The invention relates to an elongated, torsion-deformable aerodynamic element, in which the upper surface (2) is continuous while the lower surface (3) comprises a longitudinal slot (6) in the direction of the span and in the vicinity of the leading edge (4). Furthermore, an actuator device (14) inside said aerodynamic element is capable of sliding the edges (6A and 6R) of the slot (6) relative to each other.
申请公布号
WO2009103865(A2)
申请公布日期
2009.08.27
申请号
WO2008FR01681
申请日期
2008.12.03
申请人
ONERA (OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES);MERCIER DES ROCHETTES, HUGGES;JOLY, DIDIER;BUCHANIEK, LEON
发明人
MERCIER DES ROCHETTES, HUGGES;JOLY, DIDIER;BUCHANIEK, LEON