CATALOGUE
Catalogue_2016-2017 Catalogue_2016-2017
ENGINES AIRCRAFT ENGINEERING AND MAINTENANCE AI-9V, AI-9V SER. 1 AUXILIARY TURBINE ENGINE AI-9V, AI-9V SER. 1 used as power source effecting supply of compressed air to starting system of helicopter engines and electric power supply to helicopter electric power system when checking helicopter electrical and radio equipment. Installed on Мi-8 (Mi-8АМТ, Mi-8МТV, Mi-17, Mi-171, Мi-172), Мi- 24 (Mi-35), Мi-28 helicopters. t Bled air temperature: 160 °С Weight, dry: 57 kg Main Specifications: Engine AI-9V AI-9V ser. 1 Bled air consumption 0,4 kg/s Bled air total pressure not less than 2,9 kgf/cm 2 not less than 3,1 kgf/cm 2 Electric power takeoff in generator operating mode 3 kW 4,5 kW AI9-3B AUXILIARY TURBINE ENGINE AI9-3B used for starting aircraft propulsive engines and conditioning cockpits and cabins, and also for powering airborne electric equipment. Main Specifications: Aircraft electric system DC power 16 kV•A Bled air consumption 0,4 kg/s Bled air total pressure not less than 4,0 kgf/cm 2 Fuel consumption 92 kg/h Bled air temperature: 260 °С Weight, dry: 128 kg t 98
AIRCRAFT ENGINEERING AND MAINTENANCE ENGINES ТV3-117 (-КМ, -М, -МТ) SERIES 3 TURBOSHAFT ENGINES The engines are intended for the following helicopters: ТV3-117 ser.3 – for Мi-24, Мi-25, Мi-35; ТV3-117 КМ ser.3 – for Ка-27, Ка-29; ТV3-117 М ser.3 – for Мi-14; ТV3-117 МТ ser. 3 – for Мi-8МТ, Мi-17. Power: 2225 hp Weight, dry: 285 kg Main Specifications: Take-off performance (SLS; ISA) specific fuel consumption 0,230 kg/hp•h Main Specifications: 2.5- minute power rating, with one engine inoperative (OEI) (SLS, ISA): power 1765 kW 30- minute power rating, with one engine inoperative (OEI) (SLS, ISA): Power 1618 kW Specific fuel consumption 0.286 kg/kW•h Cruise power condition (SLS, ISA): Power 1103 kW Weight dry 294 kg TV3-117VMA TURBOSHAFT ENGINE The TV3-117VMA turboshaft engine is used to power in various-purpose helicopters. The TV3-117VMA turboshaft is one of the world`s best engines as regards its fuel efficiency and weight performances. High-tech development and perfect mass-production process have ensured the engine`s superior reliability and extensive service life. Main advantages of the engine: low specific fuel consumption; low weight-to-power ratio; high reliability; high reliability; long service life; high maintainability; high repairability; steady operation in harsh dust and smoke conditions; possibility of long-time operation in maritime conditions. 99
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ENGINES<br />
AIRCRAFT ENGINEERING AND MAINTENANCE<br />
AI-9V, AI-9V SER. 1<br />
AUXILIARY TURBINE ENGINE<br />
AI-9V, AI-9V SER. 1 used as power<br />
source effecting supply of compressed<br />
air to starting system of helicopter<br />
engines and electric power supply to<br />
helicopter electric power system when<br />
checking helicopter electrical and radio<br />
equipment. Installed on Мi-8 (Mi-8АМТ,<br />
Mi-8МТV, Mi-17, Mi-171, Мi-172), Мi-<br />
24 (Mi-35), Мi-28 helicopters.<br />
t<br />
Bled air temperature:<br />
160 °С<br />
Weight, dry:<br />
57 kg<br />
Main Specifications:<br />
Engine AI-9V AI-9V ser. 1<br />
Bled air consumption<br />
0,4 kg/s<br />
Bled air total pressure not less than 2,9 kgf/cm 2 not less than 3,1 kgf/cm 2<br />
Electric power takeoff in<br />
generator operating mode<br />
3 kW 4,5 kW<br />
AI9-3B<br />
AUXILIARY TURBINE ENGINE<br />
AI9-3B used for starting aircraft<br />
propulsive engines and conditioning<br />
cockpits and cabins, and also for<br />
powering airborne electric equipment.<br />
Main Specifications:<br />
Aircraft electric system DC power<br />
16 kV•A<br />
Bled air consumption<br />
0,4 kg/s<br />
Bled air total pressure not less than 4,0 kgf/cm 2<br />
Fuel consumption<br />
92 kg/h<br />
Bled air temperature:<br />
260 °С<br />
Weight, dry:<br />
128 kg<br />
t<br />
98
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