首页> 外国专利> In order to offer at least the power parameter of one propeller turbine of the aircraft, the indicator for the aircraft operation which is designed

In order to offer at least the power parameter of one propeller turbine of the aircraft, the indicator for the aircraft operation which is designed

机译:为了至少提供飞机的一台螺旋桨涡轮机的功率参数,设计了用于飞机运行的指示器

摘要

As for this invention, the data source which decides the parameter value regarding the propeller and the turbine of the turboprop and the parameter value regarding the aircraft the processing expedient which presently (2) and the turboprop & the engine calculates the power and it does not bleed at sea surface rank with normal atmospheric pressure power parameter which considers the ratio with the largest powers which are obtained on the basis of the aforementioned value the indicatory expedient which one which shows (3) and the aforementioned power parameter feature sign (11) the supervisory screen (7) is indicated at least on the operation indicator which consists of (5) it regards (1). Selective figure Figure 1
机译:对于本发明,由数据源来决定动力,而该数据源决定与当前(2)以及涡轮螺旋桨发动机和发动机有关的处理权宜的,关于涡轮螺旋桨的螺旋桨和涡轮的参数值以及关于飞机的参数值。具有正常大气压功率参数的海面等级的放气,该功率参数考虑了基于上述值获得的最大功率的比率,该权宜表示(3)和上述功率参数特征符号(11)的指示权。监控屏幕(7)至少显示在与(1)有关的(5)组成的操作指示器上。<选择图>图1

著录项

  • 公开/公告号JP2009501670A

    专利类型

  • 公开/公告日2009-01-22

    原文格式PDF

  • 申请/专利权人 エアバス;

    申请/专利号JP20080522007

  • 发明设计人 コテ、ジャン-フィリップ;

    申请日2006-07-13

  • 分类号B64D43;F02C9;F01D25;

  • 国家 JP

  • 入库时间 2022-08-21 19:39:38

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