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Methods and aircraft for optimized reverse thrust operation during landing

机译:用于在着陆期间优化反推力操作的方法和飞机

摘要

An example method of optimizing reverse thrust operation on an aircraft having two or more engines while landing the aircraft is described. The method includes operating the two or more engines on the aircraft in a reverse idle during a landing rollout of the aircraft, responsively causing deployment of a thrust reverser on each of the engines causing a first reverse idle thrust for slowing the aircraft, monitoring each of the engines for failure of deployment of the thrust reverser, and based on detection of a failure of deployment of a respective thrust reverser on one of the engines, operating the one of the engines on the aircraft at a second reverse idle thrust optimized for a direction of an applied thrust of the one of the engines. The second reverse idle thrust is lower than the first reverse idle thrust.
机译:描述了在着陆飞机时优化具有两个或更多个发动机的飞机上的反推力操作的示例方法。该方法包括在飞机着陆展开期间以反向怠速操作飞机上的两个或多个发动机,响应地引起推力反向器在每个发动机上的部署,从而引起第一反向怠速推力,以使飞机减速,监视每个所述发动机用于推力反向器的展开失败,并且基于检测到相应推力反向器在一个发动机上展开失败,以针对一个方向优化的第二反向空转推力来操作飞机上的一个发动机。一台发动机施加的推力第二反向空转推力小于第一反向空转推力。

著录项

  • 公开/公告号US10703498B2

    专利类型

  • 公开/公告日2020-07-07

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201715801486

  • 发明设计人 CHRISTOPHER M. HODGES;MELISSA L. GATES;

    申请日2017-11-02

  • 分类号B64D31/10;B64D45;B64D27/18;

  • 国家 US

  • 入库时间 2022-08-21 11:29:54

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