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Engines for commercial and transport aircraft TVD-1500B

Development: NPO Saturn JSC
Production: NPO Saturn JSC

TVD-1500B – turboprop engine for general aviation aircraft.

Design features
• 4 stages mixed-flow compressor with variable stator vanes
• reverse-flow combustion chamber
• 2 stages high pressure turbine
• 2 stages power turbine
• FADEC with redundant hydromechanical channel

TVD-1500B turboprop engine is based on NPO Saturn’s RD-600V turboshaft engine HP core.

Application
Engine is designed for general aviation aircraft with seating capacity up to 30 passengers.



Advantages
• modular design and FADEC system provide high operating performances, maintainability, operation on technical condition
• capability of operation on unpaved airfields

Specification
EngineTVD-1500B
Power output at APR*, shp -
Take-off power output, shp 1 300
Specific fuel consumption at take-off, kg/(shp∙hr) 0.212
Specific fuel consumption at cruise, kg/(shp∙hr)** 0.225
Output shaft speed, rpm 1 700
Dimensions (L x D), m 1.950 x 0.760
* – automatic power reserve
** – (H=3 000 m; M=0.3; МСА)

Contacts (sales)
Contacts (after sales support)


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