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Method of automatically regulating aircraft power plant gas generator and free turbine speeds as a function of heating, electricity generation, noise emission, and fuel consumption

机译:根据供暖,发电,噪声排放和燃料消耗自动调节飞机电厂气体发生器和自由涡轮机转速的方法

摘要

The present invention relates to an automatic method of regulating a power plant (3′) of an aircraft (1), the power plant having at least one turbine engine (3), each engine (3) being capable of operating in an idling mode of operation. A calculation system (15) executes stored instructions in order to implement the idling mode of operation as a function of operational and ordered conditions either via a first regulation mode by regulating a first speed of rotation (Ng) of said gas generator (4), or via a second mode of regulation by regulating a second speed of rotation (NTL) of said free turbine (7).
机译:自动调节飞机( 1 )的动力装置( 3 ')的方法技术领域本发明涉及一种调节飞机( 1 )的动力装置( 3 ')的自动方法,该动力装置具有至少一个涡轮发动机( 3 ),每个引擎( 3 )都可以以空转模式运行。计算系统( 15 )执行存储的指令,以便通过第一调节模式,通过调节发动机的第一旋转速度(Ng)来实现根据操作和有序条件的空转操作模式。气体发生器( 4 ),或通过调节自由涡轮( 7 )的第二旋转速度(NTL)的第二种调节方式。

著录项

  • 公开/公告号US9476360B2

    专利类型

  • 公开/公告日2016-10-25

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号US201313753690

  • 发明设计人 ALBAN CORPRON;

    申请日2013-01-30

  • 分类号F02C9;B64D31;F02C9/28;B64C27/04;

  • 国家 US

  • 入库时间 2022-08-21 14:33:24

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