GAS TURBINE FUEL SYSTEM

The invention provides a gas turbine fuel system. In a one embodiment, a gas turbine system includes a first pump that supplies distillate fuel to a combustor; a second pump that supplies fuel oil tothe combustor; a fuel selection unit that controls a first flow of distillate fuel and a second flow of fuel oil to the combustor; and a controller that receives feedback from a sensor and in responseto the feedback from the sensor controls the fuel selection unit to start the gas turbine system on the fuel oil. 本发明题为"气体涡轮燃料系统"。在一个实施方案中，本公开提供了一种气体涡轮系统，该气体涡轮系统包括：第一泵，该第一泵向燃烧器供应馏分燃料；第二泵，该第二泵向该燃烧器供应燃料油；燃料选择单元，该燃料选择单元控制到该燃烧器的第一馏分燃料流和第二燃料油流；控制器，该控制器从传感器接收反馈，并且响应于来自该传感器的该反馈而控制该燃料选择单元以依靠该燃料油开启该气体涡轮系统。