发明名称 DEVICE AND A METHOD FOR REGULATING A TURBINE ENGINE, AND AN AIRCRAFT
摘要 A regulator device (10) for reducing the risk of surging in a turbine engine (3) that includes a gas generator (4), air extraction means (8), and mechanical power take-off means (100). An engine computer (11) includes storage means (16) that store a plurality of acceleration regulation relationships, each acceleration regulation relationship corresponding to air extraction in a first range, and to mechanical power take-off in a second range, said regulator device (10) including first measurement means (20) for measuring current air extraction, and second measurement means (30) for measuring current mechanical power take-off, said engine computer (11) controlling acceleration of the engine (3) by implementing the acceleration regulation relationship corresponding to the current air extraction and to the current mechanical power take-off.
申请公布号 US2013199197(A1) 申请公布日期 2013.08.08
申请号 US201313751266 申请日期 2013.01.28
申请人 EUROCOPTER;EUROCOPTER 发明人 BEAUD SOUTHDARY;MARTIN LAURENT
分类号 F02C9/00 主分类号 F02C9/00
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