公开(公告)号：US20140107873A1

公开(公告)日：2014-04-17

申请号：US14049291

申请日：2013-10-09

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Marie-Claire Moune ,  Jean Muller ,  Stéphane Cote

IPC: G08G5/02

CPC classification number: G08G5/02 ,  G05D1/0072

Abstract: A method and system for managing automatic guidance of an aircraft during a complete engine failure. Said system includes means for monitoring engines so as to be able to detect a complete failure of the engines; means for detecting whether the aircraft is in flight; means for detecting whether the aircraft is in a different guidance mode from a guidance mode configured to make the aircraft descend with a reduced engine thrust and a fixed speed; and control means for automatically bringing guidance means of the aircraft into a guidance configuration compatible with the situation associated with the complete failure of the engines.

Abstract translation: 一种用于在整个发动机故障期间管理飞行器的自动引导的方法和系统。 所述系统包括用于监测发动机以便能够检测发动机的完全故障的装置; 检测飞机是否飞行的手段; 用于检测飞行器是否处于与引导模式不同的引导模式的装置，所述引导模式被配置成使得飞行器以降低的发动机推力和固定速度下降; 以及用于将飞行器的引导装置自动引导到与发动机完全失效相关的情况相一致的引导配置的控制装置。

公开(公告)号：US09454908B2

公开(公告)日：2016-09-27

申请号：US14049291

申请日：2013-10-09

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Marie-Claire Moune ,  Jean Muller ,  Stéphane Cote

IPC: G08G5/02 ,  G05D1/00

CPC classification number: G08G5/02 ,  G05D1/0072

Abstract: A method and system for managing automatic guidance of an aircraft during a complete engine failure. Said system includes means for monitoring engines so as to be able to detect a complete failure of the engines; means for detecting whether the aircraft is in flight; means for detecting whether the aircraft is in a different guidance mode from a guidance mode configured to make the aircraft descend with a reduced engine thrust and a fixed speed; and control means for automatically bringing guidance means of the aircraft into a guidance configuration compatible with the situation associated with the complete failure of the engines.

Abstract translation: 一种用于在整个发动机故障期间管理飞行器的自动引导的方法和系统。 所述系统包括用于监测发动机以便能够检测发动机的完全故障的装置; 检测飞机是否飞行的手段; 用于检测飞行器是否处于与引导模式不同的引导模式的装置，所述引导模式被配置为使飞行器以降低的发动机推力和固定速度下降; 以及用于将飞行器的引导装置自动引导到与发动机完全失效相关的情况相一致的引导配置的控制装置。