公开(公告)号：EP4190695A1

公开(公告)日：2023-06-07

申请号：EP22183853.5

申请日：2022-07-08

申请人： O'Leary, Patrick

发明人： O'Leary, Patrick

IPC分类号： B64C30/00 ,  B64C21/02 ,  B64C23/04 ,  B64C3/14

摘要： A wing structure for a supersonic aircraft including a pair of supersonic wave-tripping channels formed on each of two laterally extending wings of the supersonic aircraft, wherein each of the pair of supersonic wave-tripping channels extend in a span-wise direction of the wings respectively, wherein an upper supersonic wave-tripping channel of the pair of supersonic wave-tripping channels is disposed on an upper surface of each of the wings and a lower supersonic wave-tripping channel of the pair of supersonic wave-tripping channels is disposed on a lower surface of each of the wings, wherein the upper supersonic wave-tripping channel and the lower supersonic wave-tripping channel are set back from a leading edge of the wings respectively.