发明名称 航空機ガスタービンに使用される発電制御方法および該方法を実施する装置
摘要 A method improving acceleration efficiency of a gas generator of a gas turbine by reducing take-up of electric power, during transition phases, to conserve a sufficiently large surge margin for an operating line. The method increases acceleration/deceleration power of the gas generator by adjusting voltage of an electric network onboard the aircraft. After a phase of starting the gas turbine, voltage of the onboard network is adjusted by a voltage set value controlled by determining unballasting/ballasting status of a main electricity generation source of the onboard network. The status-determining is executed according to demand for taking power to be supplied for propulsion of the aircraft. The status-determining is followed by selecting a voltage set value from plural levels according to the determining the unballasting/ballasting status, and applying the selected set value to a control loop of the voltage supplied to the onboard network.
申请公布号 JP5923515(B2) 申请公布日期 2016.05.24
申请号 JP20130542595 申请日期 2011.12.12
申请人 ターボメカTURBOMECA 发明人 ランフオール,ステフアン;アリエ,ピエール
分类号 F02C3/10;B64D41/00;F02C6/00;F02C7/00;F02C7/36;F02C9/00 主分类号 F02C3/10
代理机构 代理人
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