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
WO2013006340(A1)
申请公布日期
2013.01.10
申请号
WO2012US44405
申请日期
2012.06.27
申请人
EATON CORPORATION;THOMPSON, ANDREW;BAKER, JEFFREY, A.;NEELY, JOHN, D.;TORRES, PETER, A.
发明人
THOMPSON, ANDREW;BAKER, JEFFREY, A.;NEELY, JOHN, D.;TORRES, PETER, A.