-
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。
-
Patent Agency Ranking
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：US09971969B2
公开(公告)日：2018-05-15
申请号：US15119393
申请日：2014-02-21
Applicant: Taleris Global LLP
Inventor： Robert William Horabin , Julia Ann Howard , Frank Beaven
CPC classification number: G06N5/04 , B64D13/06 , B64D13/08 , G05B23/0235
Abstract: A method of predicting a fault in an air-conditioning pack of an aircraft is disclosed. The air-conditioning pack includes one or more sensors outputting data related to air-conditioning pack temperature, air-conditioning pack pressure, or air-conditioning pack valve or actuator positions. The method includes transmitting data from at least one of the sensors operably coupled to the air-conditioning pack, comparing the transmitted data to a predetermined threshold, and predicting a fault in the air-conditioning pack based thereon.
-
公开(公告)号：US10228687B2
公开(公告)日：2019-03-12
申请号：US15119877
申请日：2014-02-21
Applicant: TALERIS GLOBAL LLP
Inventor： Frank Beaven , Julia Ann Howard , Robert William Horabin
Abstract: A method of diagnosing a fault in an air-conditioning pack of an aircraft is disclosed, wherein the air-conditioning pack includes one or more sensors. The method includes transmitting data from at least one of the sensors operably coupled to the air-conditioning pack, comparing the transmitted data to a predetermined threshold, and diagnosing a fault in the air-conditioning pack based on the comparison.
-
5.发明申请公开(公告)号：US20170060125A1
公开(公告)日：2017-03-02
申请号：US15119877
申请日：2014-02-21
Applicant: TALERIS GLOBAL LLP
Inventor： Frank Beaven , Julia Ann Howard , Robert William Horabin
CPC classification number: G05B23/0235 , B64D13/06 , B64D13/08 , B64D2013/0618 , G07C5/0816
Abstract: A method of diagnosing a fault in an air-conditioning pack of an aircraft is disclosed, wherein the air-conditioning pack includes one or more sensors. The method includes transmitting data from at least one of the sensors operably coupled to the air-conditioning pack, comparing the transmitted data to a predetermined threshold, and diagnosing a fault in the air-conditioning pack based on the comparison.
Abstract translation: 公开了一种用于诊断飞机的空调包装中的故障的方法，其中所述空调包包括一个或多个传感器。 该方法包括从可操作地耦合到空调组件的传感器中的至少一个传送数据，将传送的数据与预定阈值进行比较，以及基于该比较来诊断空调包中的故障。
-
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
6
records
(took 0.012 seconds)
