed: | 2000 Rpm |
| Weight: | 185(Engine Core)+60(Propeller)kg----293kg | Engine Core Weight: | 185 Kg |
| Propeller Weight: | 60 Kg | Total Weight: | 293 Kg |
Product Description
- High design pressure ratio, low fuel consumption
- Adoption of a single-stage high-pressure ratio centrifugal compressor with high distortion tolerance and a wide operating range
- Adoption of a front output layout, compact structure
- High design pressure ratio, low fuel consumption
- Adoption of a two-stage centrifugal compressor with high distortion tolerance and wide operating range
- Adoption of moderate cycle parameters, reducing component costs and improving the reliability of hot section components, with good economic and cost advantages
- Adoption of a rear output layout, simple structure, and high mechanical efficiency
Product Highlights
GTP800 & GTP1600 turboprop engines (600-1300kW) deliver high pressure ratios (8.8-13.5) with low fuel consumption (≥0.29 kg/kW·h). Features include centrifugal compressors, digital control systems, and compact front/rear output layouts for superior efficiency and reliability.
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