-
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
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。
-
2.发明授权公开(公告)号：US11423713B2
公开(公告)日：2022-08-23
申请号：US16621951
申请日：2017-04-04
Applicant: Taleris Global LLP
Abstract: Systems and methods for formatting aviation data for improved aircraft fault detection, diagnosis, and maintenance are provided. One example method includes determining a plurality of available parameters associated with an aircraft. The method includes matching the plurality of available parameters against a plurality of desired parameters to identify a plurality of matched parameters that are both desired and available. The plurality of matched parameters are useful to perform fault diagnosis and prognosis for the aircraft. The method includes determining a priority level for each of the plurality of matched parameters. The method includes creating a standardized maintenance-optimized data frame configuration based at least in part on the plurality of matched parameters and the priority level for each of the plurality of matched parameters.
-
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
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。
-
-
Search Results
3
records
(took 0.009 seconds)
