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14-031 is a state-of-the-art auxiliary gas turbine engine with the power up to 105 kW. This engine is designed for aircraft and helicopter APUs. ft is used for air turbine start of the main engines, supplying on-board AC electric power (200/115 V, up to 40 kVA) 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 is reduced.

    The noise level of the TA14-031 engine, when installed on the craft, does not exceed 87 dB.

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

APPLICATION: -31.

Technical features:

Absorbed electric power of AC, kVA

40

Bleed air consumption, kg/s

0,4

Bleed air pressure, kgf/sm2

3,20

Bleed air temperature, C

200

Start and operation altitude, m

4000/6000

Environmental temperature,

60

Weight (without generator), kg

65

Specified operating hours, hours/starts                    

3000/4500

Overall dimensions, mm

939483447

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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