发明名称 |
ELECTRONICALLY SYNCHRONIZED FLAP SYSTEM |
摘要 |
An electronically-synchronized flap system for a fixed-wing aircraft including a first wing (120) including a first flap panel (122), the first flap panel (122) being connected with a first in-board actuator (124) and a first out-board actuator(126), and a second wing (130) including a second flap panel(132), the second flap panel (132) being connected with a second in-board actuator (134) and a second out-board actuator (136). The system further includes an electronic control unit (ECU) (114) configured to control the first and second in-board and out-board actuators to electronically synchronize the positions of the first and second flap panels. |
申请公布号 |
CA2840391(A1) |
申请公布日期 |
2013.01.10 |
申请号 |
CA20122840391 |
申请日期 |
2012.06.27 |
申请人 |
EATON CORPORATION |
发明人 |
THOMPSON, ANDREW;BAKER, JEFFREY A.;NEELY, JOHN D.;TORRES, PETER A. |
分类号 |
B64C13/28;B64C13/30 |
主分类号 |
B64C13/28 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|