公开(公告)号：US09567106B2

公开(公告)日：2017-02-14

申请号：US14550367

申请日：2014-11-21

Applicant: Taleris Global LLP

Inventor： Olivier Paul Jacques Thanh Minh Thuong ,  Robert William Horabin ,  Guy Edward Deshotel ,  Mark John Robbins

IPC: G01R31/02 ,  G01R31/08 ,  B64F5/00 ,  G07C5/08 ,  G01M17/00 ,  B64D45/00

CPC classification number: B64F5/60 ,  B64D2045/0085 ,  G01M17/00 ,  G01R31/02 ,  G01R31/021 ,  G01R31/024 ,  G01R31/025 ,  G01R31/08 ,  G07C5/0808 ,  G07C5/0816

Abstract: System and method of identifying a fault in an aircraft having at least one monitored system, including receiving operational data for the at least one monitored system during at least a portion of a flight, receiving user input data from a user input corresponding to the operation of the at least one monitored system, and identifying an actual fault condition, by a controller, when the user input data is determined to be symptomatic of the identified possible fault condition.

Abstract translation: 识别具有至少一个监控系统的飞机中的故障的系统和方法，包括在飞行的至少一部分期间接收至少一个被监控系统的操作数据，从与用户输入相对应的用户输入接收用户输入数据 当所述用户输入数据被确定为所识别的可能的故障状况的症状时，由所述控制器识别实际的故障状况。

公开(公告)号：US20160144983A1

公开(公告)日：2016-05-26

申请号：US14550367

申请日：2014-11-21

Applicant: Taleris Global LLP

Inventor： Olivier Paul Jacques Thanh Minh Thuong ,  Robert William Horabin ,  Guy Edward Deshotel ,  Mark John Robbins

IPC: B64F5/00 ,  G07C5/08 ,  G01M17/00

CPC classification number: B64F5/60 ,  B64D2045/0085 ,  G01M17/00 ,  G01R31/02 ,  G01R31/021 ,  G01R31/024 ,  G01R31/025 ,  G01R31/08 ,  G07C5/0808 ,  G07C5/0816

Abstract: System and method of identifying a fault in an aircraft having at least one monitored system, including receiving operational data for the at least one monitored system during at least a portion of a flight, receiving user input data from a user input corresponding to the operation of the at least one monitored system, and identifying an actual fault condition, by a controller, when the user input data is determined to be symptomatic of the identified possible fault condition.

Abstract translation: 识别具有至少一个监控系统的飞机中的故障的系统和方法，包括在飞行的至少一部分期间接收至少一个被监控系统的操作数据，从与用户输入相对应的用户输入接收用户输入数据 当所述用户输入数据被确定为所识别的可能的故障状况的症状时，由所述控制器识别实际的故障状况。