
Integrated Power Plant SaM146-1S17 for Enhanced Regional Aircraft Performance
Manufacturer:PJSC "ODK-SATURN"
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FOB, CIF & EXW terms available
Available Models
Description
SaM146 is an integrated propulsion system (including turbofan engine, nacelle with thrust reverser, attachments) for a new generation of regional and long-haul aircraft with 60-120 passenger capacity.
Design Features:
- fan with wide-chord blades
- 3-stage low-pressure compressor
- 6-stage high-pressure compressor
- annular combustion chamber
- 1-stage high-pressure turbine
- 3-stage low-pressure turbine
Benefits:
Compact, reliable and environmentally friendly engine based on a combination of experience and new technologies of domestic and western engine building:
- wide thrust control range
- high reliability (at the level of CFM56 standard)
- compliance with ICAO environmental requirements
- full interchangeability in the aircraft family
- low cost of ownership
Design Features:
- fan with wide-chord blades
- 3-stage low-pressure compressor
- 6-stage high-pressure compressor
- annular combustion chamber
- 1-stage high-pressure turbine
- 3-stage low-pressure turbine
Benefits:
Compact, reliable and environmentally friendly engine based on a combination of experience and new technologies of domestic and western engine building:
- wide thrust control range
- high reliability (at the level of CFM56 standard)
- compliance with ICAO environmental requirements
- full interchangeability in the aircraft family
- low cost of ownership
Specifications
Degree of dual circuit
4.43
Diameter, m
1.22 m
Length (with mixer), m
3.59 m
Specific fuel consumption at cruising mode, kg/(kgf/hour)
0.63
Thrust at takeoff mode, kgf
7120
Thrust in emergency mode, kgf
7836
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