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US09404425B2 Device and a method of regulating a power plant including at least one turbine engine, and an aircraft 有权
装置和调节包括至少一个涡轮发动机和飞行器的动力装置的方法

  • Patent Title: Device and a method of regulating a power plant including at least one turbine engine, and an aircraft
  • Patent Title (中): 装置和调节包括至少一个涡轮发动机和飞行器的动力装置的方法
  • Application No.: US13747533
    Application Date: 2013-01-23
  • Publication No.: US09404425B2
    Publication Date: 2016-08-02
  • Inventor: Laurent Martin
  • Applicant: AIRBUS HELICOPTERS
  • Applicant Address: FR Marignane
  • Assignee: Airbus Helicopters
  • Current Assignee: Airbus Helicopters
  • Current Assignee Address: FR Marignane
  • Agency: Brooks Kushman P.C.
  • Priority: FR1200343 20120206
  • Main IPC: F02C9/00
  • IPC: F02C9/00 ;  F02C9/56
Device and a method of regulating a power plant including at least one turbine engine, and an aircraft
Abstract:
A regulator device (10) for regulating a turbine engine (3). The regulator device (10) includes mechanical power take-off means (100) for taking off power mechanically from a gas generator (4), and an engine computer (20) controlling said engine (3) to comply with at least a first limitation (LimTET, LimT45) of a temperature (TET, T45) of the gas within the engine, and with a second limitation (LimNg) of a speed of rotation (Ng) of the gas generator (4). The engine computer (20) determines whether the speed of rotation (Ng) of the gas generator has reached said second limitation (LimNg), and whether said temperature (TET, T45) has reached said first limitation (LimTET, LimT45). An avionics computer (30) causes the mechanical power take-off means (100) to operate if the speed of rotation (Ng) of the gas generator (4) has reached said second limitation (LimNg), and if said temperature (TET, T45) has not reached said first limitation (LimTET, LimT45).
Abstract(Chinese):

一种用于调节涡轮发动机（3）的调节装置（10）。 调节装置（10）包括用于从气体发生器（4）机械地断电的机械动力输出装置（100）和控制所述发动机（3）的发动机计算机（20）至少符合第一限制 （LimTET，LimT45）和发动机内气体的温度（TET，T45）以及气体发生器（4）的旋转速度（Ng）的第二限制（LimNg）。 发动机计算机（20）确定气体发生器的旋转速度（Ng）是否已达到所述第二限制（LimNg），以及所述温度（TET，T45）是否达到所述第一限制（LimTET，LimT45）。 如果气体发生器（4）的旋转速度（Ng）达到第二限制（LimNg），则航空电子计算机（30）使得机械动力输出装置（100）运行，并且如果所述温度（TET， T45）尚未达到第一个限制（LimTET，LimT45）。

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