Transverse driving bodies, particularly airplane wings

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 45R, B64C 310

Patent

active

047009110

ABSTRACT:
This invention relates to a transverse driving body, particularly an aircraft wing, the wing comprising a wing tip extending basic parts of the wing in the span direction for the purpose of increasing the aspect ratio, the wing tip being of triangular design with a sweptback leading edge, and the profile camber of each of the wing tip increasing at least over a portion of the extension thereof from a basic wing part to the wing tip.

REFERENCES:
patent: 1337515 (1920-04-01), Holle
patent: 1421934 (1922-07-01), Gary
patent: 1547644 (1925-07-01), Crowst et al.
patent: 1817275 (1931-08-01), Soldenhoff
patent: 2441758 (1948-05-01), Garbel
patent: 2609055 (1952-09-01), Monroe
patent: 2643076 (1953-06-01), Hurel
patent: 2709052 (1955-05-01), Berg
"Jane's All the World Aircraft" 1977-78 p. 248.

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