发明名称 PROCEDE DE CONTROLE DE LA GENERATION ELECTRIQUE APPLIQUEE A UNE TURBINE A GAZ D'AERONEF ET TURBOMOTEUR METTANT EN OEUVRE UN TEL PROCEDE
摘要 <p>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.</p>
申请公布号 FR2968716(B1) 申请公布日期 2012.12.28
申请号 FR20100060419 申请日期 2010.12.13
申请人 TURBOMECA 发明人 LANGFORD STEPHEN;HARRIET PIERRE
分类号 F02C6/00;B64D31/00;H02J3/28;H02J3/38 主分类号 F02C6/00
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