A wingtip device for a wing is provided. The wingtip device has an inner end and an outer end, and in which the local dihedral of the wingtip device increases or reduces from the inner end to the outer end, with a pressure-side flow surface and a suction-side flow surface. At least two ancillary wing sections are arranged on the wingtip device, projecting in each case from the flow surface of the wingtip device. The ancillary wing sections in each case form an interface with the surface of the wingtip device; which interfaces are located spaced apart from one another. A wing with such a wingtip device is also provided.
Wingtip device of a wing, and also a wing with such a wingtip device
2020-01-07
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Wingtip device of a wing, and also a wing with such a wingtip device
Europäisches Patentamt | 2016
|WINGTIP DEVICE OF A WING AND ALSO A WING WITH SUCH A WINGTIP DEVICE
Europäisches Patentamt | 2019
Wingtip Treatments for Transonic Wing Planforms
AIAA | 2024
|