| 摘要 |
<p>Disclosed is an electronic control device (60) which is applied to a gas turbine (1) provided with a cylindrical combustor (40) to which air compressed by compressors (20, 30) is supplied, a plurality of fuel injection valves (41) which are circumferentially arranged on the combustor (40) so that fuel can be injected to the interior of the combustor (40), and an ignition plug (47) provided so as to ignite a fuel mixture within the combustor (40), wherein, when the gas turbine (1) is started, the operation of each fuel injection valve (41) is controlled so that the fuel injection starting time of the #6 and #12 fuel injection valves (41) that are far from the ignition plug (47) is followed by the fuel injection starting time of the #1 and #7 fuel injection valves (41) that are near the ignition plug (47).</p> |
