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TA18-200 engine is a modern auxiliary gas turbine having equivalent power up to 365 kW. The engine is intended for use in aircraft and helicopter APUs. It is used for starting the main ( in flight) engines, supplying on-board electric power (115/200V, with power up to 60 kVA) and providing for cockpit and cabins air conditioning.

Optimization of auxiliary compressor, turbo compressor (centrifugal compressor and centripetal turbine), combustion chamber, gearbox and mountain units has allowed us to achieve fuel saving for 30% and considerable, (up to 2 times), reduction of engine mass comparison with the earlier primary models.

TA18-200 complies with the modern technical requirements and is equipped with full-authority electronic-digital control system providing regulation, control, check and error detection and operation time count. Modular structure allows to fulfil diagnostics and repair of the engine.

APPLICATION: Tu-204, Tu-214, Tu-330, An-70.

 

Technical features:

Absorbed electric power of AC, kVA

60

Bleed air consumption, kg/s

1,7

Bleed air pressure, kgf/sm2

4,7

Bleed air temperature, C

220

Start and operation altitude, m

9000

Environmental temperature,

60

Weight (without generator), kg

190

Primary number of operating hours/starts

2000/4000

Specified number of operating hours/starts

12000/15000

Overall dimensions, mm

1376 750 770

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Address: 6, Zhdanov Str., Stupino,
Moscow region, Russian Federation, 142800,
Tel.: (496) 642-33-30 Fax: (496) 642-04-24
Email: vint@aerosila.ru