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D-436-148 Turbofan engine

D-436-148 Turbofan engine © Konstantinos Panitsidis
Photo archive K. Panitsidi

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It is intended for installation in An-148 aircraft used by regional and short haul routs.

Main advantages D-436-148:
- low specific fuel consuption

- low levels noise
- low levels of emission
- ease of maintenance
- high performance system
- low long service life
- it has system FADEC (Fuell autohority digital engine control)
- service life up to 12.000 h. 

 

D-436-148 Turbofan engine © Konstantinos Panitsidis
Basic specifications D-436-148 Short-range aircraft Long-range aircraft
Operating mode Take off rating (PAMB=760 mm Hg, MFL=0) tAMB+37,5 oC Take off rating (PAMB=760 mm Hg, MFL=0) tAMB+30 oC
Thrust, kgf (N) 6.400 (62784) 6.830 (67002)
Specific fuel consumption, kg/kgf*h (kg/N*h) 0,374 (0.0381) 0,377 (0.0384)
Maximum cruse rating (Η=11.000 m, MFL=0,75, ISA+10oC)    
Thrust, kgf (N) 1.500 (14.715) 1.500 (14.715)
Specific fuel consumption, kg/kgf*h (kg/N*h) 0,618 (0,063) 0,618 (0,063)
Dry weight, not more than, kg 1.400 1.400

 



Technical specifications

DESIGNER Ivchenko - Progress ZMKB, UMPO και NPC Saljut
COUNTRY Russia, Ukraine
TYPE
is a triple-spool high-bypass turbofan engine
Installed On (aerial means)
An-148, Be-200, Tu-334
Fuel 
-
Oil -
Maximum thrust take-off power rating 6.570 kgf
Specific fuel consumption, take-off power rating 0.351 kg/kgf*h
Maximum thrust, cruise power(H=11.000 m, M=0,75) 1.560 kgf 
Specific fuel consumption, cruise power  0,60 kg/kgf*h
Pressure ratio, take-off power rating -
Bypass ratio -
Temperature of the gas at the turbine intake, take-off power rating -
Air flow rate, take-off power rating -
Compressor rotation frequency low-pressure, take-off power rating -
Compressor rotation frequency high-pressure, take-off power rating  -
OVERALL DIMENSIONS  
Diameter -
Height 1930 mm
Width 1784 mm
Length 4034 mm
WEIGHT  
Engine weight  1.400 kg 
Overhaul operation time -
Specified service life -
Shelf life of preserved engine -





Photos D-436-148 Turbofan engine