Turbine Electric Engine with Hybrid Propulsion System - High Efficiency, Low Operating Costs, and STOL Capability

Hybrid turbine electric engine (300-1000 kW) with high efficiency, 1000km range, low operating costs, and STOL capability. Ideal for CTOL/STOL/VTOL applications with superior safety and lifecycle savings.

TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation

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.

3-Ton Thrust Medium Bypass Ratio Dual-Spool Turbofan Engine for Business Jets

3-ton thrust turbofan engine with 21 pressure ratio & 0.42 SFC. Features combined compressor, FADEC system, and medium bypass ratio for optimal thrust-efficiency balance. Ideal for business jets and special-mission aircraft.