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TA18-100 engine is a modern gas-turbine having equivalent power up to 256 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 (115/220 V, with power up to 60 kVA) and supporting cockpit and cabin air conditioning.

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

TA18-100 complies with the market requirements and is equipped with full-authority electronic-digital control system regulation control that provided error detection and operation time.

Modular structure allows to fulfil diagnostics and repair of the engine.

 

The engine complies with the requirement of the Aviation Rules (section Auxiliary Engines) and has a type certificate ST 211-VD issued by the Aviation Register of the Interstate Aviation Committee (10.12.2002).

APPLICATION: Tu-334, Be-200, Yak-42, Tu-134, An-74TK-300.

Technical features:

Absorbed electric power of AC, kVA

60

Bleed air consumption, kg/s

1,27

Bleed air pressure, kgf/sm2

4,52

Bleed air temperature, C

210

Start and operation altitude, m

9000

Environmental temperature,

60

Weight (without generator), kg

152

Primary number of operating hours/starts

2000/4000

Specified number of operating hours/starts

12000/15000

Overall dimensions, mm

1076684675

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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