| 发明名称 |
METHOD AND SYSTEM FOR INTEGRATING GAS TURBINE TRIM BALANCING SYSTEM INTO ELECTRONIC ENGINE CONTROLS |
| 摘要 |
Methods and systems for determining a rebalancing strategy for trim balancing one or more rotational components of a gas turbine. One or more noise, acoustics or vibrational signals may be received at a control device of an aircraft comprising the gas turbine engine while the aircraft is in operation. The one or more noise, acoustics or vibrational signals may be used for determining a rebalancing strategy for one or more unbalanced rotational components. |
| 申请公布号 |
US2014150550(A1) |
申请公布日期 |
2014.06.05 |
| 申请号 |
US201213689855 |
申请日期 |
2012.11.30 |
| 申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
BORWANKAR Paraag;GRANT Heather;MACCHIA Enzo;MCELVAINE Christopher |
| 分类号 |
G01M1/14 |
主分类号 |
G01M1/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for determining a rebalancing strategy for trim balancing one or more rotational components of a gas turbine, the method comprising:
receiving one or more noise, acoustics or vibrational signals at a control device of an aircraft comprising the gas turbine engine while the aircraft is in operation; and using the one or more noise, acoustics or vibrational signals and one or more processors of the control device, determining a rebalancing strategy for one or more unbalanced rotational components.
|
| 地址 |
Longueuil CA |
