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TA12-60 is a single-shaft auxiliary gas-turbine engine with the equivalent power of 360 kWt. This engine is designed for aircraft and helicopter APUs. It is used for air turbine start of the helicopter and aircraft mid-flight engines, AC electric power of 115/200 V, power up to 60 kWA and providing air conditioning for cockpit and cabins.

High overall efficiency of the engine is based on the use of a 4-stage axial compressor. An annular reverse-flow combustion chamber of evaporative type provides 0,99 burning and low content of hydrocarbons in the exhaust gases. The engine contains a 3-stage axial turbine. Driving units, including alternator, are installed on the engine's gearbox.

The noise level of the TA12-60 engine, when installed on the craft, does not exceed 90 dB.

The engine complies with the Norms of Aircraft Airworthiness (NLGS-3); this is confirmed by a type certificate No 101-VD issued by the Aviation Register of the IAC.

 

Since 2005 the TA 12-60 APU has been operated under the second strategy. The TA 12-60 APU is operated subject to the technical condition till the specified life time of the principle components is terminated (4,000 hr/starts).

 

The TA12-60 engine has been in serial production since 1996.

 

APPLICATION: Tu-204, Tu-214, Tu-334, Be-200, An-70, Yak-42.

Technical features:

Absorbed electric power of AC, kVA

60

Bleed air consumption, kgf

1,6

Bleed air pressure, kgf/sm2

4,9

Bleed air temperature,

250

Start and operation altitude, m

7000/9000

Environmental temperature,

60

Weight (without generator), kg

297

Specified number of operating hours/starts

2000/4000

Overall dimensions, mm

1588682718

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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