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

Torque estimation apparatus for vertical take-off and landing aircraft, vertical take-off and landing aircraft, torque estimation program for vertical take-off and landing aircraft, and torque estimation method for vertical take-off and landing aircraft

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

摘要

A torque estimation apparatus (12) of a helicopter (10) stores in a storage apparatus (14) a measurement point that is a measured value of the torque of an engine (28) with respect to a measured value of an engine performance parameter that relates to performance of the engine that rotates a rotor (26) together with a time at which the measurement point is measured, generates an approximate expression based on the measurement point that is stored in the storage apparatus (14), and estimates the amount of a utilizable torque based on the generated approximate expression.
机译:直升机( 10 )的扭矩估计装置( 12 )在存储装置( 14 )中存储作为测量值的测量点发动机扭矩( 28 )相对于与旋转转子( 26 )的发动机性能相关的发动机性能参数的测量值的变化测量点的时间,根据存储在存储设备中的测量点生成近似表达式( 14 ),并根据生成的近似值估算可利用的扭矩量表达。

著录项

  • 公开/公告号US9334064B2

    专利类型

  • 公开/公告日2016-05-10

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY INDUSTRIES LTD.;

    申请/专利号US201314374399

  • 发明设计人 TETSUYA TAKASAKI;

    申请日2013-03-14

  • 分类号B64D45/00;B64C27/04;B64D31/06;F02C9/00;G01L5/13;B64C29/00;

  • 国家 US

  • 入库时间 2022-08-21 14:28:42

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