The disclosure relates to a wing 2 with at least two winglets 8, 9, 10 having a relative dihedral angle between them, and to an airplane having such wings. An upstream winglet 8 broadens a region of inclined airflow, and a more downstream winglet 9 produces a thrust contribution therein.
本发明涉及具有至少两个小翼8、9、10的机翼2,小翼8、9、10具有在其之间的相对上反角,以及涉及具有这样的机翼的飞机。上游小翼8加宽倾斜空气流动的区域,并且更下游的小翼9产生在其中的推力贡献。
Airplane wing
飞机机翼
2020-09-04
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |