| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide a gas turbine engine system (10) including at least one combustor (14) and a fuel control system (288). <P>SOLUTION: The present gas turbine engine system (10) includes a gas turbine engine comprising at least one combustor (14) made up so as to receive fuel flow from a flow controller and a fuel control system (288). The fuel control system (288) includes a piping system made up so as to feed fuel flow from a fuel supply source to the flow controller, a sensor made up so as to generate a signal indicating fuel flow property variable with elapse of time, and a controller comprising a processor programmed so as to receive the generated signal and repeatedly follows up the progress of a plurality of discrete volumes flowing through the piping system by using the piping system and a flowing model of the received signal and then control the fuel flow by using the flow controller. <P>COPYRIGHT: (C)2010,JPO&INPIT</p> |
