|ISO conditions, fuel – natural gas|
|Output power at PT shaft, MW||10.26|
|Efficiency at PT shaft, %||32.5|
|Multiplying gearbox output shaft speed, rpm||9000|
|Exhaust gas temperature, °C||463|
|Exhaust gas flow, kg/ s||43.9|
|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-10P 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.
The GTU-10P features a high speed power turbine which provides for a highly efficient operation of the gas compressor.
Gazprom, Lukoil, Rosneft, Nortgaz, 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