FIELD: machine engineering.
SUBSTANCE: gas-compressor unit contains an air path, which in turn contains an air intake, a compressor, a combustion chamber, a gas turbine, a shaft connecting the compressor and the gas turbine, a free turbine connected to the gas compressor and a fuel gas supply system to the combustion chamber with the fuel line. The fuel gas supply system comprises a water electrolyser and a hydrogen and oxygen mixer with a fuel gas installed in front of the combustion chamber.
EFFECT: increasing performance of a gas turbine engine used as a drive for a gas-compressor unit on natural gas by increasing the completeness of fuel combustion in a gas turbine engine, improving its specific characteristics and reducing emissions of harmful substances.
18 cl, 24 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS COMPRESSOR UNIT | 2015 |
|
RU2610631C1 |
| GAS PUMPING UNIT | 2021 |
|
RU2773995C1 |
| GAS PUMPING UNIT | 2021 |
|
RU2773994C1 |
| GAS PUMPING UNIT | 2022 |
|
RU2785168C1 |
| GAS PUMPING UNIT | 2020 |
|
RU2764940C1 |
| GAS PUMPING UNIT | 2020 |
|
RU2758172C1 |
| GAS TRANSFER UNIT | 2020 |
|
RU2735881C1 |
| GAS TRANSFER UNIT | 2020 |
|
RU2735040C1 |
| PROCESS FOR INCREASING GAS TURBINE ENGINE EFFICIENCY AND GAS TURBINE ENGINE | 2014 |
|
RU2572258C2 |
| ENGINE OF HYPERSONIC AIRCRAFT | 2015 |
|
RU2591361C1 |
