| 摘要 |
Liquid fuel assist ignition system (1) for providing a fuel -air mixture to a gas turbine in its start-up phase, comprising a high pressure tank (2), a vacuum pump (3) connected to the high pressure tank (2), a liquid fuel inlet (4) connected to the high pressure tank (2), an air inlet (5) connected to the high pressure tank (2) and an outlet (6) of the high pressure tank (2) connected to a burner of the gas turbine (20), and method to provide a fuel/air mixture to a gas turbine (20) in its start-up phase using a liquid fuel assist ignition system (1). |
