
Parameter | Existing facilities | Upgraded facilities |
---|---|---|
Mass flow rate | 0.35 kg/s | 10 kg/s |
Pressure | 15 bar | 50 bar |
Temperature | 150 oC | 800 oC |
Max. labyrinth seal diameter | 300 mm | 600 mm |

INFRASEAL
* This temperature can be reached after the air line will be equipped with a combustor chamber which can be fuelled either by natural gas, or by liquid fuel, able to raise the working fluid temperature up to 800 oC. The combustor chamber is not including in this project.
