The invention relates to a flow controlling component (10) for influencing flows around a flow-exposed part (56) in particular of an aircraft. Said flow controlling component (10) comprises a driving device (12) for moving a flow-effective surface (14). In order to allow the flow controlling element (10) to be very easily integrated into the part (56) and allow for a great degree of deflection in a high frequency range while keeping the structure very compact, the driving device (12) has an actuator (16) that can convert a signal into a movement as well as a micro mechanically produced lift-boosting device (18).
申请公布号
WO2009124913(A2)
申请公布日期
2009.10.15
申请号
WO2009EP54096
申请日期
2009.04.06
申请人
EADS DEUTSCHLAND GMBH;BAUER, KARIN;BOLZMACHER, CHRISTIAN;SCHMID, ULRICH;SEIDEL, HELMUT
发明人
BAUER, KARIN;BOLZMACHER, CHRISTIAN;SCHMID, ULRICH;SEIDEL, HELMUT