首页> 外国专利> FLIGHT MANAGEMENT SYSTEM FOR GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE

FLIGHT MANAGEMENT SYSTEM FOR GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE

机译:飞机起飞期间产生可变推力回切的飞行管理系统

摘要

A flight management system is provided for generating a variable thrust cutback during aircraft departure. The flight management system includes memory storing a sound exposure level limit for a navigation flight and storing expected sound exposure levels for an aircraft, and one or more inputs for receiving sensed aircraft variables including altitude and airspeed. The system also includes a processor for processing the sensed altitude and airspeed and stored sound exposure levels. The processor further computes an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels for controlling aircraft throttle during departure.
机译:提供了一种飞行管理系统,用于在飞机离开期间产生可变的推力减小。飞行管理系统包括存储器,该存储器存储用于导航飞行的声音暴露水平极限并存储飞机的预期声音暴露水平,以及一个或多个输入,用于接收所感测的飞机变量,包括高度和空速。该系统还包括处理器,用于处理感测到的高度和空速以及存储的声音暴露水平。处理器还基于高度,空速和在飞机起飞时控制飞机油门的声音暴露水平,计算出符合声音暴露水平极限的发动机推力值。

著录项

  • 公开/公告号CA2680287C

    专利类型

  • 公开/公告日2015-04-28

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号CA20082680287

  • 发明设计人 DEJONGE MICHAEL K.;

    申请日2008-03-07

  • 分类号G05D1/06;

  • 国家 CA

  • 入库时间 2022-08-21 15:11:39

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号