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TA14-130-35 is a state-of-the-art gas-turbine engine with the power up to 105 kW. This engine is designed for SU-35 aircraft APU. It is used for supplying on-board AC electric power 200/115 V, up to 30 kV and providing air conditioning for cockpit and cabin.

The engine is equipped with a highly efficient turbo compressor and integrated system of oil cooling. As a result, fuel consumption and the weight are reduced.

The engine is compliant with the contemporary engineering requirements and is equipped with a full-authority electronic digital control system that provides regulation, control and error detection as well as operating time count.

APPLICATION: Su-35.

Technical features:

Absorbed electric power of AC, kVA

30

Bleed air consumption, kg/s

0,55

Bleed air pressure, kgf/sm2

3,70

Bleed air temperature, C

210

Start and operation altitude, m

10000

Environmental temperature,

60

Weight (without generator), kg

62

Overall dimensions, mm

868481426

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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