ISO conditions, fuel – natural gas | |
Output power at PT shaft, MW | 16.47 |
Efficiency at PT shaft, % | 37.0 |
Multiplying gearbox output shaft speed, rpm | 5300 |
Exhaust gas temperature, °C | 540 |
Exhaust gas flow, kg/ s | 60.28 |
MTBO, h | 25000 |
Total assigned life, h | 100000 |
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high efficiency;
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low lube oil consumption;
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high durability;
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reliable starting system;
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low maintenance and repair costs throughout the entire life cycle;
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full automation of processes;
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easy to control and maintain;
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factory preassembled enabling fast putting into service.
The GTU-16P gas turbine is built based on the gas generator of the PS-90A aero engine used in modern Russian passenger aircraft such as IL-96, Tu-204, Tu-214.
Gazprom, Yamalgazinvest, NOVATEK, etc. See the Page “Perm IGTs at the Customers’ Sites” for more detailed information.
Contact details
Maksim A. Snitko
Deputy General Designer – Chief Designer, IGTs for Gas Compressor Packages



Andrei L. Polyanin
Head of Lead Department


