首页> 外国专利> Torque estimation device of vertical take-off and landing aircraft, vertical take-off and landing aircraft, vertical take-off and landing aircraft torque estimation program, and torque estimation method of vertical take-off and landing aircraft

Torque estimation device of vertical take-off and landing aircraft, vertical take-off and landing aircraft, vertical take-off and landing aircraft torque estimation program, and torque estimation method of vertical take-off and landing aircraft

机译:垂直起降飞机的扭矩估计装置,垂直起降飞机,垂直起降飞机扭矩估计程序以及垂直起降飞机的扭矩估计方法

摘要

PROBLEM TO BE SOLVED: To easily estimate a magnitude of an available torque from limited engine performance parameters in real time regardless of a rapid change in engine performance.;SOLUTION: In a torque estimation apparatus 12 for a helicopter 10, a measuring point that is a measurement of a torque of an engine 28 which rotates a rotor 26, with respect to a measurement of an engine parameter relating to a performance of the engine is stored in a storage device 14 together with a time of measurement, an approximate expression is generated based on the measuring point stored in the storage device 14, and a magnitude of an available torque is estimated from the generated approximate expression.;COPYRIGHT: (C)2014,JPO&INPIT
机译:要解决的问题:无论发动机性能如何快速变化,都可以从有限的发动机性能参数中实时轻松地轻松估算可用扭矩的大小。解决方案:在直升机10的扭矩估算设备12中,测量点相对于与发动机的性能有关的发动机参数的测量值,将使转子26旋转的发动机28的转矩的测量值与测量时间一起存储在存储装置14中。基于存储在存储设备14中的测量点,并根据所生成的近似表达式估算可用扭矩的大小。;版权:(C)2014,JPO&INPIT

著录项

  • 公开/公告号JP5832352B2

    专利类型

  • 公开/公告日2015-12-16

    原文格式PDF

  • 申请/专利权人 三菱重工業株式会社;

    申请/专利号JP20120077012

  • 发明设计人 高崎 徹也;

    申请日2012-03-29

  • 分类号B64D45/00;B64C27/04;B64C29/00;

  • 国家 JP

  • 入库时间 2022-08-21 14:40:29

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