|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|
|Total assigned life, h||100000|
low lube oil consumption;
reliable starting system;
low maintenance and repair costs throughout the entire life cycle;
full automation of processes;
easy to control and maintain;
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.
Mikhail F. Khairullin
Deputy General Designer – Chief Designer, IGTs for Gas Compressor Packages
Andrei L. Polyanin
Head of Lead Department