| 发明名称 | Method, systems, and computer readable media for troubleshooting an aircraft system during system failure | ||
| 摘要 | Methods, systems, and computer readable media are disclosed for troubleshooting and repairing an aircraft system failure during abnormal situations of an aircraft's operation. One aspect of a method for implementing the subject matter described herein includes at least one interactive interface configured for troubleshooting and repairing an aircraft system failure. The method also includes displaying at least one or more graphic object representing at least one or more aircraft system and configured for receiving interaction from a user, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and displaying at least one or more macro action icon configured for performing an automated action sequence configured for troubleshooting and repairing the system failure. | ||
| 申请公布号 | US9399525(B2) | 申请公布日期 | 2016.07.26 |
| 申请号 | US201414171444 | 申请日期 | 2014.02.03 |
| 申请人 | AIRBUS OPERATIONS (S.A.S.) | 发明人 | Mesguen Mael;Buron François;Poux Thibaut |
| 分类号 | G01M17/00;B64F5/00;B64D43/00;B64D45/00 | 主分类号 | G01M17/00 |
| 代理机构 | Jenkins, Wilson, Taylor & Hunt, P.A. | 代理人 | Jenkins, Wilson, Taylor & Hunt, P.A. |
| 主权项 | 1. A method for troubleshooting an aircraft system failure, the method comprising: at least one interactive interface configured for troubleshooting and repairing the aircraft system failure and in association with a hardware processor: displaying at least one or more graphic object representing at least one or more aircraft system and configured for receiving interaction from a user, wherein receiving interaction from the user comprises at least one or more of: activating or deactivating an aircraft system associated with the aircraft system failure by functionally interacting with the one or more graphic object displayed on the interactive interface and representing the aircraft system, and activating a safeguard mechanism embedded in the aircraft system by requiring the user to perform a specific interaction to confirm execution of a procedure;displaying at least one or more energy flow icon representing a direction of circulation of an energy flow; anddisplaying at least one or more macro action icon configured for performing an automated action sequence for troubleshooting and repairing the system failure. | ||
| 地址 | Toulouse FR | ||