An aircraft lift device (100) comprises a strake (102) capable of coupling to an aircraft fuselage (104) and extending to a leading edge (106) of a wing (108). The strake (102) has a leading edge (110). The lift device (100) further comprises a leading-edge flap (112) coupled to the strake leading edge (110).
申请公布号
WO2005049424(A3)
申请公布日期
2006.02.02
申请号
WO2004US27652
申请日期
2004.08.25
申请人
SUPERSONIC AEROSPACE INTERNATIONAL, LLC;MORGENSTERN, JOHN, M.;ARSLAN, ALAN
