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公开(公告)号:US20150084963A1
公开(公告)日:2015-03-26
申请号:US14265625
申请日:2014-04-30
Applicant: GE Aviation Systems Limited
Inventor: Donna Louise Green , Brian David Larder , Andrew James Smith , Peter Robin Knight
CPC classification number: G01D7/02 , G06T11/206
Abstract: A method of displaying a parameter that can be modeled by an algorithm having multiple variables on a display to provide an understanding of an impact of the variables on the parameter, the method includes displaying on a first portion of the display a plot of the parameter for a first period and simultaneously with the display of the plot of the parameter, displaying on a second portion of the display, different from the first portion, a plot related to the parameter.
Abstract translation: 一种显示可以通过在显示器上具有多个变量的算法来建模的参数以提供对变量对参数的影响的理解的方法,所述方法包括在显示器的第一部分上显示参数的图, 第一时段,同时显示参数图,在与第一部分不同的显示器的第二部分上显示与该参数有关的曲线。
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公开(公告)号:US11113610B2
公开(公告)日:2021-09-07
申请号:US14836288
申请日:2015-08-26
Applicant: GE Aviation Systems Limited
Inventor: Donna Louise Green , Brian David Larder , Peter Robin Knight , Olivier Thuong
Abstract: A system and related method for building and deploying one or more inference models for use in remote condition monitoring of a first fleet of a first asset. The system includes model configuration data for subsequent use by a model builder application to construct one or more desired inference models for the first asset. The model configuration data is customized to the first asset and the desired one or more inference models, and is provided in a format which is easily readable and editable by a user of the system. The model configuration data is separate from the underlying processing algorithms which are employed by the model builder application in the constructing of the one or more desired inference models during a learning mode of operation of the system.
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公开(公告)号:US10008051B2
公开(公告)日:2018-06-26
申请号:US15115916
申请日:2015-02-10
Applicant: GE Aviation Systems Limited
Inventor: Donna Louise Green , Peter Robin Knight , Oliver Thuong
CPC classification number: G07C5/0825 , F02C6/08 , F02C9/18 , F05D2220/323 , F05D2260/80 , F05D2270/306 , G07C5/0808
Abstract: A method of detecting a fault in a bleed air system of an aircraft having multiple engines is disclosed. The method includes transmitting a bleed air flow rate from multiple engines, determining a difference between the transmitted bleed air flow rates to define a difference value, and determining, by a controller, a fault condition with the bleed air system based on the difference value.
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