首页> 外国专利> METHOD AND AN APPARATUS FOR ASSISTING THE PILOTAGE OF AN AIRCRAFT AND THE AIRCRAFT CAPABLE OF PROVIDING YAWING CONTROL WITH A MAIN LIFT AND A PROPULSION ROTOR

METHOD AND AN APPARATUS FOR ASSISTING THE PILOTAGE OF AN AIRCRAFT AND THE AIRCRAFT CAPABLE OF PROVIDING YAWING CONTROL WITH A MAIN LIFT AND A PROPULSION ROTOR

机译:用于辅助飞机的引航的方法和装置以及具有主升降和推进转子的偏航控制能力的飞机

摘要

PURPOSE: A method and an apparatus for assisting the pilotage of an aircraft and the aircraft are provided to assist the pilotage of the aircraft with first and second rotors driven by a power plant including a main gear box.;CONSTITUTION: A method for assisting the pilotage of an aircraft is as follows. Current first and second collective pitches are determined. An index(63) is displayed in a diagram(60) with a first shaft(61) and a second shaft(62). Scales are marked on the first and second shafts by collective pitch units related to the first and second collective pitches. The index indicates the first and second collective pitches. A limited parameter which is the closet one to its limitations among monitoring parameters in a current operational rating of engines(2,3) is determined. Power margin capable of being used to at least one of the engines is determined. One power limitation curve(70) is determined per each power margin.;COPYRIGHT KIPO 2013
机译:目的:提供一种用于辅助飞机驾驶的方法和装置,以及飞机,以利用由包括主齿轮箱的动力装置驱动的第一和第二转子辅助飞机的驾驶。飞机的领航情况如下。确定当前的第一和第二集体音调。在图(60)中显示具有第一轴(61)和第二轴(62)的索引(63)。标尺在第一和第二轴上通过与第一和第二集合螺距相关的集合螺距单位进行标记。该索引指示第一和第二集体音调。确定一个限制参数,该限制参数是引擎(2,3)当前运行额定值中与监控参数之间的限制最接近的限制。确定能够用于至少一个发动机的功率裕度。每个功率裕度确定一条功率限制曲线(70)。; COPYRIGHT KIPO 2013

著录项

  • 公开/公告号KR20120112223A

    专利类型

  • 公开/公告日2012-10-11

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号KR20120033149

  • 发明设计人 CORPRON ALBAN;PETIT STEPHANE;

    申请日2012-03-30

  • 分类号B64D45/00;G01C23/00;G06F3/14;B64C27/00;

  • 国家 KR

  • 入库时间 2022-08-21 17:09:01

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