| 发明名称 |
POWER CONTROL FOR PROPELLER-DRIVEN AIRCRAFT |
| 摘要 |
A method of controlling an engine for a propeller-driven aircraft, including setting an initial maximum power limit, wherein the initial maximum power limit is associated with a maximum allowable thrust for an aircraft, receiving an indication that a predetermined aircraft condition is satisfied, and setting an updated maximum power limit. |
| 申请公布号 |
US2016207633(A1) |
申请公布日期 |
2016.07.21 |
| 申请号 |
US201614992465 |
申请日期 |
2016.01.11 |
| 申请人 |
Unison Industries, LLC |
发明人 |
McWaters Mark Wayne;Nielsen Scott Richard |
| 分类号 |
B64D31/06;B64D27/04;B64D27/10;B64D31/04;B64D43/00 |
主分类号 |
B64D31/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of controlling an engine for a propeller-driven aircraft, comprising:
setting an initial maximum power limit, wherein the initial maximum power limit is associated with a maximum allowable thrust for an aircraft; receiving an indication that a predetermined aircraft condition is satisfied; and setting an updated maximum power limit above which the engine power is automatically reduced, wherein the updated maximum power limit is greater than the initial maximum power limit. |
| 地址 |
Jacksonville FL US |
