By-pass Turbofan Engine Family Based on PS-12
PS-7
Thrust
Take off (N = 0; M = 0), kgf 7000
Maximum take off power, kgf 7700
Cruise
(N = 11 km; M = 0.8; ISA), kgf 1550.
Specific fuel consumption
at cruise, kg/kgf hr 0.620
Fan diameter, mm 1210
Dry weight, kg 1350
For long-range executive (business) aircraft of the TU-414 type and "Global express" (Bombardier)
Number of passengers 8...19
Flight range, km 8000...11000
Take-off weight, ton 40...45
and regional aircraft
Number of passengers 60-95;
Flight range, km 2500...4000
Take-off weight, ton 40...45
PS-9
Thrust
Take-off (N = 0; M = 0), kgf 9000
Maximum take-off power, kgf 10000
Cruise
(N = 11 km; M = 0.8; ISA), kgf 2100
Specific fuel consumption
at cruise, kg/kgf hr 0.590
Fan diameter, mm 1435
Dry weight, kg 1800
For short-haul aircraft of the TU-334 type
Number of passengers 100...110
Flight length, km 2000...2500
Take-off weight, ton 50...60
and multi-purpose amphibious airplane of the Be-200 type.
PS-14P
Thrust
Take off (N = 0; M = 0), kgf 14 500
Maximum take-off power, kgf 15 900
Cruise mode
(N = 11 km; M = 0.8; ISA), kgf 2750
Specific fuel consumption
at cruise, kg/kgf hr 0.530
Fan diameter, mm 2 050
Dry weight, kg 2600
For advanced modifications of medium-haul aircraft and transport aircraft of IL-76 family.
PS-18P
Thrust
Take off (N = 0; M = 0), kgf 18 000
Maximum take-off power, kgf 20 000
Cruise mode
(N = 11 km; M = 0.8; ISA), kgf 3 500
Specific fuel consumption
at cruise, kg/kgf hr 0.520
Fan diameter, mm 2 300
Dry weight, kg 3 200
For advanced modifications of medium-haul aircraft of Tu-204 family and long-haul aircraft of IL-96 family.
Contact
Aviadvigatel Open Joint Stock Co.
93, Komsomolsky prospect
GSP, 614990 Perm
Alexander N. Semenov
Deputy General Designer-
Chief Designer
Tel. +7 (342) 245-75-68
Fax +7 (342) 245-97-77
E-mail: semenov@avid.ru
