发明名称 Method for regulating the flow rate of fuel to a turboshaft engine in acceleration or in deceleration
摘要 Apparatus for regulating the flow rate of fuel to a turboshaft engine in acceleration or deceleration, the engine having a free turbine and a core engine, the apparatus including sensors transmitting information to regulator elements, the information relating: to a first speed of rotation NTL of the free turbine; to a second speed of rotation Ng of the engine's gas generator; to an internal temperature T4 of the gas at the inlet to the free turbine; to the external pressure; and to the external temperature. The apparatus further includes control elements activated by the regulator to actuate a fuel metering system of the engine. The regulator evaluates the flow rate of fuel to be supplied to the engine in acceleration or deceleration on the basis of at least one optimum regulation relationship, which determines a main modulated flow rate as a function of a modulated speed of rotation.
申请公布号 US7530232(B2) 申请公布日期 2009.05.12
申请号 US20050115277 申请日期 2005.04.27
申请人 EUROCOPTER 发明人 CERTAIN BERNARD
分类号 F02C9/28 主分类号 F02C9/28
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