首页> 外国专利> METHOD AND ELECTRONIC DEVICE FOR DETERMINING AT LEAST ONE FUEL CONSUMPTION DOMAIN FOR AN AIRCRAFT, RELATED COMPUTER PROGRAM AND ELECTRONIC DISPLAY SYSTEM

METHOD AND ELECTRONIC DEVICE FOR DETERMINING AT LEAST ONE FUEL CONSUMPTION DOMAIN FOR AN AIRCRAFT, RELATED COMPUTER PROGRAM AND ELECTRONIC DISPLAY SYSTEM

机译:用于确定飞机的至少一个燃料消耗域的方法和电子装置,相关的计算机程序和电子显示系统

摘要

This method for determining at least one fuel cosumption domain for an aircraft is implemented by an electronic device. It comprises acquiring a flight envelope as a function of the altitude and a propulsion variable.;It comprises, for at least one flight phase, calculating a consumption limit curve as a function of the altitude and the propulsion variable, corresponding to a forecasted average consumption for said flight phase; and determining—from the flight envelope and the limit curve—the consumption domain as a function of the altitude and the propulsion variable and including a first consumption subdomain lower than the forecasted consumption for said flight phase and a second consumption subdomain greater than said forecasted consumption, the first and second subdomains being separated by the limit curve.
机译:用于确定飞机的至少一个燃料消耗域的这种方法由电子设备实现。它包括获取作为海拔高度和推进变量的函数的飞行包络线;它包括针对至少一个飞行阶段计算作为海拔高度和推进变量的函数的消耗极限曲线,对应于预测的平均消耗量在所述飞行阶段;从飞行包线和极限曲线确定作为高度和推进变量的函数的消耗域,包括低于所述飞行阶段的预测消耗的第一消耗子域和大于所述预测消耗的第二消耗子域,第一和第二子域由极限曲线分开。

著录项

  • 公开/公告号US2020262575A1

    专利类型

  • 公开/公告日2020-08-20

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号US202016790434

  • 申请日2020-02-13

  • 分类号B64D37;G01F9/02;

  • 国家 US

  • 入库时间 2022-08-21 11:25:17

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