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TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
Specifications
Model Number :
GTP 800，GTP 1600
Place of Origin :
China
MOQ :
2
Price :
USD： 410，000-USD-860,000
Payment Terms :
T/T
Supply Ability :
200
Delivery Time :
180days
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
Description
TurboProp Engine
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
GTP800 and GTP1600 are constant-speed variable-pitch turboprop engines, consisting of an engine and a matching propeller. The GTP800 adopts a front-output layout, while the GTP1600 adopts a rear-output layout. The engine is primarily composed of centrifugal compressor, reverse-flow annular combustor, gas turbine, free power turbine, reduction gearbox, propeller, control system, fuel system, and lubrication system. All of these components are controlled by an integrated propeller and fully authority digital control system.
Product Advantages
GTP 800
  • 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
GTP 1600
  • 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
Application Scenarios
Applied to general aviation aircraft such as small manned aircraft, agricultural planes, cargo planes and other aviation applications.
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TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation

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Product Detail
Model Number :
GTP 800，GTP 1600
Place of Origin :
China
MOQ :
2
Price :
USD： 410，000-USD-860,000
Payment Terms :
T/T
Supply Ability :
200
Contact Supplier
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation
TurboProp Engine with 600-kw to 1300kw Output Shaft Power, Low Fuel Consumption, and Compact Structure for General Aviation

Jumeirah Industry Co.，Limited

Verified Supplier
1 Years
Since 2020
Business Type :
Manufacturer, Distributor/Wholesaler, Other
Main Products :
Drone & UAV, Turbine Engine Electricity Generation, Aircraft Turbine Engine
Employee Number :
>50-100
Certification Level :
Verified Supplier
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