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D-27 Propfan engine

D-27 Propfan engine © Konstantinos Panitsidis
Photo archive K. Panitsidi

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This engine is mainly intended for the Antonov, An-70, An-70T, An-180 and Beriev Be-42 aircraft, but also for aircraft with a low fuel consumption requirement, such as passenger aircraft.

The Progress D-27 Propfan turboprop engine has a contra-rotating propellers, SV-27 type variable pitch propellers of Russian origin and made entirely of composite materialы with a diameter of 4,5 meters.

Its front row is equipped with eight propellers and the rear row has six. All this combination yields a maximum power of 14.000 horsepower (each engine). In addition to these, the engine has the lowest fuel consumption (130 grams for every ton of cargo per kilometer). 

 

D-27 Propfan engine, SV-27 propeller © Konstantinos Panitsidis
Diameter of contra-rotating propellers 4.500 mm. Rotational frequency take-off condition 1.000 RPM. Weight 1.100 kg. Takeoff power 13.400 h.p. Thrust (Vfl=0) 12.150 kgf. 

 

The design parameters (characteristics) of the D-27 have:- 
- parameter stability ( very low fuel consumption in all operating phases high reliability)
- reliability
- long service life
- low labor intensity of manufacturing and maintenance
- low emission of pollutants
- permissible noise level
 

 

D-27 Propfan engine, SV-27 propeller © Konstantinos Panitsidis





Technical specifications

DESIGNER Ivchenko - Progress ZMKB, NPC Saljut
COUNTRY Russia, Ukraine
TYPE
Propfan engine
Installed On (aerial means)
An-70, An-180, A-42
Fuel  RT brand aviation kerosene
Oil -
Propeller shaft power, take-off power rating 14.000 e.h.p
Specific fuel consumption, take-off power rating  0,170 kg/e.h.p.*h
Propeller shaft power, cruise power  6.340 e.h.p
Specific fuel consumption, cruise power (H=11.000 m, M=0,7) 0,130 kg/e.h.p.*h
Pressure ratio, take-take-off power rating 22,9
Pressure ratio, cruise power 29,7
Temperature of the gas at the turbine intake, take-off power rating 1.640 K
Temperature of the gas at the turbine intake, cruise power 1.450 K
Air flow rate, take-off power rating 27,7 kg/s
Air flow rate, cruise power 24,4 kg/s
Air flow rate, cruise power  maximum 12,1 kg/s
Compressor rotation frequency low-pressure, take-off power rating -
The rotational speed of the propfan turbine take-off mode 8.934 rpm
Power-weight ratio 8,485 h.p/kgf
Energy conversion efficiency (Mf=0) 0,9
OVERALL DIMENSIONS  
Diameter propellers 4500 mm
Length 4198 mm
Width 1260 mm
Diameter engine 1370 mm
WEIGHT  
Weight (without the non-rotating propellers, high distortion) 1.650 kg
Specified service life 18.000 h
Overhaul operation time 6.000 h





Photos D-27 Propfan engine