CATALOGUE
Catalogue_2016-2017 Catalogue_2016-2017
ENGINES AIRCRAFT ENGINEERING AND MAINTENANCE AI-25TLSH TUBRBOFAN AERO ENGINE Designed to power other existing trainers and combat trainers used as light attack aircraft. In this respect, a combat maximum power rating of enhanced thrust, employed for strike operations, has been additionally introduced and engine acceleration time has been substantially reduced. Dimensions: 3358х985х958 mm Weight, dry: 350 kg Main Specifications: Combat Training Maximum performance (SLS; ISA) thrust 1850 kgf 1720 kgf specific fuel consumption 0,58 kg/kgf•h Maximum cruise performance (Н=0 m; Мfl=0,6; ISA+15 o C) thrust 1250 kgf 1100 kgf Acceleration time 6 sec D-27 TURBOFAN AERO ENGINE D-27 Tubofan Aero Engine is designed for installation on An-70 highly efficient transport aircraft featuring improved takeoff and landing characteristics. It offers efficiency increased by 30% to aircraft. It meets the effective environmental requirements of ICAO standards. It is passing flight and state bench tests. Main Specifications: Take-off performance (SLS; ISA) power 14000 ehp specific fuel consumption 0,170 kg/ehp•h Maximum cruise performance (Н=11000 m; Мfl=0,7; ISA) power 6750 ehp specific fuel consumption 0,130 kg/ehp•h Dimensions: 4575х1570х1372 Propfan diameter: 4500 mm Weight, dry: 1650 kg 96
AIRCRAFT ENGINEERING AND MAINTENANCE ENGINES D-136, D-136 SERIES 1 TURBOSHAFT AERO ENGINE Designed to power the largest in the world Mi-26, Mi-26T transport helicopters. The most powerful turboshaft engine in the world has low specific fuel consumption and gravity of engine. It has undergone state bench tests and certification. The engine has Type Certificate. It meets the effective environmental requirements of ICAO standards. Dimensions: 3715x1382x1124 Weight, dry: 1077 kg Main Specifications: Take-off performance (SLS; ISA) power specific fuel consumption 11400 hp 0,194 kg/hp•h AI-450M GAS-TURBINE TURBOSHAFT AERO ENGINE Gas Turbine Turboshaft Aero Engine AI-450M is intended for upgraded Mi-2M helicopter and multipurpose helicopters МSB-2, Rusmas. Main Specifications: Take-off performance (SLS; ISA; Ointel=1,0) power specific fuel consumption Maximum cruise performance (SLS; ISA; Ointel=1,0) power specific fuel consumption 400 hp 0,280 kg/hp•h 285 hp 0,320 kg/hp•h Dimensions: 1047х538х684 Weight, dry: 115 kg 97
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AIRCRAFT ENGINEERING AND MAINTENANCE<br />
ENGINES<br />
D-136, D-136 SERIES 1<br />
TURBOSHAFT AERO ENGINE<br />
Designed to power the largest in the world<br />
Mi-26, Mi-26T transport helicopters. The<br />
most powerful turboshaft engine in the<br />
world has low specific fuel consumption<br />
and gravity of engine. It has undergone<br />
state bench tests and certification. The<br />
engine has Type Certificate. It meets the<br />
effective environmental requirements of<br />
ICAO standards.<br />
Dimensions:<br />
3715x1382x1124<br />
Weight, dry:<br />
1077 kg<br />
Main Specifications:<br />
Take-off performance (SLS; ISA)<br />
power<br />
specific fuel consumption<br />
11400 hp<br />
0,194 kg/hp•h<br />
AI-450M<br />
GAS-TURBINE TURBOSHAFT AERO ENGINE<br />
Gas Turbine Turboshaft Aero Engine<br />
AI-450M is intended for upgraded<br />
Mi-2M helicopter and multipurpose<br />
helicopters МSB-2, Rusmas.<br />
Main Specifications:<br />
Take-off performance (SLS; ISA; Ointel=1,0)<br />
power<br />
specific fuel consumption<br />
Maximum cruise performance (SLS; ISA; Ointel=1,0)<br />
power<br />
specific fuel consumption<br />
400 hp<br />
0,280 kg/hp•h<br />
285 hp<br />
0,320 kg/hp•h<br />
Dimensions:<br />
1047х538х684<br />
Weight, dry:<br />
115 kg<br />
97
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