The invention relates to a wing (2, 3) with two winglets (9-12) and a respective airplane. An upstream winglet broadens a region of inclined airflow and a downstream winglet produces a thrust contribution therein.
КОНСОЛЬ КРЫЛА САМОЛЕТА
2020-08-12
Patent
Electronic Resource
Russian
IPC: | B64C AEROPLANES , Flugzeuge |
НЕРВЮР КРЫЛА, КРЫЛО, ИМЕЮЩЕЕ НЕРВЮРУ КРЫЛА, И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ
European Patent Office | 2020