| 摘要 |
A gas turbine engine (100) configured to operate using a liquid fuel and a gaseous fuel may include a combustor system (20) fluidly coupled to a compressor system (10) and a turbine system (70). The gas turbine engine may also include a control system (60) configured to selectively direct the gaseous fuel and the liquid fuel to the combustor system based on a concentration of a constituent in the gaseous fuel. |
