| 发明名称 |
Aircraft Prognostics Health System |
| 摘要 |
According to one example embodiment, a method of reassessing use of an aircraft component installed on an aircraft includes receiving, from one or more sensors installed on the aircraft, one or more measurements representative of at least one load applied against the aircraft component; determining, based on the received one or more measurements and based on at least one other received input, an amount of change in probability of failure caused by application of the at least one load against the aircraft component; receiving a change to one of the received one or more measurements or the at least one other received input; and redetermining the change in probability of failure based on the received change. |
| 申请公布号 |
US2015274314(A1) |
申请公布日期 |
2015.10.01 |
| 申请号 |
US201414577314 |
申请日期 |
2014.12.19 |
| 申请人 |
Bell Helicopter Textron Inc. |
发明人 |
Conrad Kevin |
| 分类号 |
B64D45/00;G01M17/007;G01L5/16;G07C5/08 |
主分类号 |
B64D45/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of reassessing use of an aircraft component installed on an aircraft, comprising:
receiving, from one or more sensors installed on the aircraft, one or more measurements representative of at least one load applied against the aircraft component; determining, based on the received one or more measurements and based on at least one other received input, an amount of change in probability of failure caused by application of the at least one load against the aircraft component; receiving a change to one of the received one or more measurements or the at least one other received input; and redetermining the change in probability of failure based on the received change. |
| 地址 |
Fort Worth TX US |
